--- /dev/null
+
+#
+# English base translation file
+#
+# Should you need to add new logical keys here is the proposed method
+#
+# className.ComponentType.componentName
+#
+#
+# Text tokens within braces should not be translated, e.g.
+# "The file '{filename}' exists."
+# They are pieces that are inserted dynamically.
+#
+
+
+! Set to the name of the current translation file (used for debugging purposes)
+debug.currentFile = messages.properties
+
+! RocketActions
+RocketActions.checkbox.Donotaskmeagain = Do not ask me again
+RocketActions.lbl.Youcanchangedefop = You can change the default operation in the preferences.
+RocketActions.showConfirmDialog.lbl1 = Delete the selected simulations?
+RocketActions.showConfirmDialog.lbl2 = <html><i>This operation cannot be undone.</i>
+RocketActions.showConfirmDialog.title = Delete simulations
+RocketActions.DelCompAct.Delete = Delete
+RocketActions.DelCompAct.ttip.Delete = Delete the selected component.
+RocketActions.DelSimuAct.Delete = Delete
+RocketActions.DelSimuAct.ttip.Delete = Delete the selected simulation.
+RocketActions.DelAct.Delete = Delete
+RocketActions.DelAct.ttip.Delete = Delete the selected component or simulation.
+RocketActions.CutAction.Cut = Cut
+RocketActions.CutAction.ttip.Cut = Cut this component or simulation to the clipboard and remove from this design
+RocketActions.CopyAct.Copy = Copy
+RocketActions.CopyAct.ttip.Copy = Copy this component (and subcomponents) to the clipboard.
+RocketActions.PasteAct.Paste = Paste
+RocketActions.PasteAct.ttip.Paste = Paste the component or simulation on the clipboard to the design.
+RocketActions.EditAct.Edit = Edit
+RocketActions.EditAct.ttip.Edit = Edit the selected component.
+RocketActions.NewStageAct.Newstage = New stage
+RocketActions.NewStageAct.ttip.Newstage = Add a new stage to the rocket design.
+RocketActions.ActBoosterstage = Booster stage
+RocketActions.MoveUpAct.Moveup = Move up
+RocketActions.MoveUpAct.ttip.Moveup = Move this component upwards.
+RocketActions.MoveDownAct.Movedown = Move down
+RocketActions.MoveDownAct.ttip.Movedown = Move this component downwards.
+
+! RocketPanel
+RocketPanel.FigTypeAct.Sideview = Side view
+RocketPanel.FigTypeAct.ttip.Sideview = Side view
+RocketPanel.FigTypeAct.Backview = Back view
+RocketPanel.FigTypeAct.ttip.Backview = Rear view
+RocketPanel.lbl.Motorcfg = Motor configuration:
+RocketPanel.lbl.infoMessage = <html>Click to select Shift+click to select other Double-click to edit Click+drag to move
+
+
+! BasicFrame
+BasicFrame.SimpleFileFilter1 = All rocket designs (*.ork; *.rkt)
+BasicFrame.SimpleFileFilter2 = OpenRocket designs (*.ork)
+BasicFrame.SimpleFileFilter3 = RockSim designs (*.rkt)
+BasicFrame.tab.Rocketdesign = Rocket design
+BasicFrame.tab.Flightsim = Flight simulations
+BasicFrame.title.Addnewcomp = Add new component
+BasicFrame.dlg.lbl1 = Design '
+BasicFrame.dlg.lbl2 = ' has not been saved.
+BasicFrame.dlg.lbl3 = Do you want to save it?
+BasicFrame.dlg.title = Design not saved
+BasicFrame.StageName.Sustainer = Sustainer
+BasicFrame.WarningDialog.txt1 = The following problems were encountered while opening
+BasicFrame.WarningDialog.txt2 = Some design features may not have been loaded correctly.
+BasicFrame.WarningDialog.title = Warnings while opening file
+
+
+! General error messages used in multiple contexts
+error.fileExists.title = File exists
+error.fileExists.desc = File '{filename}' exists. Do you want to overwrite it?
+
+error.writing.title = Error writing file
+error.writing.desc = An error occurred while writing to the file:
+
+
+! Labels used in buttons of dialog windows
+# TODO: Rename these to "btn.xxx"
+button.ok = OK
+button.cancel = Cancel
+button.close = Close
+
+! Common labels used in buttons of dialog windows
+dlg.but.ok = OK
+dlg.but.cancel = Cancel
+dlg.but.close = Close
+
+
+! General file type names
+filetypes.pdf = PDF files
+
+
+! About Dialog
+AboutDialog.lbl.version = Version
+! The texts below provide additional credits for the translation maintainer
+! - In AboutDialog.lbl.translation replace "English" with the current language.
+! - AboutDialog.lbl.translator is the translator / group name (may be empty)
+! - AboutDialog.lbl.translatorWebsite is a URL to the translator / group (may be empty)
+! - AboutDialog.lbl.translatorIcon is the file name of an icon under pix/translators/ (may be empty)
+AboutDialog.lbl.translation = English translation by:
+AboutDialog.lbl.translator =
+AboutDialog.lbl.translatorWebsite =
+AboutDialog.lbl.translatorIcon =
+
+
+! Print dialog
+PrintDialog.title = Print or export
+PrintDialog.but.previewAndPrint = Preview & Print
+PrintDialog.checkbox.showByStage = Show by stage
+PrintDialog.lbl.selectElements = Select elements to include:
+printdlg.but.saveaspdf = Save as PDF
+printdlg.but.preview = Preview
+printdlg.but.settings = Settings
+PrintDialog.error.preview.title = Unable to open preview
+PrintDialog.error.preview.desc1 = Unable to open PDF preview.
+PrintDialog.error.preview.desc2 = Please use the "Save as PDF" option instead.
+
+
+!PrintSettingsDialog
+PrintSettingsDialog.title = Print settings
+PrintSettingsDialog.lbl.Templatefillcolor = Template fill color:
+PrintSettingsDialog.lbl.Templatebordercolor = Template border color:
+PrintSettingsDialog.lbl.Papersize = Paper size:
+PrintSettingsDialog.lbl.Paperorientation = Paper orientation:
+PrintSettingsDialog.but.Reset = Reset
+PrintSettingsDialog.but.Close = Close
+
+
+! Bug Report dialog
+bugreport.dlg.title = Bug report
+bugreport.dlg.but.Sendbugreport = Send bug report
+bugreport.dlg.but.Sendbugreport.Ttip = Automatically send the bug report to the OpenRocket developers.
+bugreport.dlg.successmsg1 = Bug report successfully sent.
+bugreport.dlg.successmsg2 = Thank you for helping make OpenRocket better!
+bugreport.dlg.successmsg3 = Bug report sent
+bugreport.dlg.connectedInternet = <html>If connected to the Internet, you can simply click <em>Send bug report</em>.
+bugreport.dlg.otherwise = Otherwise, send the text below to the address:
+bugreport.lbl.Theinformation = The information above may be included in a public bug report. Make sure it does not contain any sensitive information you do not want to be made public.
+bugreport.dlg.failedmsg1 = OpenRocket was unable to send the bug report:
+bugreport.dlg.failedmsg2 = Please send the report manually to
+bugreport.dlg.failedmsg3 = Error sending report
+bugreport.reportDialog.txt = <html><b>You can report a bug in OpenRocket by filling in and submitting the form below.</b><br>You can also report bugs and include attachments on the project web site.
+bugreport.reportDialog.txt2 = <html><b>Please include a short description about what you were doing when the exception occurred.</b>
+bugreport.dlg.provideDescription = Please provide a description of the bug first.
+bugreport.dlg.provideDescription.title = Bug description missing
+
+
+! Debug log dialog
+debuglogdlg.but.clear = Clear
+debuglogdlg.OpenRocketdebuglog = OpenRocket debug log
+debuglogdlg.Displayloglines = Display log lines:
+debuglogdlg.Follow = Follow
+debuglogdlg.col.Time = Time
+debuglogdlg.col.Level = Level
+debuglogdlg.col.Location = Location
+debuglogdlg.col.Message = Message
+debuglogdlg.lbl.Loglinenbr = Log line number:
+debuglogdlg.lbl.Time = Time:
+debuglogdlg.lbl.Level = Level:
+debuglogdlg.lbl.Location = Location:
+debuglogdlg.lbl.Logmessage = Log message:
+debuglogdlg.lbl.Stacktrace = Stack trace:
+
+
+! Edit Motor configuration dialog
+edtmotorconfdlg.but.removemotor = Remove motor
+edtmotorconfdlg.but.Selectmotor = Select motor
+edtmotorconfdlg.but.Removeconfiguration = Remove configuration
+edtmotorconfdlg.but.Newconfiguration = New configuration
+edtmotorconfdlg.lbl.Motormounts = <html><b>Motor mounts:</b>
+edtmotorconfdlg.title.Editmotorconf = Edit motor configurations
+edtmotorconfdlg.selectcomp = <html>Select which components function as motor mounts:
+edtmotorconfdlg.lbl.Motorconfig = <html><b>Motor configurations:</b>
+edtmotorconfdlg.lbl.Configname = Configuration name:
+edtmotorconfdlg.lbl.Leavenamedefault = Leave name empty for default.
+
+! Example design dialog
+exdesigndlg.but.open = Open
+exdesigndlg.lbl.Selectexample = Select example designs to open:
+exdesigndlg.lbl.Openexampledesign = Open example design
+exdesigndlg.lbl.Exampledesignsnotfound = Example designs could not be found.
+exdesigndlg.lbl.Examplesnotfound = Examples not found
+
+
+! Material edit panel
+matedtpan.but.new = New
+matedtpan.but.edit = Edit
+matedtpan.but.delete = Delete
+matedtpan.but.revertall = Revert all
+matedtpan.col.Material = Material
+matedtpan.col.Type = Type
+matedtpan.col.Density = Density
+matedtpan.col.but.ttip.New = Add a new material
+matedtpan.title.Addcustmaterial = Add a custom material
+matedtpan.but.ttip.edit = Edit an existing material
+matedtpan.title.Editmaterial = Edit material
+matedtpan.title2.Editmaterial = The built-in materials cannot be modified.
+matedtpan.but.ttip.delete = Delete a user-defined material
+matedtpan.but.ttip.revertall = Delete all user-defined materials
+matedtpan.title.Deletealluser-defined = Delete all user-defined materials?
+matedtpan.title.Revertall = Revert all?
+matedtpan.lbl.edtmaterials = Editing materials will not affect existing rocket designs.
+
+!MaterialModel
+MaterialModel.title.Material = Material
+MaterialModel.title.Defcustmat = Define custom material
+
+
+! Preference dialog
+pref.dlg.but.add = Add
+pref.dlg.but.reset = Reset
+pref.dlg.but.checknow = Check now
+pref.dlg.but.defaultmetric = Default metric
+pref.dlg.but.defaultimperial = Default imperial
+pref.dlg.title.Preferences = Preferences
+pref.dlg.tab.Units = Units
+pref.dlg.tab.Defaultunits = Default units
+pref.dlg.tab.Materials = Materials
+pref.dlg.tab.Custommaterials = Custom materials
+pref.dlg.tab.Options = Options
+pref.dlg.tab.Miscellaneousoptions = Miscellaneous options
+pref.dlg.lbl.Positiontoinsert = Position to insert new body components:
+pref.dlg.lbl.Confirmdeletion = Confirm deletion of simulations:
+pref.dlg.lbl.User-definedthrust = User-defined thrust curves:
+pref.dlg.Allthrustcurvefiles = All thrust curve files (*.eng; *.rse; *.zip; directories)
+pref.dlg.RASPfiles = RASP motor files (*.eng)
+pref.dlg.RockSimfiles = RockSim engine files (*.rse)
+pref.dlg.ZIParchives = ZIP archives (*.zip)
+pref.dlg.checkbox.Checkupdates = Check for software updates at startup
+pref.dlg.ttip.Checkupdatesnow = Check for software updates now
+pref.dlg.lbl.Selectprefunits = Select your preferred units:
+pref.dlg.lbl.Rocketdimensions = Rocket dimensions:
+pref.dlg.lbl.Linedensity = Line density:
+pref.dlg.lbl.Motordimensions = Motor dimensions:
+pref.dlg.lbl.Surfacedensity = Surface density:
+pref.dlg.lbl.Distance = Distance:
+pref.dlg.lbl.Bulkdensity = Bulk density:
+pref.dlg.lbl.Velocity = Velocity:
+pref.dlg.lbl.Surfaceroughness = Surface roughness:
+pref.dlg.lbl.Acceleration = Acceleration:
+pref.dlg.lbl.Area = Area:
+pref.dlg.lbl.Mass = Mass:
+pref.dlg.lbl.Angle = Angle:
+pref.dlg.lbl.Force = Force:
+pref.dlg.lbl.Rollrate = Roll rate:
+pref.dlg.lbl.Totalimpulse = Total impulse:
+pref.dlg.lbl.Temperature = Temperature:
+pref.dlg.lbl.Momentofinertia = Moment of inertia:
+pref.dlg.lbl.Pressure = Pressure:
+pref.dlg.lbl.Stability = Stability:
+pref.dlg.lbl.FlightTime = Flight time:
+pref.dlg.lbl.effect1 = The effects will take place the next time you open a window.
+pref.dlg.lbl.Checkingupdates = Checking for updates...
+pref.dlg.lbl.msg1 = An error occurred while communicating with the server.
+pref.dlg.lbl.msg2 = Unable to retrieve update information
+pref.dlg.lbl.msg3 = You are running the latest version of OpenRocket.
+pref.dlg.lbl.msg4 = No updates available
+pref.dlg.PrefChoiseSelector1 = Always ask
+pref.dlg.PrefChoiseSelector2 = Insert in middle
+pref.dlg.PrefChoiseSelector3 = Add to end
+pref.dlg.PrefBooleanSelector1 = Delete
+pref.dlg.PrefBooleanSelector2 = Confirm
+pref.dlg.Add = Add
+pref.dlg.DescriptionArea.Adddirectories = Add directories, RASP motor files (*.eng), RockSim engine files (*.rse) or ZIP archives separated by a semicolon (;) to load external thrust curves. Changes will take effect the next time you start OpenRocket.
+
+PreferencesDialog.lbl.language = Interface language:
+PreferencesDialog.languages.default = System default
+PreferencesDialog.lbl.languageEffect = The language will change the next time you start OpenRocket.
+
+! Simulation edit dialog
+simedtdlg.but.runsimulation = Run simulation
+simedtdlg.but.resettodefault = Reset to default
+simedtdlg.but.add = Add
+simedtdlg.but.remove = Remove
+simedtdlg.title.Editsim = Edit simulation
+simedtdlg.lbl.Simname = Simulation name:
+simedtdlg.tab.Launchcond = Launch conditions
+simedtdlg.tab.Simopt = Simulation options
+simedtdlg.tab.Plotdata = Plot data
+simedtdlg.tab.Exportdata = Export data
+simedtdlg.lbl.Motorcfg = Motor configuration:
+simedtdlg.lbl.ttip.Motorcfg = Select the motor configuration to use.
+simedtdlg.combo.ttip.motorconf = Select the motor configuration to use.
+simedtdlg.lbl.Wind = Wind
+simedtdlg.lbl.Averwindspeed = Average windspeed:
+simedtdlg.lbl.ttip.Averwindspeed = The average windspeed relative to the ground.
+simedtdlg.lbl.Stddeviation = Standard deviation:
+simedtdlg.lbl.ttip.Stddeviation = <html>The standard deviation of the windspeed.<br>The windspeed is within twice the standard deviation from the average for 95% of the time.
+simedtdlg.lbl.Turbulenceintensity = Turbulence intensity:
+simedtdlg.lbl.ttip.Turbulenceintensity1 = <html>The turbulence intensity is the standard deviation divided by the average windspeed.<br>
+simedtdlg.lbl.ttip.Turbulenceintensity2 = Typical values range from
+simedtdlg.lbl.ttip.Turbulenceintensity3 = to
+simedtdlg.border.Atmoscond = Atmospheric conditions
+simedtdlg.checkbox.InterStdAtmosphere = Use International Standard Atmosphere
+simedtdlg.checkbox.ttip.InterStdAtmosphere1 = <html>Select to use the International Standard Atmosphere model.<br>This model has a temperature of
+simedtdlg.checkbox.ttip.InterStdAtmosphere2 = and a pressure of
+simedtdlg.checkbox.ttip.InterStdAtmosphere3 = at sea level.
+simedtdlg.lbl.Temperature = Temperature:
+simedtdlg.lbl.ttip.Temperature = The temperature at the launch site.
+simedtdlg.lbl.Pressure = Pressure:
+simedtdlg.lbl.ttip.Pressure = The atmospheric pressure at the launch site.
+simedtdlg.lbl.Launchsite = Launch site
+simedtdlg.lbl.Latitude = Latitude:
+simedtdlg.lbl.ttip.Latitude = <html>The launch site latitude affects the gravitational pull of Earth.<br>Positive values are on the Northern hemisphere, negative values on the Southern hemisphere.
+
+simedtdlg.lbl.Longitude = Longitude:
+simedtdlg.lbl.ttip.Longitude = <html>Required for weather prediction and elevation models.
+
+simedtdlg.lbl.Altitude = Altitude:
+simedtdlg.lbl.ttip.Altitude = <html>The launch altitude above mean sea level.<br>This affects the position of the rocket in the atmospheric model.
+simedtdlg.border.Launchrod = Launch rod
+simedtdlg.lbl.Length = Length:
+simedtdlg.lbl.ttip.Length = The length of the launch rod.
+simedtdlg.lbl.Angle = Angle:
+simedtdlg.lbl.ttip.Angle = The angle of the launch rod from vertical.
+simedtdlg.lbl.Direction = Direction:
+simedtdlg.lbl.ttip.Direction1 = <html>Direction of the launch rod relative to the wind.<br>
+simedtdlg.lbl.ttip.Direction2 = = towards the wind,
+simedtdlg.lbl.ttip.Direction3 = = downwind.
+simedtdlg.border.Simopt = Simulator options
+simedtdlg.lbl.Calcmethod = Calculation method:
+simedtdlg.lbl.ttip.Calcmethod = <html>The Extended Barrowman method calculates aerodynamic forces according <br>to the Barrowman equations extended to accommodate more components.
+simedtdlg.lbl.ExtBarrowman = Extended Barrowman
+simedtdlg.lbl.Simmethod = Simulation method:
+simedtdlg.lbl.ttip.Simmethod1 = <html>The six degree-of-freedom simulator allows the rocket total freedom during flight.<br>
+simedtdlg.lbl.ttip.Simmethod2 = Integration is performed using a 4<sup>th</sup> order Runge-Kutta 4 numerical integration.
+simedtdlg.lbl.GeodeticMethod = Geodetic calculations:
+simedtdlg.lbl.ttip.GeodeticMethodTip = Relate to the calculation of coordinates on the earth. This also enables coriolis effect computations.
+simedtdlg.lbl.Timestep = Time step:
+simedtdlg.lbl.ttip.Timestep1 = <html>The time between simulation steps.<br>A smaller time step results in a more accurate but slower simulation.<br>
+simedtdlg.lbl.ttip.Timestep2 = The 4<sup>th</sup> order simulation method is quite accurate with a time step of
+simedtdlg.but.ttip.resettodefault = Reset the time step to its default value (
+simedtdlg.border.Simlist = Simulator listeners
+simedtdlg.txt.longA1 = <html><i>Simulation listeners</i> is an advanced feature that allows user-written code to listen to and interact with the simulation.
+simedtdlg.txt.longA2 = For details on writing simulation listeners, see the OpenRocket technical documentation.
+simedtdlg.lbl.Curlist = Current listeners:
+simedtdlg.lbl.Addsimlist = Add simulation listener
+simedtdlg.lbl.Noflightdata = No flight data available.
+simedtdlg.lbl.runsimfirst = Please run the simulation first.
+simedtdlg.chart.Simflight = Simulated flight
+simedtdlg.dlg.Simres = Simulation results
+simedtdlg.IntensityDesc.None = None
+simedtdlg.IntensityDesc.Verylow = Very low
+simedtdlg.IntensityDesc.Low = Low
+simedtdlg.IntensityDesc.Medium = Medium
+simedtdlg.IntensityDesc.High = High
+simedtdlg.IntensityDesc.Veryhigh = Very high
+simedtdlg.IntensityDesc.Extreme = Extreme
+
+GeodeticComputationStrategy.flat.name = Flat Earth
+GeodeticComputationStrategy.flat.desc = Perform computations with a flat Earth approximation. Sufficient for low-altitude flights.
+GeodeticComputationStrategy.spherical.name = Spherical approximation
+GeodeticComputationStrategy.spherical.desc = <html>Perform geodetic computations assuming a spherical Earth.<br>This is sufficiently accurate for almost all purposes.
+GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid
+GeodeticComputationStrategy.wgs84.desc = <html>Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.<br>Slower and unnecessary in most cases.
+
+
+
+
+! Simulation Panel
+simpanel.but.newsimulation = New simulation
+simpanel.but.editsimulation = Edit simulation
+simpanel.but.runsimulations = Run simulations
+simpanel.but.deletesimulations = Delete simulations
+simpanel.but.plotexport = Plot / export
+simpanel.but.ttip.newsimulation = Add a new simulation
+simpanel.but.ttip.editsim = Edit the selected simulation
+simpanel.but.ttip.runsimu = Re-run the selected simulations
+simpanel.but.ttip.deletesim = Delete the selected simulations
+simpanel.checkbox.donotask = Do not ask me again
+simpanel.lbl.defpref = You can change the default operation in the preferences.
+simpanel.dlg.lbl.DeleteSim1 = Delete the selected simulations?
+simpanel.dlg.lbl.DeleteSim2 = <html><i>This operation cannot be undone.</i>
+simpanel.dlg.lbl.DeleteSim3 = Delete simulations
+simpanel.col.Name = Name
+simpanel.col.Motors = Motors
+simpanel.col.Apogee = Apogee
+simpanel.col.Maxvelocity = Max. velocity
+simpanel.col.Maxacceleration = Max. acceleration
+simpanel.col.Timetoapogee = Time to apogee
+simpanel.col.Flighttime = Flight time
+simpanel.col.Groundhitvelocity = Ground hit velocity
+
+! SimulationRunDialog
+SimuRunDlg.title.RunSim = Running simulations...
+SimuRunDlg.lbl.Running = Running ...
+SimuRunDlg.lbl.Simutime = Simulation time:
+SimuRunDlg.lbl.Altitude = Altitude:
+SimuRunDlg.lbl.Velocity = Velocity:
+SimuRunDlg.msg.Unabletosim = Unable to simulate:
+SimuRunDlg.msg.errorOccurred = An error occurred during the simulation:
+SimuRunDlg.msg.AnException1 = An exception occurred during the simulation:
+SimuRunDlg.msg.AnException2 = Please report this as a bug along with the details below.
+SimuRunDlg.msg.AssertionError1 = A computation error occurred during the simulation.
+SimuRunDlg.msg.AssertionError2 = Please report this as a bug along with the details below.
+SimuRunDlg.msg.unknownerror1 = An unknown error was encountered during the simulation.
+SimuRunDlg.msg.unknownerror2 = The program may be unstable, you should save all your designs and restart OpenRocket now!
+
+
+RK4SimulationStepper.error.valuesTooLarge = Simulation values exceeded limits. Try selecting a shorter time step.
+
+
+! SimulationExportPanel
+SimExpPan.desc = Comma Separated Files (*.csv)
+SimExpPan.border.Vartoexport = Variables to export
+SimExpPan.but.Selectall = Select all
+SimExpPan.but.Selectnone = Select none
+SimExpPan.border.Fieldsep = Field separator
+SimExpPan.lbl.Fieldsepstr = Field separator string:
+SimExpPan.lbl.longA1 = <html>The string used to separate the fields in the exported file.<br>
+SimExpPan.lbl.longA2 = Use ',' for a Comma Separated Values (CSV) file.
+SimExpPan.checkbox.Includesimudesc = Include simulation description
+SimExpPan.checkbox.ttip.Includesimudesc = Include a comment at the beginning of the file describing the simulation.
+SimExpPan.border.Comments = Comments
+SimExpPan.checkbox.Includefielddesc = Include field descriptions
+SimExpPan.checkbox.ttip.Includefielddesc = Include a comment line with the descriptions of the exported variables.
+SimExpPan.checkbox.Incflightevents = Include flight events
+SimExpPan.checkbox.ttip.Incflightevents = Include a comment line for every flight event.
+SimExpPan.lbl.Commentchar = Comment character:
+SimExpPan.lbl.ttip.Commentchar = The character(s) that mark a comment line.
+SimExpPan.but.Exporttofile = Export to file...
+SimExpPan.Fileexists.desc1 = File \"
+SimExpPan.Fileexists.desc2 = \" exists. Overwrite?
+SimExpPan.Fileexists.title = File exists
+SimExpPan.ExportingVar.desc1 = Exporting 1 variable out of
+SimExpPan.ExportingVar.desc2 = Exporting
+SimExpPan.ExportingVar.desc3 = variables out of
+SimExpPan.Col.Variable = Variable
+SimExpPan.Col.Unit = Unit
+
+
+CsvOptionPanel.separator.space = SPACE
+CsvOptionPanel.separator.tab = TAB
+
+
+
+! MotorPlot
+MotorPlot.title.Motorplot = Motor plot
+MotorPlot.but.Select = Select
+MotorPlot.Chart.Motorthrustcurve = Motor thrust curve
+MotorPlot.Chart.Time = Time / s
+MotorPlot.Chart.Thrust = Thrust / N
+MotorPlot.txt.Designation = Designation:
+MotorPlot.txt.Manufacturer = Manufacturer:
+MotorPlot.txt.Type = Type:
+MotorPlot.txt.Delays = Delays:
+MotorPlot.txt.Comment = Comment:\n
+
+
+
+! Simulation plot panel
+simplotpanel.lbl.Presetplotconf = Preset plot configurations:
+simplotpanel.lbl.Xaxistype = X axis type:
+simplotpanel.lbl.Unit = Unit:
+simplotpanel.lbl.Yaxistypes = Y axis types:
+simplotpanel.lbl.Flightevents = Flight events:
+simplotpanel.but.All = All
+simplotpanel.but.None = None
+simplotpanel.but.NewYaxisplottype = New Y axis plot type
+simplotpanel.but.Plotflight = Plot flight
+simplotpanel.lbl.Axis = Axis:
+simplotpanel.but.ttip.Removethisplot = Remove this plot
+simplotpanel.Desc = The data will be plotted in time order even if the X axis type is not time.
+simplotpanel.OptionPane.lbl1 = A maximum of 15 plots is allowed.
+simplotpanel.OptionPane.lbl2 = Cannot add plot
+simplotpanel.AUTO_NAME = Auto
+simplotpanel.LEFT_NAME = Left
+simplotpanel.RIGHT_NAME = Right
+simplotpanel.CUSTOM = Custom
+SimulationPlotPanel.error.noPlotSelected = Please add one or more variables to plot on the Y-axis.
+SimulationPlotPanel.error.noPlotSelected.title = Nothing to plot
+
+
+! Component add buttons
+compaddbuttons.Bodycompandfinsets = Body components and fin sets
+compaddbuttons.Nosecone = Nose cone
+compaddbuttons.Bodytube = Body tube
+compaddbuttons.Transition = Transition
+compaddbuttons.Trapezoidal = Trapezoidal
+compaddbuttons.Elliptical = Elliptical
+compaddbuttons.Freeform = Freeform
+compaddbuttons.Launchlug = Launch lug
+compaddbuttons.Innercomponent = Inner component
+compaddbuttons.Innertube = Inner tube
+compaddbuttons.Coupler = Coupler
+compaddbuttons.Centeringring = Centering\nring
+compaddbuttons.Bulkhead = Bulkhead
+compaddbuttons.Engineblock = Engine\nblock
+compaddbuttons.Massobjects = Mass objects
+compaddbuttons.Parachute = Parachute
+compaddbuttons.Streamer = Streamer
+compaddbuttons.Shockcord = Shock cord
+compaddbuttons.Masscomponent = Mass\ncomponent
+compaddbuttons.Donotaskmeagain = Do not ask me again
+compaddbuttons.Selectcomppos = Select component position
+compaddbuttons.lbl.Youcanchange = You can change the default operation in the preferences.
+compaddbuttons.lbl.insertcomp = Insert the component after the current component or as the last component?
+compaddbuttons.askPosition.Inserthere = Insert here
+compaddbuttons.askPosition.Addtotheend = Add to the end
+compaddbuttons.askPosition.Cancel = Cancel
+
+! Component Analysis Dialog
+componentanalysisdlg.componentanalysis = Component analysis
+componentanalysisdlg.lbl.winddir = Wind direction:
+componentanalysisdlg.TitledBorder.warnings = Warnings:
+componentanalysisdlg.ToggleBut.worst = Worst
+componentanalysisdlg.lbl.angleofattack = Angle of attack:
+componentanalysisdlg.lbl.machnumber = Mach number:
+componentanalysisdlg.lbl.rollrate = Roll rate:
+componentanalysisdlg.lbl.activestages = Active stages:
+componentanalysisdlg.lbl.motorconf = Motor configuration:
+componentanalysisdlg.TabStability.Col = Component
+componentanalysisdlg.TabStability = Stability
+componentanalysisdlg.TabStability.ttip = Stability information
+componentanalysisdlg.dragTableModel.Col.Component = Component
+componentanalysisdlg.dragTableModel.Col.Pressure = <html>Pressure C<sub>D</sub>
+componentanalysisdlg.dragTableModel.Col.Base = <html>Base C<sub>D</sub>
+componentanalysisdlg.dragTableModel.Col.friction = <html>Friction C<sub>D</sub>
+componentanalysisdlg.dragTableModel.Col.total = <html>Total C<sub>D</sub>
+componentanalysisdlg.dragTabchar = Drag characteristics
+componentanalysisdlg.dragTabchar.ttip = Drag characteristics
+componentanalysisdlg.rollTableModel.Col.component = Component
+componentanalysisdlg.rollTableModel.Col.rollforc = Roll forcing coefficient
+componentanalysisdlg.rollTableModel.Col.rolldamp = Roll damping coefficient
+componentanalysisdlg.rollTableModel.Col.total = <html>Total C<sub>l</sub>
+componentanalysisdlg.rollTableModel = Roll dynamics
+componentanalysisdlg.rollTableModel.ttip = Roll dynamics
+componentanalysisdlg.println.closingmethod = Closing method called:
+componentanalysisdlg.println.settingnam = SETTING NAN VALUES
+componentanalysisdlg.lbl.reflenght = Reference length:
+componentanalysisdlg.lbl.refarea = Reference area:
+!componentanalysisdlg.But.close =Close
+componentanalysisdlg.TabStability.Col.Component = Component
+
+! Custom Material dialog
+custmatdlg.title.Custommaterial = Custom material
+custmatdlg.lbl.Materialname = Material name:
+custmatdlg.lbl.Materialtype = Material type:
+custmatdlg.lbl.Materialdensity = Material density:
+custmatdlg.checkbox.Addmaterial = Add material to database
+
+
+! Ring Component Config
+ringcompcfg.OuterRadius = OuterRadius
+ringcompcfg.Automatic = Automatic
+ringcompcfg.InnerRadius = InnerRadius
+ringcompcfg.Thickness = Thickness
+ringcompcfg.Length = Length
+ringcompcfg.Positionrelativeto = Position relative to:
+ringcompcfg.plus = plus
+ringcompcfg.PositionValue = PositionValue
+ringcompcfg.Radialdistance = Radial distance:
+ringcompcfg.Distancefrom = Distance from the rocket centerline
+ringcompcfg.Radialdirection = Radial direction:
+ringcompcfg.radialdirectionfrom = The radial direction from the rocket centerline
+ringcompcfg.but.Reset = Reset
+ringcompcfg.but.Resetcomponant = Reset the component to the rocket centerline
+ringcompcfg.EngineBlock.desc = <html>An <b>engine block</b> stops the motor from moving forwards in the motor mount tube.<br><br>In order to add a motor, create a <b>body tube</b> or <b>inner tube</b> and mark it as a motor mount in the <em>Motor</em> tab.
+ringcompcfg.note.desc = Note: An inner tube will not affect the aerodynamics of the rocket even if it is located outside of the body tube.
+
+
+! Body Tube Config
+BodyTubecfg.lbl.Bodytubelength = Body tube length:
+BodyTubecfg.lbl.Outerdiameter = Outer diameter:
+BodyTubecfg.lbl.Innerdiameter = Inner diameter:
+BodyTubecfg.lbl.Wallthickness = Wall thickness:
+BodyTubecfg.tab.General = General
+BodyTubecfg.tab.Generalproperties = General properties
+BodyTubecfg.tab.Motor = Motor
+BodyTubecfg.tab.Motormountconf = Motor mount configuration
+BodyTubecfg.checkbox.Automatic = Automatic
+BodyTubecfg.checkbox.Filled = Filled
+
+! FinSetConfig
+FinSetConfig.tab.Fintabs = Fin tabs
+FinSetConfig.tab.Through-the-wall = Through-the-wall fin tabs
+FinSetConfig.but.Converttofreeform = Convert to freeform
+FinSetConfig.but.Converttofreeform.ttip = Convert this fin set into a freeform fin set
+FinSetConfig.Convertfinset = Convert fin set
+FinSetConfig.but.Splitfins = Split fins
+FinSetConfig.but.Splitfins.ttip = Split the fin set into separate fins
+FinSetConfig.but.AutoCalc = Calculate automatically
+FinSetConfig.lbl.Through-the-wall = Through-the-wall fin tabs:
+FinSetConfig.lbl.Tablength = Tab length:
+FinSetConfig.ttip.Tablength = The length of the fin tab.
+FinSetConfig.lbl.Tabheight = Tab height:
+FinSetConfig.ttip.Tabheight = The spanwise height of the fin tab.
+FinSetConfig.lbl.Tabposition = Tab position:
+FinSetConfig.ttip.Tabposition = The position of the fin tab.
+FinSetConfig.lbl.relativeto = relative to
+
+!FinMarkingGuide
+FinMarkingGuide.lbl.Front = Front
+
+! MotorDatabaseLoadingDialog
+MotorDbLoadDlg.title = Loading motors
+MotorDbLoadDlg.Loadingmotors = Loading motors...
+
+! RocketConfig
+RocketCfg.lbl.Designname = Design name:
+RocketCfg.lbl.Designer = Designer:
+RocketCfg.lbl.Comments = Comments:
+RocketCfg.lbl.Revisionhistory = Revision history:
+RocketCfg.lbl.Material = Material:
+
+! ShockCordConfig
+ShockCordCfg.lbl.Shockcordlength = Shock cord length:
+
+! RocketComponentConfig
+RocketCompCfg.lbl.Componentname = Component name:
+RocketCompCfg.ttip.Thecomponentname = The component name.
+RocketCompCfg.tab.Override = Override
+RocketCompCfg.tab.MassandCGoverride = Mass and CG override options
+RocketCompCfg.tab.Figure = Figure
+RocketCompCfg.tab.Figstyleopt = Figure style options
+RocketCompCfg.tab.Comment = Comment
+RocketCompCfg.tab.Specifyacomment = Specify a comment for the component
+RocketCompCfg.lbl.Mass = Mass:
+RocketCompCfg.lbl.Componentmass = Component mass:
+RocketCompCfg.lbl.overriddento = (overridden to
+RocketCompCfg.lbl.overriddenby = (overridden by
+RocketCompCfg.lbl.Componentmaterial = Component material:
+RocketCompCfg.lbl.Componentfinish = Component finish:
+RocketCompCfg.lbl.ttip.componentmaterialaffects = The component material affects the weight of the component.
+RocketCompCfg.combo.ttip.componentmaterialaffects = The component material affects the weight of the component.
+RocketCompCfg.lbl.longA1 = <html>The component finish affects the aerodynamic drag of the component.<br>
+RocketCompCfg.lbl.longA2 = The value indicated is the average roughness height of the surface.
+RocketCompCfg.but.Setforall = Set for all
+RocketCompCfg.but.ttip.Setforall = Set this finish for all components of the rocket.
+RocketCompCfg.lbl.Overridemassorcenter = Override the mass or center of gravity of the
+RocketCompCfg.checkbox.Overridemass = Override mass:
+RocketCompCfg.checkbox.Overridecenterofgrav = Override center of gravity:
+RocketCompCfg.checkbox.OverridemassandCG = Override mass and CG of all subcomponents
+RocketCompCfg.lbl.longB1 = <html>The overridden mass does not include motors.<br>
+RocketCompCfg.lbl.longB2 = The center of gravity is measured from the front end of the
+RocketCompCfg.lbl.Commentsonthe = Comments on the
+RocketCompCfg.lbl.Figurestyle = Figure style:
+RocketCompCfg.lbl.Componentcolor = Component color:
+RocketCompCfg.lbl.Choosecolor = Choose color
+RocketCompCfg.checkbox.Usedefaultcolor = Use default color
+RocketCompCfg.lbl.Complinestyle = Component line style:
+RocketCompCfg.but.Saveasdefstyle = Save as default style
+RocketCompCfg.lbl.Diameter = Diameter:
+RocketCompCfg.lbl.Length = Length:
+RocketCompCfg.lbl.Thickness = Thickness:
+RocketCompCfg.checkbox.Endcapped = End capped
+RocketCompCfg.ttip.Endcapped = Whether the end of the shoulder is capped.
+RocketCompCfg.title.Noseconeshoulder = Nose cone shoulder
+RocketCompCfg.title.Aftshoulder = Aft shoulder
+RocketCompCfg.border.Foreshoulder = Fore shoulder
+!RocketCompCfg.lbl.Length = Length:
+
+! BulkheadConfig
+BulkheadCfg.tab.Diameter = Diameter:
+BulkheadCfg.tab.Thickness = Thickness:
+BulkheadCfg.tab.General = General
+BulkheadCfg.tab.Generalproperties = General properties
+
+!CenteringRingConfig
+CenteringRingCfg.tab.Outerdiam = Outer diameter:
+CenteringRingCfg.tab.Innerdiam = Inner diameter:
+CenteringRingCfg.tab.Thickness = Thickness:
+CenteringRingCfg.tab.General = General
+CenteringRingCfg.tab.Generalproperties = General properties
+
+!ComponentConfigDialog
+ComponentCfgDlg.configuration = configuration
+ComponentCfgDlg.configuration1 =
+ComponentCfgDlg.Modify = Modify
+
+!EllipticalFinSetConfig
+EllipticalFinSetCfg.Nbroffins = Number of fins:
+EllipticalFinSetCfg.Rotation = Rotation:
+EllipticalFinSetCfg.Fincant = Fin cant:
+EllipticalFinSetCfg.Rootchord = Root chord:
+EllipticalFinSetCfg.Height = Height:
+EllipticalFinSetCfg.Positionrelativeto = Position relative to:
+EllipticalFinSetCfg.plus = plus
+EllipticalFinSetCfg.FincrossSection = Fin cross section:
+EllipticalFinSetCfg.Thickness = Thickness:
+EllipticalFinSetCfg.General = General
+EllipticalFinSetCfg.Generalproperties = General properties
+EllipticalFinSetCfg.ttip.Fincant = The angle that the fins are canted with respect to the rocket body.
+
+!FreeformFinSetConfig
+FreeformFinSetCfg.tab.General = General
+FreeformFinSetCfg.tab.ttip.General = General properties
+FreeformFinSetCfg.tab.Shape = Shape
+FreeformFinSetCfg.tab.ttip.Finshape = Fin shape
+FreeformFinSetCfg.lbl.Numberoffins = Number of fins:
+FreeformFinSetCfg.lbl.Finrotation = Fin rotation:
+FreeformFinSetCfg.lbl.Fincant = Fin cant:
+FreeformFinSetCfg.lbl.ttip.Fincant = The angle that the fins are canted with respect to the rocket body.
+FreeformFinSetCfg.lbl.Posrelativeto = Position relative to:
+FreeformFinSetCfg.lbl.plus = plus
+FreeformFinSetCfg.lbl.FincrossSection = Fin cross section:
+FreeformFinSetCfg.lbl.Thickness = Thickness:
+! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle
+FreeformFinSetConfig.lbl.doubleClick1 = Double-click
+FreeformFinSetConfig.lbl.doubleClick2 = to edit
+FreeformFinSetConfig.lbl.clickDrag = Click+drag: Add and move points
+FreeformFinSetConfig.lbl.ctrlClick = Ctrl+click: Remove point
+
+
+!InnerTubeConfig
+InnerTubeCfg.tab.Motor = Motor
+InnerTubeCfg.tab.ttip.Motor = Motor mount configuration
+InnerTubeCfg.tab.Cluster = Cluster
+InnerTubeCfg.tab.ttip.Cluster = Cluster configuration
+InnerTubeCfg.tab.Radialpos = Radial position
+InnerTubeCfg.tab.ttip.Radialpos = Radial position
+InnerTubeCfg.lbl.Selectclustercfg = Select cluster configuration:
+InnerTubeCfg.lbl.TubeSep = Tube separation:
+InnerTubeCfg.lbl.ttip.TubeSep = The separation of the tubes, 1.0 = touching each other
+InnerTubeCfg.lbl.Rotation = Rotation:
+InnerTubeCfg.lbl.ttip.Rotation = Rotation angle of the cluster configuration
+InnerTubeCfg.lbl.Rotangle = Rotation angle of the cluster configuration
+InnerTubeCfg.but.Splitcluster = Split cluster
+InnerTubeCfg.lbl.longA1 = <html>Split the cluster into separate components.<br>
+InnerTubeCfg.lbl.longA2 = This also duplicates all components attached to this inner tube.
+InnerTubeCfg.but.Resetsettings = Reset settings
+InnerTubeCfg.but.ttip.Resetsettings = Reset the separation and rotation to the default values
+
+! LaunchLugConfig
+LaunchLugCfg.lbl.Length = Length:
+LaunchLugCfg.lbl.Outerdiam = Outer diameter:
+LaunchLugCfg.lbl.Innerdiam = Inner diameter:
+LaunchLugCfg.lbl.Thickness = Thickness:
+LaunchLugCfg.lbl.Radialpos = Radial position:
+LaunchLugCfg.lbl.Posrelativeto = Position relative to:
+LaunchLugCfg.lbl.plus = plus
+LaunchLugCfg.tab.General = General
+LaunchLugCfg.tab.Generalprop = General properties
+
+! MassComponentConfig
+MassComponentCfg.lbl.Mass = Mass:
+MassComponentCfg.lbl.Length = Length:
+MassComponentCfg.lbl.Diameter = Diameter:
+MassComponentCfg.lbl.PosRelativeto = Position relative to:
+MassComponentCfg.lbl.plus = plus
+MassComponentCfg.tab.General = General
+MassComponentCfg.tab.ttip.General = General properties
+MassComponentCfg.tab.Radialpos = Radial position
+MassComponentCfg.tab.ttip.Radialpos = Radial position configuration
+MassComponentCfg.lbl.Radialdistance = Radial distance:
+MassComponentCfg.lbl.Radialdirection = Radial direction:
+MassComponentCfg.but.Reset = Reset
+
+! MotorConfig
+MotorCfg.checkbox.compmotormount = This component is a motor mount
+MotorCfg.lbl.Motorcfg = Motor configuration:
+MotorCfg.but.New = New
+MotorCfg.lbl.Currentmotor = Current motor:
+MotorCfg.lbl.Motoroverhang = Motor overhang:
+MotorCfg.lbl.Ignitionat = Ignition at:
+MotorCfg.lbl.plus = plus
+MotorCfg.lbl.seconds = seconds
+MotorCfg.lbl.longA1 = The current design has only one stage.
+MotorCfg.lbl.longA2 = Stages can be added by clicking \"New stage\".
+MotorCfg.lbl.longB1 = The current design has
+MotorCfg.lbl.longB2 = stages.
+MotorCfg.but.Selectmotor = Select motor
+MotorCfg.but.Removemotor = Remove motor
+MotorCfg.lbl.motorLabel = None
+
+! NoseConeConfig
+NoseConeCfg.lbl.Noseconeshape = Nose cone shape:
+NoseConeCfg.lbl.Shapeparam = Shape parameter:
+NoseConeCfg.lbl.Noseconelength = Nose cone length:
+NoseConeCfg.lbl.Basediam = Base diameter:
+NoseConeCfg.checkbox.Automatic = Automatic
+NoseConeCfg.lbl.Wallthickness = Wall thickness:
+NoseConeCfg.checkbox.Filled = Filled
+NoseConeCfg.tab.General = General
+NoseConeCfg.tab.ttip.General = General properties
+NoseConeCfg.tab.Shoulder = Shoulder
+NoseConeCfg.tab.ttip.Shoulder = Shoulder properties
+
+! ParachuteConfig
+ParachuteCfg.lbl.Canopy = Canopy:
+ParachuteCfg.lbl.Diameter = Diameter:
+ParachuteCfg.lbl.Material = Material:
+ParachuteCfg.combo.MaterialModel = The component material affects the weight of the component.
+ParachuteCfg.lbl.longA1 = <html>Drag coefficient C<sub>D</sub>:
+ParachuteCfg.lbl.longB1 = <html>The drag coefficient relative to the total area of the parachute.<br>
+ParachuteCfg.lbl.longB2 = A larger drag coefficient yields a slowed descent rate.
+ParachuteCfg.lbl.longB3 = A typical value for parachutes is 0.8.
+ParachuteCfg.but.Reset = Reset
+ParachuteCfg.lbl.Shroudlines = Shroud lines:
+ParachuteCfg.lbl.Numberoflines = Number of lines:
+ParachuteCfg.lbl.Linelength = Line length:
+ParachuteCfg.lbl.Material = Material:
+ParachuteCfg.lbl.Posrelativeto = Position relative to:
+ParachuteCfg.lbl.plus = plus
+ParachuteCfg.lbl.Packedlength = Packed length:
+ParachuteCfg.lbl.Packeddiam = Packed diameter:
+ParachuteCfg.lbl.Deploysat = Deploys at:
+ParachuteCfg.lbl.seconds = seconds
+ParachuteCfg.lbl.Altitude = Altitude:
+ParachuteCfg.tab.General = General
+ParachuteCfg.tab.ttip.General = General properties
+ParachuteCfg.tab.Radialpos = Radial position
+ParachuteCfg.tab.ttip.Radialpos = Radial position configuration
+ParachuteCfg.lbl.Radialdistance = Radial distance:
+ParachuteCfg.lbl.Radialdirection = Radial direction:
+ParachuteCfg.but.Reset = Reset
+ParachuteCfg.lbl.plusdelay = plus
+
+! ShockCordConfig
+ShockCordCfg.lbl.Shockcordlength = Shock cord length:
+ShockCordCfg.lbl.Shockcordmaterial = Shock cord material:
+ShockCordCfg.lbl.Posrelativeto = Position relative to:
+ShockCordCfg.lbl.plus = plus
+ShockCordCfg.lbl.Packedlength = Packed length:
+ShockCordCfg.lbl.Packeddiam = Packed diameter:
+ShockCordCfg.tab.General = General
+ShockCordCfg.tab.ttip.General = General properties
+
+!SleeveConfig
+SleeveCfg.tab.Outerdiam = Outer diameter:
+SleeveCfg.tab.Innerdiam = Inner diameter:
+SleeveCfg.tab.Wallthickness = Wall thickness:
+SleeveCfg.tab.Length = Length:
+SleeveCfg.tab.General = General
+SleeveCfg.tab.Generalproperties = General properties
+
+! StreamerConfig
+StreamerCfg.lbl.Striplength = Strip length:
+StreamerCfg.lbl.Stripwidth = Strip width:
+StreamerCfg.lbl.Striparea = Strip area:
+StreamerCfg.lbl.Aspectratio = Aspect ratio:
+StreamerCfg.lbl.Material = Material:
+StreamerCfg.combo.ttip.MaterialModel = The component material affects the weight of the component.
+StreamerCfg.lbl.longA1 = <html>Drag coefficient C<sub>D</sub>:
+StreamerCfg.lbl.longB1 = <html>The drag coefficient relative to the total area of the streamer.<br>
+StreamerCfg.lbl.longB2 = A larger drag coefficient yields a slowed descent rate.
+StreamerCfg.lbl.Automatic = Automatic
+StreamerCfg.lbl.longC1 = The drag coefficient is relative to the area of the streamer.
+StreamerCfg.lbl.Posrelativeto = Position relative to:
+StreamerCfg.lbl.plus = plus
+StreamerCfg.lbl.Packedlength = Packed length:
+StreamerCfg.lbl.Packeddiam = Packed diameter:
+StreamerCfg.lbl.Deploysat = Deploys at:
+StreamerCfg.lbl.seconds = seconds
+StreamerCfg.lbl.Altitude = Altitude:
+StreamerCfg.tab.General = General
+StreamerCfg.tab.ttip.General = General properties
+StreamerCfg.tab.Radialpos = Radial position
+StreamerCfg.tab.ttip.Radialpos = Radial position configuration
+StreamerCfg.lbl.Radialdistance = Radial distance:
+StreamerCfg.lbl.Radialdirection = Radial direction:
+StreamerCfg.but.Reset = Reset
+StreamerCfg.lbl.plusdelay = plus
+
+! ThicknessRingComponentConfig
+ThicknessRingCompCfg.tab.Outerdiam = Outer diameter:
+ThicknessRingCompCfg.tab.Innerdiam = Inner diameter:
+ThicknessRingCompCfg.tab.Wallthickness = Wall thickness:
+ThicknessRingCompCfg.tab.Length = Length:
+ThicknessRingCompCfg.tab.General = General
+ThicknessRingCompCfg.tab.Generalprop = General properties
+
+! TransitionConfig
+TransitionCfg.lbl.Transitionshape = Transition shape:
+TransitionCfg.checkbox.Clipped = Clipped
+TransitionCfg.lbl.Shapeparam = Shape parameter:
+TransitionCfg.lbl.Transitionlength = Transition length:
+TransitionCfg.lbl.Forediam = Fore diameter:
+TransitionCfg.checkbox.Automatic = Automatic
+TransitionCfg.lbl.Aftdiam = Aft diameter:
+TransitionCfg.lbl.Wallthickness = Wall thickness:
+TransitionCfg.checkbox.Filled = Filled
+TransitionCfg.tab.General = General
+TransitionCfg.tab.Generalproperties = General properties
+TransitionCfg.tab.Shoulder = Shoulder
+TransitionCfg.tab.Shoulderproperties = Shoulder properties
+
+! TrapezoidFinSetConfig
+TrapezoidFinSetCfg.lbl.Nbroffins = Number of fins:
+TrapezoidFinSetCfg.lbl.ttip.Nbroffins = The number of fins in the fin set.
+TrapezoidFinSetCfg.lbl.Finrotation = Fin rotation:
+TrapezoidFinSetCfg.lbl.ttip.Finrotation = The angle of the first fin in the fin set.
+TrapezoidFinSetCfg.lbl.Fincant = Fin cant:
+TrapezoidFinSetCfg.lbl.ttip.Fincant =The angle that the fins are canted with respect to the rocket body.
+TrapezoidFinSetCfg.lbl.Rootchord = Root chord:
+TrapezoidFinSetCfg.lbl.Tipchord = Tip chord:
+TrapezoidFinSetCfg.lbl.Height = Height:
+TrapezoidFinSetCfg.lbl.Sweeplength = Sweep length:
+TrapezoidFinSetCfg.lbl.Sweepangle = Sweep angle:
+TrapezoidFinSetCfg.lbl.FincrossSection = Fin cross section:
+TrapezoidFinSetCfg.lbl.Thickness = Thickness:
+TrapezoidFinSetCfg.lbl.Posrelativeto = Position relative to:
+TrapezoidFinSetCfg.lbl.plus = plus
+TrapezoidFinSetCfg.tab.General = General
+TrapezoidFinSetCfg.tab.Generalproperties = General properties
+
+!MotorConfigurationModel
+MotorCfgModel.Editcfg = Edit configurations
+
+! StorageOptionChooser
+StorageOptChooser.lbl.Simdatatostore = Simulated data to store:
+StorageOptChooser.rdbut.Allsimdata = All simulated data
+StorageOptChooser.lbl.longA1 = <html>Store all simulated data.<br>
+StorageOptChooser.lbl.longA2 = This can result in very large files!
+StorageOptChooser.rdbut.Every = Every
+StorageOptChooser.lbl.longB1 = <html>Store plottable values approximately this far apart.<br>
+StorageOptChooser.lbl.longB2 = Larger values result in smaller files.
+StorageOptChooser.lbl.seconds = seconds
+StorageOptChooser.rdbut.Onlyprimfig = Only primary figures
+StorageOptChooser.lbl.longC1 = <html>Store only the values shown in the summary table.<br>
+StorageOptChooser.lbl.longC2 = This results in the smallest files.
+StorageOptChooser.checkbox.Compfile = Compress file
+StorageOptChooser.lbl.UsingComp = Using compression reduces the file size significantly.
+StorageOptChooser.lbl.longD1 = An estimate on how large the resulting file would be with the present options.
+StorageOptChooser.ttip.Saveopt = Save options
+StorageOptChooser.lbl.Estfilesize = Estimated file size:
+StorageOptChooser.lbl.Saveopt = Save options
+
+! ThrustCurveMotorSelectionPanel
+TCMotorSelPan.lbl.Selrocketmotor = Select rocket motor:
+TCMotorSelPan.checkbox.hideSimilar = Hide very similar thrust curves
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Show all motors
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Show motors with diameter less than that of the motor mount
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Show motors with diameter equal to that of the motor mount
+TCMotorSelPan.lbl.Motormountdia = Motor mount diameter:
+TCMotorSelPan.lbl.Search = Search:
+TCMotorSelPan.lbl.Selectthrustcurve = Select thrust curve:
+TCMotorSelPan.lbl.Ejectionchargedelay = Ejection charge delay:
+TCMotorSelPan.equalsIgnoreCase.None = None
+TCMotorSelPan.lbl.NumberofsecondsorNone = (Number of seconds or \"None\")
+TCMotorSelPan.lbl.Totalimpulse = Total impulse:
+TCMotorSelPan.lbl.Avgthrust = Avg. thrust:
+TCMotorSelPan.lbl.Maxthrust = Max. thrust:
+TCMotorSelPan.lbl.Burntime = Burn time:
+TCMotorSelPan.lbl.Launchmass = Launch mass:
+TCMotorSelPan.lbl.Emptymass = Empty mass:
+TCMotorSelPan.lbl.Datapoints = Data points:
+TCMotorSelPan.lbl.Digest = Digest:
+TCMotorSelPan.title.Thrustcurve = Thrust curve:
+TCMotorSelPan.title.Thrust = Thrust
+TCMotorSelPan.delayBox.None = None
+
+
+! PlotDialog
+PlotDialog.title.Flightdataplot = Flight data plot
+PlotDialog.Chart.Simulatedflight = Simulated flight
+PlotDialog.CheckBox.Showdatapoints = Show data points
+PlotDialog.lbl.Chart = Click and drag down+right to zoom in, up+left to zoom out
+
+
+! "main" prefix is used for the main application dialog
+
+# FIXME: Rename the description keys
+
+main.menu.file = File
+main.menu.file.desc = File-handling related tasks
+main.menu.file.new = New
+main.menu.file.new.desc = Create a new rocket design
+main.menu.file.open = Open...
+BasicFrame.item.Openrocketdesign = Open a rocket design
+main.menu.file.openExample = Open example...
+BasicFrame.item.Openexamplerocketdesign = Open an example rocket design
+main.menu.file.save = Save
+BasicFrame.item.SavecurRocketdesign = Save the current rocket design
+main.menu.file.saveAs = Save as...
+BasicFrame.item.SavecurRocketdesnewfile = Save the current rocket design to a new file
+main.menu.file.print = Print / Export PDF...
+main.menu.file.print.desc = Print or save as PDF the parts list and fin templates
+main.menu.file.close = Close
+BasicFrame.item.Closedesign = Close the current rocket design
+main.menu.file.quit = Quit
+BasicFrame.item.Quitprogram = Quit the program
+
+main.menu.edit = Edit
+BasicFrame.menu.Rocketedt = Rocket editing
+main.menu.edit.undo = Undo
+main.menu.edit.undo.desc = Undo the previous operation
+main.menu.edit.redo = Redo
+main.menu.edit.redo.desc = Redo the previously undone operation
+main.menu.edit.cut = Cut
+main.menu.edit.copy = Copy
+main.menu.edit.paste = Paste
+main.menu.edit.delete = Delete
+main.menu.edit.resize = Scale...
+main.menu.edit.resize.desc = Scale parts of the rocket design
+main.menu.edit.preferences = Preferences
+main.menu.edit.preferences.desc = Setup the application preferences
+
+main.menu.analyze = Analyze
+main.menu.analyze.desc = Rocket analysis
+main.menu.analyze.componentAnalysis = Component analysis
+main.menu.analyze.componentAnalysis.desc = Analyze the rocket components separately
+main.menu.analyze.optimization = Rocket optimization
+main.menu.analyze.optimization.desc = General rocket design optimization
+
+main.menu.help = Help
+main.menu.help.desc = Information about OpenRocket
+main.menu.help.tours = Guided tours
+main.menu.help.tours.desc = Take guided tours on OpenRocket
+main.menu.help.license = License
+main.menu.help.license.desc = OpenRocket license information
+main.menu.help.bugReport = Bug report
+main.menu.help.bugReport.desc = Information about reporting bugs in OpenRocket
+main.menu.help.debugLog = Debug log
+main.menu.help.debugLog.desc = View the OpenRocket debug log
+main.menu.help.about = About
+main.menu.help.about.desc = Copyright details about OpenRocket
+
+main.menu.debug = Debug
+main.menu.debug.whatisthismenu = What is this menu?
+main.menu.debug.createtestrocket = Create test rocket
+
+! database
+! Translate here all material database
+!
+
+! Material database
+! BULK_MATERIAL
+Databases.materials.Acrylic = Acrylic
+Databases.materials.Balsa = Balsa
+Databases.materials.Basswood = Basswood
+Databases.materials.Birch = Birch
+Databases.materials.Cardboard = Cardboard
+Databases.materials.Carbonfiber = Carbon fiber
+Databases.materials.Cork = Cork
+Databases.materials.DepronXPS = Depron (XPS)
+Databases.materials.Fiberglass = Fiberglass
+Databases.materials.Kraftphenolic = Kraft phenolic
+Databases.materials.Maple = Maple
+Databases.materials.Paperoffice = Paper (office)
+Databases.materials.Pine = Pine
+Databases.materials.Plywoodbirch = Plywood (birch)
+Databases.materials.PolycarbonateLexan = Polycarbonate (Lexan)
+Databases.materials.Polystyrene = Polystyrene
+Databases.materials.PVC = PVC
+Databases.materials.Spruce = Spruce
+Databases.materials.StyrofoamgenericEPS = Styrofoam (generic EPS)
+Databases.materials.StyrofoamBluefoamXPS = Styrofoam \"Blue foam\" (XPS)
+Databases.materials.Quantumtubing = Quantum tubing
+Databases.materials.BlueTube = Blue tube
+!SURFACE_MATERIAL
+Databases.materials.Ripstopnylon = Ripstop nylon
+Databases.materials.Mylar = Mylar
+Databases.materials.Polyethylenethin = Polyethylene (thin)
+Databases.materials.Polyethyleneheavy = Polyethylene (heavy)
+Databases.materials.Silk = Silk
+Databases.materials.Paperoffice = Paper (office)
+Databases.materials.Cellophane = Cellophane
+Databases.materials.Crepepaper = Cr\u00eape paper
+! LINE_MATERIAL
+Databases.materials.Threadheavy-duty = Thread (heavy-duty)
+Databases.materials.Elasticcordround2mm = Elastic cord (round 2mm, 1/16 in)
+Databases.materials.Elasticcordflat6mm = Elastic cord (flat 6mm, 1/4 in)
+Databases.materials.Elasticcordflat12mm = Elastic cord (flat 12mm, 1/2 in)
+Databases.materials.Elasticcordflat19mm = Elastic cord (flat 19mm, 3/4 in)
+Databases.materials.Elasticcordflat25mm = Elastic cord (flat 25mm, 1 in)
+Databases.materials.Braidednylon2mm = Braided nylon (2 mm, 1/16 in)
+Databases.materials.Braidednylon3mm = Braided nylon (3 mm, 1/8 in)
+Databases.materials.Tubularnylon11mm = Tubular nylon (11 mm, 7/16 in)
+Databases.materials.Tubularnylon14mm = Tubular nylon (14 mm, 9/16 in)
+Databases.materials.Tubularnylon25mm = Tubular nylon (25 mm, 1 in)
+
+! ExternalComponent
+ExternalComponent.Rough = Rough
+ExternalComponent.Unfinished = Unfinished
+ExternalComponent.Regularpaint = Regular paint
+ExternalComponent.Smoothpaint = Smooth paint
+ExternalComponent.Polished = Polished
+
+! LineStyle
+LineStyle.Solid = Solid
+LineStyle.Dashed = Dashed
+LineStyle.Dotted = Dotted
+LineStyle.Dash-dotted = Dash-dotted
+LineStyle.Defaultstyle = Default style
+
+! Shape
+Shape.Conical = Conical
+Shape.Conical.desc1 = A conical nose cone has a profile of a triangle.
+Shape.Conical.desc2 = A conical transition has straight sides.
+Shape.Ogive = Ogive
+Shape.Ogive.desc1 = An ogive nose cone has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube, values less than 1 produce <b>secant ogives</b>.
+Shape.Ogive.desc2 = An ogive transition has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube at the aft end, values less than 1 produce <b>secant ogives</b>.
+Shape.Ellipsoid = Ellipsoid
+Shape.Ellipsoid.desc1 = An ellipsoidal nose cone has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>.
+Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>. If the transition is not clipped, then the profile is extended at the center by the corresponding radius.
+Shape.Powerseries = Power series
+Shape.Powerseries.desc1 = A power series nose cone has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 this is a <b>\u00BD-power</b> or <b>parabolic</b> nose cone, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 a <b>conical</b> nose cone.
+Shape.Powerseries.desc2 = A power series transition has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 the transition is <b>\u00BD-power</b> or <b>parabolic</b>, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 <b>conical</b>.
+Shape.Parabolicseries = Parabolic series
+Shape.Parabolicseries.desc1 = A parabolic series nose cone has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> nose cone.
+Shape.Parabolicseries.desc2 = A parabolic series transition has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube at the aft end, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> transition.
+Shape.Haackseries = Haack series
+Shape.Haackseries.desc1 = The Haack series nose cones are designed to minimize drag. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> nose cone, which minimizes drag for fixed length and diameter, while a value of 0.333 produces an <b>LV-Haack</b> nose cone, which minimizes drag for fixed length and volume.
+Shape.Haackseries.desc2 = The Haack series <i>nose cones</i> are designed to minimize drag. These transition shapes are their equivalents, but do not necessarily produce optimal drag for transitions. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> shape, while a value of 0.333 produces an <b>LV-Haack</b> shape.
+
+
+! RocketComponent
+RocketComponent.Position.TOP = Top of the parent component
+RocketComponent.Position.MIDDLE = Middle of the parent component
+RocketComponent.Position.BOTTOM = Bottom of the parent component
+RocketComponent.Position.AFTER = After the parent component
+RocketComponent.Position.ABSOLUTE = Tip of the nose cone
+
+! LaunchLug
+LaunchLug.Launchlug = Launch lug
+! NoseCone
+NoseCone.NoseCone = Nose cone
+! Transition
+Transition.Transition = Transition
+!Stage
+Stage.Stage = Stage
+! BodyTube
+BodyTube.BodyTube = Body tube
+! TubeCoupler
+TubeCoupler.TubeCoupler = Tube coupler
+!InnerTube
+InnerTube.InnerTube = Inner Tube
+! TrapezoidFinSet
+TrapezoidFinSet.TrapezoidFinSet = Trapezoidal fin set
+! FreeformFinSet
+FreeformFinSet.FreeformFinSet = Freeform fin set
+!MassComponent
+MassComponent.MassComponent = Mass component
+! Parachute
+Parachute.Parachute = Parachute
+! ShockCord
+ShockCord.ShockCord = Shock cord
+! Bulkhead
+Bulkhead.Bulkhead = Bulkhead
+
+!Rocket
+Rocket.motorCount.Nomotor = [No motors]
+Rocket.compname.Rocket = Rocket
+
+!MotorMount
+MotorMount.IgnitionEvent.AUTOMATIC = Automatic (launch or ejection charge)
+MotorMount.IgnitionEvent.LAUNCH = Launch
+MotorMount.IgnitionEvent.EJECTION_CHARGE = First ejection charge of previous stage
+MotorMount.IgnitionEvent.BURNOUT = First burnout of previous stage
+MotorMount.IgnitionEvent.NEVER = Never
+
+!ComponentIcons
+ComponentIcons.Nosecone = Nose cone
+ComponentIcons.Bodytube = Body tube
+ComponentIcons.Transition = Transition
+ComponentIcons.Trapezoidalfinset = Trapezoidal fin set
+ComponentIcons.Ellipticalfinset = Elliptical fin set
+ComponentIcons.Freeformfinset = Freeform fin set
+ComponentIcons.Launchlug = Launch lug
+ComponentIcons.Innertube = Inner tube
+ComponentIcons.Tubecoupler = Tube coupler
+ComponentIcons.Centeringring = Centering ring
+ComponentIcons.Bulkhead = Bulk head
+ComponentIcons.Engineblock = Engine block
+ComponentIcons.Parachute = Parachute
+ComponentIcons.Streamer = Streamer
+ComponentIcons.Shockcord = Shock cord
+ComponentIcons.Masscomponent = Mass component
+ComponentIcons.disabled = (disabled)
+
+! StageAction
+StageAction.Stage = Stage
+
+! RecoveryDevice
+RecoveryDevice.DeployEvent.LAUNCH = Launch (plus NN seconds)
+RecoveryDevice.DeployEvent.EJECTION = First ejection charge of this stage
+RecoveryDevice.DeployEvent.APOGEE = Apogee
+RecoveryDevice.DeployEvent.ALTITUDE = Specific altitude during descent
+RecoveryDevice.DeployEvent.NEVER = Never
+
+! FlightEvent
+FlightEvent.Type.LAUNCH = Launch
+FlightEvent.Type.IGNITION = Motor ignition
+FlightEvent.Type.LIFTOFF = Lift-off
+FlightEvent.Type.LAUNCHROD = Launch rod clearance
+FlightEvent.Type.BURNOUT = Motor burnout
+FlightEvent.Type.EJECTION_CHARGE = Ejection charge
+FlightEvent.Type.STAGE_SEPARATION = Stage separation
+FlightEvent.Type.APOGEE = Apogee
+FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Recovery device deployment
+FlightEvent.Type.GROUND_HIT = Ground hit
+FlightEvent.Type.SIMULATION_END = Simulation end
+FlightEvent.Type.ALTITUDE = Altitude change
+
+! ThrustCurveMotorColumns
+TCurveMotorCol.MANUFACTURER = Manufacturer
+TCurveMotorCol.DESIGNATION = Designation
+TCurveMotorCol.TYPE = Type
+TCurveMotorCol.DIAMETER = Diameter
+TCurveMotorCol.LENGTH = Length
+
+! RocketInfo
+RocketInfo.lengthLine.Length = Length
+RocketInfo.lengthLine.maxdiameter = , max. diameter
+RocketInfo.massText1 = Mass with motors
+RocketInfo.massText2 = Mass with no motors
+RocketInfo.at = at M=
+RocketInfo.cgText = CG:
+RocketInfo.cpText = CP:
+RocketInfo.stabText = Stability:
+RocketInfo.Warning = Warning:
+RocketInfo.Calculating = Calculating...
+RocketInfo.Apogee = Apogee:
+RocketInfo.Maxvelocity = Max. velocity:
+RocketInfo.Maxacceleration = Max. acceleration:
+RocketInfo.apogeeValue = N/A
+RocketInfo.Mach = (Mach
+RocketInfo.velocityValue = N/A
+RocketInfo.accelerationValue = N/A
+
+! FinSet
+FinSet.CrossSection.SQUARE = Square
+FinSet.CrossSection.ROUNDED = Rounded
+FinSet.CrossSection.AIRFOIL = Airfoil
+FinSet.TabRelativePosition.FRONT = Root chord leading edge
+FinSet.TabRelativePosition.CENTER = Root chord midpoint
+FinSet.TabRelativePosition.END = Root chord trailing edge
+
+! FlightDataType
+FlightDataType.TYPE_TIME = Time
+FlightDataType.TYPE_ALTITUDE = Altitude
+FlightDataType.TYPE_VELOCITY_Z = Vertical velocity
+FlightDataType.TYPE_ACCELERATION_Z = Vertical acceleration
+FlightDataType.TYPE_VELOCITY_TOTAL = Total velocity
+FlightDataType.TYPE_ACCELERATION_TOTAL = Total acceleration
+FlightDataType.TYPE_POSITION_X = Position upwind
+FlightDataType.TYPE_POSITION_Y = Position parallel to wind
+FlightDataType.TYPE_POSITION_XY = Lateral distance
+FlightDataType.TYPE_POSITION_DIRECTION = Lateral direction
+FlightDataType.TYPE_VELOCITY_XY = Lateral velocity
+FlightDataType.TYPE_ACCELERATION_XY = Lateral acceleration
+FlightDataType.TYPE_AOA = Angle of attack
+FlightDataType.TYPE_ROLL_RATE = Roll rate
+FlightDataType.TYPE_PITCH_RATE = Pitch rate
+FlightDataType.TYPE_YAW_RATE = Yaw rate
+FlightDataType.TYPE_MASS = Mass
+FlightDataType.TYPE_LONGITUDINAL_INERTIA = Longitudinal moment of inertia
+FlightDataType.TYPE_ROTATIONAL_INERTIA = Rotational moment of inertia
+FlightDataType.TYPE_CP_LOCATION = CP location
+FlightDataType.TYPE_CG_LOCATION = CG location
+FlightDataType.TYPE_STABILITY = Stability margin calibers
+FlightDataType.TYPE_MACH_NUMBER = Mach number
+FlightDataType.TYPE_REYNOLDS_NUMBER = Reynolds number
+FlightDataType.TYPE_THRUST_FORCE = Thrust
+FlightDataType.TYPE_DRAG_FORCE = Drag force
+FlightDataType.TYPE_DRAG_COEFF = Drag coefficient
+FlightDataType.TYPE_AXIAL_DRAG_COEFF = Axial drag coefficient
+FlightDataType.TYPE_FRICTION_DRAG_COEFF = Friction drag coefficient
+FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Pressure drag coefficient
+FlightDataType.TYPE_BASE_DRAG_COEFF = Base drag coefficient
+FlightDataType.TYPE_NORMAL_FORCE_COEFF = Normal force coefficient
+FlightDataType.TYPE_PITCH_MOMENT_COEFF = Pitch moment coefficient
+FlightDataType.TYPE_YAW_MOMENT_COEFF = Yaw moment coefficient
+FlightDataType.TYPE_SIDE_FORCE_COEFF = Side force coefficient
+FlightDataType.TYPE_ROLL_MOMENT_COEFF = Roll moment coefficient
+FlightDataType.TYPE_ROLL_FORCING_COEFF = Roll forcing coefficient
+FlightDataType.TYPE_ROLL_DAMPING_COEFF = Roll damping coefficient
+FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Pitch damping coefficient
+FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Yaw damping coefficient
+FlightDataType.TYPE_REFERENCE_LENGTH = Reference lenght
+FlightDataType.TYPE_REFERENCE_AREA = Reference area
+FlightDataType.TYPE_ORIENTATION_THETA = Vertical orientation (zenith)
+FlightDataType.TYPE_ORIENTATION_PHI = Lateral orientation (azimuth)
+FlightDataType.TYPE_WIND_VELOCITY = Wind velocity
+FlightDataType.TYPE_AIR_TEMPERATURE = Air temperature
+FlightDataType.TYPE_AIR_PRESSURE = Air pressure
+FlightDataType.TYPE_SPEED_OF_SOUND = Speed of sound
+FlightDataType.TYPE_TIME_STEP = Simulation time step
+FlightDataType.TYPE_COMPUTATION_TIME = Computation time
+FlightDataType.TYPE_LATITUDE = Latitude
+FlightDataType.TYPE_LONGITUDE = Longitude
+FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration
+
+! PlotConfiguration
+PlotConfiguration.Verticalmotion = Vertical motion vs. time
+PlotConfiguration.Totalmotion = Total motion vs. time
+PlotConfiguration.Flightside = Flight side profile
+PlotConfiguration.Stability = Stability vs. time
+PlotConfiguration.Dragcoef = Drag coefficients vs. Mach number
+PlotConfiguration.Rollcharacteristics = Roll characteristics
+PlotConfiguration.Angleofattack = Angle of attack and orientation vs. time
+PlotConfiguration.Simulationtime = Simulation time step and computation time
+
+! Warning
+Warning.LargeAOA.str1 = Large angle of attack encountered.
+Warning.LargeAOA.str2 = Large angle of attack encountered (
+Warning.DISCONTINUITY = Discontinuity in rocket body diameter.
+Warning.THICK_FIN = Thick fins may not be modeled accurately.
+Warning.JAGGED_EDGED_FIN = Jagged-edged fin predictions may be inaccurate.
+Warning.LISTENERS_AFFECTED = Listeners modified the flight simulation
+Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Recovery device opened while motor still burning.
+Warning.FILE_INVALID_PARAMETER = Invalid parameter encountered, ignoring.
+
+
+! Scale dialog
+ScaleDialog.lbl.scaleRocket = Entire rocket
+ScaleDialog.lbl.scaleSubselection = Selection and all subcomponents
+ScaleDialog.lbl.scaleSelection = Only selected component
+ScaleDialog.title = Scale design
+ScaleDialog.lbl.scale = Scale:
+ScaleDialog.lbl.scale.ttip = Select whether to scale the entire design or only the selected component
+ScaleDialog.lbl.scaling = Scaling to apply:
+ScaleDialog.lbl.scaling.ttip = Resulting size, values above 100% grow and values below 100% shrink the design.
+! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"
+ScaleDialog.lbl.scaleFrom = Scale from
+ScaleDialog.lbl.scaleTo = to
+ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and resulting length.
+ScaleDialog.checkbox.scaleMass = Update explicit mass values
+ScaleDialog.checkbox.scaleMass.ttip = Scale mass component and override mass values by the cube of the scaling factor
+ScaleDialog.button.scale = Scale
+ScaleDialog.undo.scaleRocket = Scale rocket
+ScaleDialog.undo.scaleComponent = Scale component
+ScaleDialog.undo.scaleComponents = Scale components
+
+!icons
+Icons.Undo = Undo
+Icons.Redo = Redo
+
+OpenRocketPrintable.Partsdetail = Parts detail
+OpenRocketPrintable.Fintemplates = Fin templates
+OpenRocketPrintable.Transitiontemplates = Transition templates
+OpenRocketPrintable.Noseconetemplates = Nose Cone templates
+OpenRocketPrintable.Finmarkingguide = Fin marking guide
+OpenRocketPrintable.DesignReport = Design Report
+
+OpenRocketDocument.Redo = Redo
+OpenRocketDocument.Undo = Undo
+
+!EllipticalFinSet
+EllipticalFinSet.Ellipticalfinset = Elliptical fin set
+
+! Optimization
+
+! Modifiers
+
+optimization.modifier.nosecone.length = Length
+optimization.modifier.nosecone.length.desc = Optimize the nose cone length.
+optimization.modifier.nosecone.diameter = Diameter
+optimization.modifier.nosecone.diameter.desc = Optimize the nose cone base diameter.
+optimization.modifier.nosecone.thickness = Thickness
+optimization.modifier.nosecone.thickness.desc = Optimize the nose cone wall thickness.
+optimization.modifier.nosecone.shapeparameter = Shape parameter
+optimization.modifier.nosecone.shapeparameter.desc = Optimize the nose cone shape parameter.
+
+optimization.modifier.transition.length = Length
+optimization.modifier.transition.length.desc = Optimize the transition length.
+optimization.modifier.transition.forediameter = Fore diameter
+optimization.modifier.transition.forediameter.desc = Optimize the transition fore diameter.
+optimization.modifier.transition.aftdiameter = Aft diameter
+optimization.modifier.transition.aftdiameter.desc = Optimize the transition aft diameter.
+optimization.modifier.transition.thickness = Thickness
+optimization.modifier.transition.thickness.desc = Optimize the transition wall thickness.
+optimization.modifier.transition.shapeparameter = Shape parameter
+optimization.modifier.transition.shapeparameter.desc = Optimize the transition shape parameter.
+
+optimization.modifier.bodytube.length = Length
+optimization.modifier.bodytube.length.desc = Optimize the body tube length.
+optimization.modifier.bodytube.outerDiameter = Outer diameter
+optimization.modifier.bodytube.outerDiameter.desc = Optimize the body tube outer diameter while maintaining the wall thickness.
+optimization.modifier.bodytube.thickness = Thickness
+optimization.modifier.bodytube.thickness.desc = Optimize the body tube wall thickness.
+
+optimization.modifier.trapezoidfinset.rootChord = Root chord
+optimization.modifier.trapezoidfinset.rootChord.desc = Optimize the root chord length of the fin set (length of fin at the rocket body).
+optimization.modifier.trapezoidfinset.tipChord = Tip chord
+optimization.modifier.trapezoidfinset.tipChord.desc = Optimize the tip chord length of the fin set (length of fin at outer edge).
+optimization.modifier.trapezoidfinset.sweep = Sweep
+optimization.modifier.trapezoidfinset.sweep.desc = Optimize the sweep of the fin set (distance that the leading edge sweeps backwards).
+optimization.modifier.trapezoidfinset.height = Height
+optimization.modifier.trapezoidfinset.height.desc = Optimize the height (semi-span) of the fin set.
+
+optimization.modifier.ellipticalfinset.length = Root chord
+optimization.modifier.ellipticalfinset.length.desc = Optimize the root chord length of the fin set.
+optimization.modifier.ellipticalfinset.height = Height
+optimization.modifier.ellipticalfinset.height.desc = Optimize the height (semi-span) of the fin set.
+
+optimization.modifier.finset.cant = Cant angle
+optimization.modifier.finset.cant.desc = Optimize the cant angle of the fin set.
+optimization.modifier.finset.position = Position
+optimization.modifier.finset.position.desc = Optimize the fin set position along the rocket body.
+
+optimization.modifier.launchlug.length = Length
+optimization.modifier.launchlug.length.desc = Optimize the launch lug length.
+optimization.modifier.launchlug.outerDiameter = Outer diameter
+optimization.modifier.launchlug.outerDiameter.desc = Optimize the outer diameter of the launch lug.
+optimization.modifier.launchlug.thickness = Thickness
+optimization.modifier.launchlug.thickness.desc = Optimize the launch lug thickness while keeping the outer diameter constant.
+optimization.modifier.launchlug.position = Position
+optimization.modifier.launchlug.position.desc = Optimize the launch lug position along the rocket body.
+
+
+optimization.modifier.internalcomponent.position = Position
+optimization.modifier.internalcomponent.position.desc = Optimize the position of the component relative to the parent component.
+
+optimization.modifier.masscomponent.mass = Mass
+optimization.modifier.masscomponent.mass.desc = Optimize the mass of the mass component.
+
+optimization.modifier.parachute.diameter = Diameter
+optimization.modifier.parachute.diameter.desc = Optimize the parachute canopy diameter.
+optimization.modifier.parachute.coefficient = Drag coefficient
+optimization.modifier.parachute.coefficient.desc = Optimize the drag coefficient of the parachute. Typical parachutes have a drag coefficient of about 0.8.
+
+optimization.modifier.streamer.length = Length
+optimization.modifier.streamer.length.desc = Optimize the length of the streamer.
+optimization.modifier.streamer.width = Width
+optimization.modifier.streamer.width.desc = Optimize the width of the streamer.
+optimization.modifier.streamer.aspectRatio = Aspect ratio
+optimization.modifier.streamer.aspectRatio.desc = Optimize the aspect ratio of the streamer (length/width). You should NOT select streamer length or width at the same time with the aspect ratio.
+optimization.modifier.streamer.coefficient = Drag coefficient
+optimization.modifier.streamer.coefficient.desc = Optimize the drag coefficient of the streamer.
+
+optimization.modifier.recoverydevice.deployDelay = Deployment delay
+optimization.modifier.recoverydevice.deployDelay.desc = Optimize the deployment delay of the recovery device.
+optimization.modifier.recoverydevice.deployAltitude = Deployment altitude
+optimization.modifier.recoverydevice.deployAltitude.desc = Optimize the deployment altitude of the recovery device.
+
+optimization.modifier.rocketcomponent.overrideMass = Override mass
+optimization.modifier.rocketcomponent.overrideMass.desc = Optimize the overridden mass of the component.
+optimization.modifier.rocketcomponent.overrideCG = Override CG
+optimization.modifier.rocketcomponent.overrideCG.desc = Optimize the overridden center of gravity of the component.
+
+optimization.modifier.motormount.overhang = Motor overhang
+optimization.modifier.motormount.overhang.desc = Optimize the motor overhang.
+optimization.modifier.motormount.delay = Motor ignition delay
+optimization.modifier.motormount.delay.desc = Optimize the motor ignition delay.
+
+
+
+
+! General rocket design optimization dialog
+
+GeneralOptimizationDialog.title = Rocket optimization
+GeneralOptimizationDialog.goal.maximize = Maximize value
+GeneralOptimizationDialog.goal.minimize = Minimize value
+GeneralOptimizationDialog.goal.seek = Seek value of
+GeneralOptimizationDialog.btn.start = Start optimization
+GeneralOptimizationDialog.btn.stop = Stop optimization
+GeneralOptimizationDialog.lbl.paramsToOptimize = Parameters to optimize:
+GeneralOptimizationDialog.btn.add = Add
+GeneralOptimizationDialog.btn.add.ttip = Add the selected parameter to the optimization
+GeneralOptimizationDialog.btn.remove = Remove
+GeneralOptimizationDialog.btn.remove.ttip = Remove the selected parameter from the optimization
+GeneralOptimizationDialog.btn.removeAll = Remove all
+GeneralOptimizationDialog.btn.removeAll.ttip = Remove all parameters from the optimization
+GeneralOptimizationDialog.lbl.availableParams = Available parameters:
+GeneralOptimizationDialog.lbl.optimizationOpts = Optimization options
+GeneralOptimizationDialog.lbl.optimizeSim = Optimize simulation:
+GeneralOptimizationDialog.lbl.optimizeSim.ttip = Select which simulation to optimize
+GeneralOptimizationDialog.lbl.optimizeValue = Optimized value:
+GeneralOptimizationDialog.lbl.optimizeValue.ttip = Select what value is to be optimized
+GeneralOptimizationDialog.lbl.optimizeGoal = Optimization goal:
+GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Select the goal of the optimization
+GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Custom value to seek
+GeneralOptimizationDialog.lbl.requireStability = Required stability
+GeneralOptimizationDialog.lbl.requireMinStability = Minimum stability:
+GeneralOptimizationDialog.lbl.requireMinStability.ttip = Require a minimum static stability margin for the design
+GeneralOptimizationDialog.lbl.requireMaxStability = Maximum stability:
+GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Require a maximum static stability margin for the design
+GeneralOptimizationDialog.status.bestValue = Best value:
+GeneralOptimizationDialog.status.bestValue.ttip = Best optimization value found so far.
+GeneralOptimizationDialog.status.stepCount = Step count:
+GeneralOptimizationDialog.status.stepCount.ttip = Number of optimization steps that have been performed.
+GeneralOptimizationDialog.status.evalCount = Evaluations:
+GeneralOptimizationDialog.status.evalCount.ttip = Total number of function evaluations (simulations) that have been performed.
+GeneralOptimizationDialog.status.stepSize = Step size:
+GeneralOptimizationDialog.status.stepSize.ttip = Current optimization step size (relative to the optimization parameter ranges)
+GeneralOptimizationDialog.btn.plotPath = Plot path
+GeneralOptimizationDialog.btn.plotPath.ttip = Plot the optimization path (one and two dimensional optimization only)
+GeneralOptimizationDialog.btn.save = Save path
+GeneralOptimizationDialog.btn.save.ttip = Save the results of the function evaluations (simulations) as a CSV file.
+GeneralOptimizationDialog.btn.apply = Apply optimization
+GeneralOptimizationDialog.btn.apply.ttip = Apply the optimization results to the rocket design
+GeneralOptimizationDialog.btn.reset = Reset
+GeneralOptimizationDialog.btn.reset.ttip = Reset the rocket design to the current rocket design
+GeneralOptimizationDialog.btn.close = Close
+GeneralOptimizationDialog.btn.close.ttip = Close the dialog without modifying the rocket design
+GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters.
+GeneralOptimizationDialog.error.selectParams.title = Select optimization parameters
+GeneralOptimizationDialog.error.optimizationFailure.text = The optimization failed to run:
+GeneralOptimizationDialog.error.optimizationFailure.title = Optimization failed
+GeneralOptimizationDialog.undoText = Apply optimization
+GeneralOptimizationDialog.basicSimulationName = Basic simulation
+GeneralOptimizationDialog.noSimulationName = No simulation
+GeneralOptimizationDialog.table.col.parameter = Parameter
+GeneralOptimizationDialog.table.col.current = Current
+GeneralOptimizationDialog.table.col.min = Minimum
+GeneralOptimizationDialog.table.col.max = Maximum
+GeneralOptimizationDialog.export.header = Include header line
+GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions.
+GeneralOptimizationDialog.export.stability = Stability
+
+
+! Dialog for plotting optimization results
+OptimizationPlotDialog.title = Optimization results
+OptimizationPlotDialog.lbl.zoomInstructions = Click and drag down+right to zoom in, up+left to zoom out
+OptimizationPlotDialog.plot1d.title = Optimization result
+OptimizationPlotDialog.plot1d.series = Optimization result
+OptimizationPlotDialog.plot2d.title = Optimization path
+OptimizationPlotDialog.plot2d.path = Optimization path
+OptimizationPlotDialog.plot2d.evals = Evaluations
+OptimizationPlotDialog.plot.ttip.stability = Stability:
+OptimizationPlotDialog.plot.label.optimum = Optimum
+
+! Optimization parameters
+MaximumAltitudeParameter.name = Apogee altitude
+MaximumVelocityParameter.name = Maximum velocity
+MaximumAccelerationParameter.name = Maximum acceleration
+StabilityParameter.name = Stability
+GroundHitVelocityParameter.name = Ground hit speed
+LandingDistanceParameter.name = Landing distance
+TotalFlightTimeParameter.name = Total flight time
+DeploymentVelocityParameter.name = Velocity at parachute deployment
+
+
+! Compass directions drawn on a compass rose.
+CompassRose.lbl.north = N
+CompassRose.lbl.east = E
+CompassRose.lbl.south = S
+CompassRose.lbl.west = W
+
+! Compass directions with subdirections. These might not be localized even if the directions on the compass rose are.
+CompassSelectionButton.lbl.N = N
+CompassSelectionButton.lbl.NE = NE
+CompassSelectionButton.lbl.E = E
+CompassSelectionButton.lbl.SE = SE
+CompassSelectionButton.lbl.S = S
+CompassSelectionButton.lbl.SW = SW
+CompassSelectionButton.lbl.W = W
+CompassSelectionButton.lbl.NW = NW
+
+
+SlideShowDialog.btn.next = Next
+SlideShowDialog.btn.prev = Previous
+
+GuidedTourSelectionDialog.title = Guided tours
+GuidedTourSelectionDialog.lbl.selectTour = Select guided tour:
+GuidedTourSelectionDialog.lbl.description = Tour description:
+GuidedTourSelectionDialog.lbl.length = Number of slides:
+GuidedTourSelectionDialog.btn.start = Start tour!
+
+
--- /dev/null
+\r
+#\r
+# German base translation file\r
+#\r
+# Should you need to add new logical keys here is the proposed method\r
+#\r
+# className.ComponantType.componantName\r
+#\r
+#\r
+# Text tokens within braces should not be translated, e.g.\r
+# "The file '{filename}' exists."\r
+# They are pieces that are inserted dynamically.\r
+#\r
+\r
+\r
+! Set to the name of the current translation file (used for debugging purposes)\r
+debug.currentFile = messages_de.properties\r
+\r
+! RocketActions\r
+RocketActions.checkbox.Donotaskmeagain = Nicht wieder fragen\r
+RocketActions.lbl.Youcanchangedefop = Die Standardaktion kann in den Einstellungen geändert werden.\r
+RocketActions.showConfirmDialog.lbl1 = Simulationen löschen?\r
+RocketActions.showConfirmDialog.lbl2 = <html><i>Diese Aktion kann nicht rückgängig gemacht werden.</i>\r
+RocketActions.showConfirmDialog.title = Simulationen löschen\r
+RocketActions.DelCompAct.Delete = Löschen\r
+RocketActions.DelCompAct.ttip.Delete = Die ausgewählte Komponente löschen.\r
+RocketActions.DelSimuAct.Delete = Löschen\r
+RocketActions.DelSimuAct.ttip.Delete = Die ausgewählte Simulation löschen.\r
+RocketActions.DelAct.Delete = Löschen\r
+RocketActions.DelAct.ttip.Delete = Die ausgewählte Komponente oder Simulation löschen.\r
+RocketActions.CutAction.Cut = Ausschneiden\r
+RocketActions.CutAction.ttip.Cut = Diese Komponente oder Simulation ausschneiden und aus dem Design entfernen\r
+RocketActions.CopyAct.Copy = Kopieren\r
+RocketActions.CopyAct.ttip.Copy = Komponente (und Subkomponenten) in die Zwischenablage kopieren.\r
+RocketActions.PasteAct.Paste = Einfügen\r
+RocketActions.PasteAct.ttip.Paste = Fügt die Komponente oder Simulation aus der Zwischenablage in das Design ein.\r
+RocketActions.EditAct.Edit = Bearbeiten\r
+RocketActions.EditAct.ttip.Edit = Die ausgewählte Komponente bearbeiten.\r
+RocketActions.NewStageAct.Newstage = Neue Stufe\r
+RocketActions.NewStageAct.ttip.Newstage = Fügt eine neue Stufe in das Raketendesign ein.\r
+RocketActions.ActBoosterstage = Booster-Stufe\r
+RocketActions.MoveUpAct.Moveup = Nach oben verschieben\r
+RocketActions.MoveUpAct.ttip.Moveup = Verschiebt diese Komponente nach oben.\r
+RocketActions.MoveDownAct.Movedown = Nach unten verschieben\r
+RocketActions.MoveDownAct.ttip.Movedown = Verschiebt diese Komponente nach unten.\r
+\r
+! RocketPanel\r
+RocketPanel.FigTypeAct.Sideview = Seitenansicht\r
+RocketPanel.FigTypeAct.ttip.Sideview = Seitenansicht\r
+RocketPanel.FigTypeAct.Backview = Rückansicht\r
+RocketPanel.FigTypeAct.ttip.Backview = Vorderansicht\r
+RocketPanel.lbl.Motorcfg = Motorkonfiguration\r
+RocketPanel.lbl.infoMessage = <html>Zum Auswählen klicken Shift+Klick andere auswählen Doppelklick zum Bearbeiten Klicken+Ziehen zum Verschieben\r
+\r
+\r
+! BasicFrame\r
+BasicFrame.SimpleFileFilter1 = Alle Raketendesigns (*.ork; *.rkt)\r
+BasicFrame.SimpleFileFilter2 = OpenRocket Designs (*.ork)\r
+BasicFrame.SimpleFileFilter3 = RockSim Designs (*.rkt)\r
+BasicFrame.tab.Rocketdesign = Raketendesign\r
+BasicFrame.tab.Flightsim = Flugsimulation\r
+BasicFrame.title.Addnewcomp = Neue Komponente hinzufügen\r
+BasicFrame.dlg.lbl1 = Design '\r
+BasicFrame.dlg.lbl2 = ' ist nicht gespeichert.\r
+BasicFrame.dlg.lbl3 = Möchten Sie es speichern?\r
+BasicFrame.dlg.title = Design nicht gespeichert\r
+BasicFrame.StageName.Sustainer = Hauptstufe\r
+BasicFrame.WarningDialog.txt1 = Die folgenden Probleme würden beim Öffnen festgestellt\r
+BasicFrame.WarningDialog.txt2 = Einige Designeigenschaften wurde eventuell nicht korrekt geladen.\r
+BasicFrame.WarningDialog.title = Warnungen während des Öffnens der Datei\r
+\r
+\r
+! General error messages used in multiple contexts\r
+error.fileExists.title = File exists\r
+error.fileExists.desc = File '{filename}' exists. Do you want to overwrite it?\r
+\r
+error.writing.title = Error writing file\r
+error.writing.desc = An error occurred while writing to the file:\r
+\r
+\r
+! Labels used in buttons of dialog windows\r
+button.ok = OK\r
+button.cancel = Abbrechen\r
+button.close = Schließen\r
+\r
+! Common labels used in buttons of dialog windows\r
+dlg.but.ok = OK\r
+dlg.but.cancel = Abbrechen\r
+dlg.but.close = Schließen\r
+\r
+\r
+! General file type names\r
+filetypes.pdf = PDF files\r
+\r
+\r
+! About Dialog\r
+AboutDialog.lbl.version = Version\r
+! The texts below provide additional credits for the translation maintainer\r
+! - In AboutDialog.lbl.translation replace "English" with the current language.\r
+! - AboutDialog.lbl.translator is the translator / group name (may be empty)\r
+! - AboutDialog.lbl.translatorWebsite is a URL to the translator / group (may be empty)\r
+! - AboutDialog.lbl.translatorIcon is the file name of an icon under pix/translators/ (may be empty)\r
+AboutDialog.lbl.translation = Ins Deutsche übersetzt von:\r
+AboutDialog.lbl.translator = Stefan Lobas (ERIG e.V.)\r
+AboutDialog.lbl.translatorWebsite = http://www.er-ig.de/\r
+AboutDialog.lbl.translatorIcon = ERIG_Logo-small.png\r
+\r
+\r
+! Print dialog\r
+PrintDialog.title = Drucken oder exportieren\r
+PrintDialog.but.previewAndPrint = Vorschau & Drucken\r
+PrintDialog.checkbox.showByStage = In Stufen anzeigen\r
+PrintDialog.lbl.selectElements = Elemente auswählen, die berücksichtigt werden sollen:\r
+printdlg.but.saveaspdf = Als PDF speichern\r
+printdlg.but.preview = Vorschau\r
+printdlg.but.settings = Einstellungen\r
+PrintDialog.error.preview.title = Vorschau kann nicht geöffnet werden\r
+PrintDialog.error.preview.desc1 = PDF-Vorschau kann nicht geöffnet werden\r
+PrintDialog.error.preview.desc2 = Bitte "Als PDF speichern" benutzen.\r
+\r
+\r
+!PrintSettingsDialog\r
+PrintSettingsDialog.title = Print settings\r
+PrintSettingsDialog.lbl.Templatefillcolor = Template fill color:\r
+PrintSettingsDialog.lbl.Templatebordercolor = Template border color:\r
+PrintSettingsDialog.lbl.Papersize = Paper size:\r
+PrintSettingsDialog.lbl.Paperorientation = Paper orientation:\r
+PrintSettingsDialog.but.Reset = Reset\r
+PrintSettingsDialog.but.Close = Close\r
+\r
+\r
+! Bug Report dialog\r
+bugreport.dlg.title = Fehlerbericht\r
+bugreport.dlg.but.Sendbugreport = Fehlerbericht senden\r
+bugreport.dlg.but.Sendbugreport.Ttip = Automatische einen Fehlerbericht an die OpenRocket-Entwickler senden.\r
+bugreport.dlg.successmsg1 = Fehlerbericht erfolgreich gesendet.\r
+bugreport.dlg.successmsg2 = Danke für die Hilfe, OpenRocket noch besser zu machen!\r
+bugreport.dlg.successmsg3 = Fehlerbericht gesendet\r
+bugreport.dlg.connectedInternet = <html>Wenn Sie mit dem Internet verbunden sind, können Sie einfach auf <em>Fehlerbericht senden</em> klicken.\r
+bugreport.dlg.otherwise = Sonst senden Sie den den folgenden Text an diese Adresse:\r
+bugreport.lbl.Theinformation = Die oben stehenden Informationen können in einem öffentlichen Fehlerbericht erscheinen. Bitte stellen Sie sicher, dass der Bericht keine sensiblen Informationen enthält, die nicht veröffentlicht werden sollen!\r
+bugreport.dlg.failedmsg1 = OpenRocket konnte den Fehlerbericht nicht versenden:\r
+bugreport.dlg.failedmsg2 = Bitte senden Sie den Bericht manuell an\r
+bugreport.dlg.failedmsg3 = Fehler beim Versenden des Berichts\r
+bugreport.reportDialog.txt = <html><b>Sie können eine Fehler in OpenRocket mitteilen, indem Sie das unten stehende Formular ausfüllen und abschicken.</b><br>Sie können Fehler mit angehängten Dateien auch auf der Projekt-Website mitteilen.\r
+bugreport.reportDialog.txt2 = Bitte beschreiben Sie kurz, was Sie getan haben, als der Fehler auftrat.</b>\r
+bugreport.dlg.provideDescription = Please provide a description of the bug first.\r
+bugreport.dlg.provideDescription.title = Bug description missing\r
+\r
+\r
+! Debug log dialog\r
+debuglogdlg.but.clear = Löschen\r
+debuglogdlg.OpenRocketdebuglog = OpenRocket Fehler-Log\r
+debuglogdlg.Displayloglines = Zeige Log-Zeilen:\r
+debuglogdlg.Follow = Folgen\r
+debuglogdlg.col.Time = Zeit\r
+debuglogdlg.col.Level = Level\r
+debuglogdlg.col.Location = Ort\r
+debuglogdlg.col.Message = Nachricht\r
+debuglogdlg.lbl.Loglinenbr = Log-Zeilennummer\r
+debuglogdlg.lbl.Time = Zeit:\r
+debuglogdlg.lbl.Level = Level:\r
+debuglogdlg.lbl.Location = Location:\r
+debuglogdlg.lbl.Logmessage = Log message:\r
+debuglogdlg.lbl.Stacktrace = Stack trace:\r
+\r
+\r
+! Edit Motor configuration dialog\r
+edtmotorconfdlg.but.removemotor = Motor entfernen\r
+edtmotorconfdlg.but.Selectmotor = Motor auswählen\r
+edtmotorconfdlg.but.Removeconfiguration = Konfiguration entfernen\r
+edtmotorconfdlg.but.Newconfiguration = Neue Konfiguration\r
+edtmotorconfdlg.lbl.Motormounts = <html><b>Motorhalterungen:</b>\r
+edtmotorconfdlg.title.Editmotorconf = Motorkonfiguration bearbeiten\r
+edtmotorconfdlg.selectcomp = <html>Auswählen, welche Komponenten Motorhalterungen sind:\r
+edtmotorconfdlg.lbl.Motorconfig = <html><b>Motorkonfigurationen:</b>\r
+edtmotorconfdlg.lbl.Configname = Name der Konfiguration:\r
+edtmotorconfdlg.lbl.Leavenamedefault = Leer lassen für Standardwert.\r
+\r
+! Example design dialog\r
+exdesigndlg.but.open = Öffnen\r
+exdesigndlg.lbl.Selectexample = Beispieldesigns zum Öffnen auswählen:\r
+exdesigndlg.lbl.Openexampledesign = Beispieldesign öffnen\r
+exdesigndlg.lbl.Exampledesignsnotfound = Beispieldesigns konnten nicht gefunden werden.\r
+exdesigndlg.lbl.Examplesnotfound = Beispieldesign konnten nicht gefunden werden\r
+\r
+\r
+! Material edit panel\r
+matedtpan.but.new = Neu\r
+matedtpan.but.edit = Bearbeiten\r
+matedtpan.but.delete = Löschen\r
+matedtpan.but.revertall = Alle löschen\r
+matedtpan.col.Material = Material\r
+matedtpan.col.Type = Typ\r
+matedtpan.col.Density = Dichte\r
+matedtpan.col.but.ttip.New = Neues Material hinzufügen\r
+matedtpan.title.Addcustmaterial = Benutzerdefiniertes Material hinzufügen\r
+matedtpan.but.ttip.edit = Bestehendes Material bearbeiten\r
+matedtpan.title.Editmaterial = Material bearbeiten\r
+matedtpan.title2.Editmaterial = Die mitgelieferten Materialien können nicht verändert werden.\r
+matedtpan.but.ttip.delete = Benutzerdefiniertes Material löschen\r
+matedtpan.but.ttip.revertall = Alle benutzerdefinierten Materialien löschen\r
+matedtpan.title.Deletealluser-defined = Alle benutzerdefinierten Materialien löschen?\r
+matedtpan.title.Revertall = Alle löschen?\r
+matedtpan.lbl.edtmaterials = Das Bearbeiten der Materialien beeinflusst keine bereits existierenden Raketendesigns.\r
+\r
+!MaterialModel\r
+MaterialModel.title.Material = Material\r
+MaterialModel.title.Defcustmat = Benutzerdefiniertes Material definieren\r
+\r
+\r
+! Preference dialog\r
+pref.dlg.but.add = Hinzufügen\r
+pref.dlg.but.reset = Zurücksetzen\r
+pref.dlg.but.checknow = Jetzt überprüfen\r
+pref.dlg.but.defaultmetric = Metrisches System\r
+pref.dlg.but.defaultimperial = Imperialistisches System\r
+pref.dlg.title.Preferences = Einstellungen\r
+pref.dlg.tab.Units = Einheiten\r
+pref.dlg.tab.Defaultunits = Standardeinheiten\r
+pref.dlg.tab.Materials = Materialien\r
+pref.dlg.tab.Custommaterials = Benutzerdefinierte Materialien\r
+pref.dlg.tab.Options = Optionen\r
+pref.dlg.tab.Miscellaneousoptions = Weiter Optionen\r
+pref.dlg.lbl.Positiontoinsert = Position, um neue Komponenten einzufügen:\r
+pref.dlg.lbl.Confirmdeletion = Löschen von Simulationen bestätigen\r
+pref.dlg.lbl.User-definedthrust = Benutzerdefinierte Schubkurven:\r
+pref.dlg.Allthrustcurvefiles = Alle Schubkurvendateien (*.eng; *.rrse; *.zzip; Verzeichnisse)\r
+pref.dlg.RASPfiles = RASP Schubkurven (*.eng)\r
+pref.dlg.RockSimfiles = RockSim Schubkurven(*.rse)\r
+pref.dlg.ZIParchives = ZIP-Archiv (*.zip)\r
+pref.dlg.checkbox.Checkupdates = Beim Starten auf neue Version prüfen\r
+pref.dlg.ttip.Checkupdatesnow = Jetzt auf neue Version prüfen\r
+pref.dlg.lbl.Selectprefunits = Wählen Sie Ihre bevorzugten Einheiten aus:\r
+pref.dlg.lbl.Rocketdimensions = Raketendimensionen:\r
+pref.dlg.lbl.Linedensity = Liniendichte:\r
+pref.dlg.lbl.Motordimensions = Motordimensionen:\r
+pref.dlg.lbl.Surfacedensity = Oberflächendichte:\r
+pref.dlg.lbl.Distance = Entfernung:\r
+pref.dlg.lbl.Bulkdensity = Bulk density::\r
+pref.dlg.lbl.Velocity = Geschwindigkeit\r
+pref.dlg.lbl.Surfaceroughness = Oberflächenrauhheit:\r
+pref.dlg.lbl.Acceleration = Beschleunigung:\r
+pref.dlg.lbl.Area = Fläche\r
+pref.dlg.lbl.Mass = Masse:\r
+pref.dlg.lbl.Angle = Winkel:\r
+pref.dlg.lbl.Force = Kraft:\r
+pref.dlg.lbl.Rollrate = Roll-Rate:\r
+pref.dlg.lbl.Totalimpulse = Gesamtimpuls:\r
+pref.dlg.lbl.Temperature = Temperatur:\r
+pref.dlg.lbl.Momentofinertia = Trägheitsmoment:\r
+pref.dlg.lbl.Pressure = Druck:\r
+pref.dlg.lbl.Stability = Stabilität:\r
+pref.dlg.lbl.FlightTime = Flight time:\r
+pref.dlg.lbl.effect1 = Die Änderungen werden wirksam, wenn Sie das nächste Mal ein Fenster öffnen.\r
+pref.dlg.lbl.Checkingupdates = Prüfe, ob Aktualisierungen verfügbar sind...\r
+pref.dlg.lbl.msg1 = Ein Fehler trat bei der Kommunikation mit dem Server auf.\r
+pref.dlg.lbl.msg2 = Es konnten keine Informationen über Programmaktualisierungen empfangen werden.\r
+pref.dlg.lbl.msg3 = Sie benutzen die neueste Version von OpenRocket.\r
+pref.dlg.lbl.msg4 = Keine Aktualisierungen verfügbar.\r
+pref.dlg.PrefChoiseSelector1 = Immer fragen\r
+pref.dlg.PrefChoiseSelector2 = in der Mitte einfügen\r
+pref.dlg.PrefChoiseSelector3 = an das Ende anhängen\r
+pref.dlg.PrefBooleanSelector1 = Löschen\r
+pref.dlg.PrefBooleanSelector2 = Bestätigen\r
+pref.dlg.Add = Hinzufügen\r
+pref.dlg.DescriptionArea.Adddirectories = Um eigene Schubkurven zu laden, Verzeichnisse, RASP-Motordateien (*.eng), RockSim-Motordateien (*.rse) oder ZIP-Archive mit Semikolon getrennt eingeben. Änderungen werden beim nächsten Neustart von OpenRocket übernommen.\r
+\r
+PreferencesDialog.lbl.language = Interface language:\r
+PreferencesDialog.languages.default = System default\r
+PreferencesDialog.lbl.languageEffect = The language will change the next time you start OpenRocket.\r
+\r
+! Simulation edit dialog\r
+simedtdlg.but.runsimulation = Simulation starten\r
+simedtdlg.but.resettodefault = Auf Standardeinstellungen zurücksetzen\r
+simedtdlg.but.add = Hinzufügen\r
+simedtdlg.but.remove = Entfernen\r
+simedtdlg.title.Editsim = Simulation bearbeiten\r
+simedtdlg.lbl.Simname = Name der Simulation:\r
+simedtdlg.tab.Launchcond = Startbedingungen\r
+simedtdlg.tab.Simopt = Simulationsoptionen\r
+simedtdlg.tab.Plotdata = Daten plotten\r
+simedtdlg.tab.Exportdata = Daten exportieren\r
+simedtdlg.lbl.Motorcfg = Motorkonfiguration:\r
+simedtdlg.lbl.ttip.Motorcfg = Motorkonfiguration auswählen\r
+simedtdlg.combo.ttip.motorconf = Die Motorkonfiguration auswählen.\r
+simedtdlg.lbl.Wind = Wind\r
+simedtdlg.lbl.Averwindspeed = Durchschnittliche Windgeschwindigkeit:\r
+simedtdlg.lbl.ttip.Averwindspeed = Die durchschnittliche Windgeschwindigkeit relativ zum Boden.\r
+simedtdlg.lbl.Stddeviation = Standardabweichung\r
+simedtdlg.lbl.ttip.Stddeviation = <html>Die Standardabweichung der Windgeschwindigkeit. <br>Die Windgeschwindigkeit liegt im Durchschnitt zu 95% der Zeit in der doppelten Standardabweichung.\r
+simedtdlg.lbl.Turbulenceintensity = Intensität der Turbulenz:\r
+simedtdlg.lbl.ttip.Turbulenceintensity1 = <html>Die Intensität der Turbulenz ist die Standardabweichung geteilt durch durch die durchschnittliche Windgeschwindigkeit.<br>\r
+simedtdlg.lbl.ttip.Turbulenceintensity2 = Typischer Wertebereich von\r
+simedtdlg.lbl.ttip.Turbulenceintensity3 = bis\r
+simedtdlg.border.Atmoscond = Atmosphärische Bedingungen\r
+simedtdlg.checkbox.InterStdAtmosphere = Internationale Standardatmosphäre benutzen\r
+simedtdlg.checkbox.ttip.InterStdAtmosphere1 = <html>Auswählen, um das Modell der Internationalen Standardatmosphäre zu verwenden.<br>In diesem Modell gilt eine Temperatur von\r
+simedtdlg.checkbox.ttip.InterStdAtmosphere2 = und ein Luftdruck von\r
+simedtdlg.checkbox.ttip.InterStdAtmosphere3 = auf Meeresniveau.\r
+simedtdlg.lbl.Temperature = Temperatur:\r
+simedtdlg.lbl.ttip.Temperature = Die Temperatur am Startplatz.\r
+simedtdlg.lbl.Pressure = Luftdruck:\r
+simedtdlg.lbl.ttip.Pressure = Der Luftdruck am Startplatz.\r
+simedtdlg.lbl.Launchsite = Startplatz\r
+simedtdlg.lbl.Latitude = Breitengrad:\r
+simedtdlg.lbl.ttip.Latitude = <html>Der Breitengrad des Startplatzes beeinflusst die wirksame Gravitationskraft.<br>Positive Werte liegen auf der Nordhalbkugel, negative Werte auf der Südhalbkugel.\r
+\r
+simedtdlg.lbl.Longitude = Longitude:\r
+simedtdlg.lbl.ttip.Longitude = <html>Required for weather prediction and elevation models.\r
+\r
+simedtdlg.lbl.Altitude = Höhe:\r
+simedtdlg.lbl.ttip.Altitude = <html>Die Höhe des Startplatzes über Meeresniveau.<br>Die Höhe des Startplatzes beeinflusst die Position der Rakete im atmosphärischen Modell.\r
+simedtdlg.border.Launchrod = Startrampe\r
+simedtdlg.lbl.Length = Länge:\r
+simedtdlg.lbl.ttip.Length = Die Länge der Startrampe\r
+simedtdlg.lbl.Angle = Winkel:\r
+simedtdlg.lbl.ttip.Angle = Der Winkel der Startrampe aus der Vertikalen.\r
+simedtdlg.lbl.Direction = Richtung:\r
+simedtdlg.lbl.ttip.Direction1 = <html>Richtung der Startrampe relativ zur Windrichtung<br>\r
+simedtdlg.lbl.ttip.Direction2 = = gegen den Wind.\r
+simedtdlg.lbl.ttip.Direction3 = = mit dem Wind\r
+simedtdlg.border.Simopt = Simulationsoptionen\r
+simedtdlg.lbl.Calcmethod = Berechnungsmethode\r
+simedtdlg.lbl.ttip.Calcmethod = <html>Die erweiterte Methode nach Barrowman berechnet die aerodynamischen Kräfte<br>nach den Gleichungen von Barrowman, die um weitere Faktoren erweitert wurden.\r
+simedtdlg.lbl.ExtBarrowman = Barrowman (erweitert)\r
+simedtdlg.lbl.Simmethod = Simulationsmethode:\r
+simedtdlg.lbl.ttip.Simmethod1 = <html>Der Sechs-Freiheitsgradsimulator erlaubt der Rakete völlige Bewegungsfreiheit während des Fluges.<br>\r
+simedtdlg.lbl.ttip.Simmethod2 = Das Integrieren wird nach dem numerischen Runge-Kutta-Verfahren 4. Ordnung durchgeführt.\r
+simedtdlg.lbl.GeodeticMethod = Geodetic calculations:\r
+simedtdlg.lbl.ttip.GeodeticMethodTip = Relate to the calculation of coordinates on the earth. This also enables coriolis effect computations.\r
+simedtdlg.lbl.Timestep = Zeitschritt:\r
+simedtdlg.lbl.ttip.Timestep1 = <html>Die Zeit zwischen den Simulationsschritten.<br>Kleinere Schritte ergeben genauere Ergebnisse, die Simulationen dauern aber länger.<br>\r
+simedtdlg.lbl.ttip.Timestep2 = Die Berechnung der Simulation mit dem Verfahren 4. Ordnung liefert gute Ergebnisse mit Zeitschritten von\r
+simedtdlg.but.ttip.resettodefault = Zeitschritte zurücksetzen auf den Standardwert (\r
+simedtdlg.border.Simlist = Simulationsempfänger\r
+simedtdlg.txt.longA1 = <html><i>Simulationsempfänger</i> sind ein fortgeschrittenes Feature, dass es benutzerdefinierten Programmen erlaubt, die Simulationsdaten zu empfangen und mit der Simulation zu interagieren. \r
+simedtdlg.txt.longA2 = Mehr Information zum Schreiben von Simualtionsempfängern sind in der OpenRocket technical documentation zu finden.\r
+simedtdlg.lbl.Curlist = Aktuelle Simulationsempfänger:\r
+simedtdlg.lbl.Addsimlist = Simulationsempfänger hinzufügen\r
+simedtdlg.lbl.Noflightdata = Keine Flugdaten verfügbar.\r
+simedtdlg.lbl.runsimfirst = Bitte erst die Simulation ausführen.\r
+simedtdlg.chart.Simflight = Simulierter Flug\r
+simedtdlg.dlg.Simres = Ergebnisse der Simulation\r
+simedtdlg.IntensityDesc.None = Keine\r
+simedtdlg.IntensityDesc.Verylow = Sehr niedrig\r
+simedtdlg.IntensityDesc.Low = Niedrig\r
+simedtdlg.IntensityDesc.Medium = Mittel\r
+simedtdlg.IntensityDesc.High = Hoch\r
+simedtdlg.IntensityDesc.Veryhigh = Sehr hoch\r
+simedtdlg.IntensityDesc.Extreme = Extrem\r
+\r
+GeodeticComputationStrategy.none.name = None\r
+GeodeticComputationStrategy.none.desc = Perform no geodetic computations.\r
+GeodeticComputationStrategy.spherical.name = Spherical approximation\r
+GeodeticComputationStrategy.spherical.desc = <html>Perform geodetic computations assuming a spherical Earth.<br>This is sufficiently accurate for almost all purposes.\r
+GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid\r
+GeodeticComputationStrategy.wgs84.desc = <html>Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.<br>Slower and unnecessary in most cases.\r
+\r
+\r
+\r
+\r
+! Simulation Panel\r
+simpanel.but.newsimulation = Neue Simulation\r
+simpanel.but.editsimulation = Simulation bearbeiten\r
+simpanel.but.runsimulations = Simulation ausführen\r
+simpanel.but.deletesimulations = Simulation löschen\r
+simpanel.but.plotexport = Plotten / exportieren\r
+simpanel.but.ttip.newsimulation = Neue Simulation hinzufügen\r
+simpanel.but.ttip.editsim = Ausgewählte Simulation bearbeiten\r
+simpanel.but.ttip.runsimu = Neuberechnen der ausgewählten Simulationen\r
+simpanel.but.ttip.deletesim = Ausgewählte Simulationen löschen\r
+simpanel.checkbox.donotask = Nicht wieder fragen\r
+simpanel.lbl.defpref = Die Standardaktion kann in den Einstellungen geändert werden.\r
+simpanel.dlg.lbl.DeleteSim1 = Die ausgewählten Simulationen löschen?\r
+simpanel.dlg.lbl.DeleteSim2 = <html><i>Diese Aktion kann nicht rückgängig gemacht werden.</i>\r
+simpanel.dlg.lbl.DeleteSim3 = Simulationen löschen\r
+simpanel.col.Name = Name der Simulation:\r
+simpanel.col.Motors = Motoren\r
+simpanel.col.Apogee = Apogäum\r
+simpanel.col.Maxvelocity = max. Geschwindigkeit\r
+simpanel.col.Maxacceleration = max. Beschleunigung\r
+simpanel.col.Timetoapogee = Zeit bis zum Apogäum\r
+simpanel.col.Flighttime = Flugzeit\r
+simpanel.col.Groundhitvelocity = Landegeschwindigkeit\r
+\r
+! SimulationRunDialog\r
+SimuRunDlg.title.RunSim = Simuliere...\r
+SimuRunDlg.lbl.Running = Arbeite...\r
+SimuRunDlg.lbl.Simutime = Simulationsdauer:\r
+SimuRunDlg.lbl.Altitude = Höhe:\r
+SimuRunDlg.lbl.Velocity = Geschwindigkeit:\r
+SimuRunDlg.msg.Unabletosim = Simulieren nicht möglich:\r
+SimuRunDlg.msg.errorOccurred = Während der Simulation trat ein Fehler auf:\r
+SimuRunDlg.msg.AnException1 = Während der Simulation trat eine Ausnahme auf:\r
+SimuRunDlg.msg.AnException2 = Bitte berichten Sie diesen Fehler mit den unten stehenden Details.\r
+SimuRunDlg.msg.AssertionError1 = Während der Simulation trat ein Berechnungsfehler auf:\r
+SimuRunDlg.msg.AssertionError2 = Bitte berichten Sie diesen Fehler mit den unten stehenden Details.\r
+SimuRunDlg.msg.unknownerror1 = Während der Simulation trat ein unbekannter Fehler auf:\r
+SimuRunDlg.msg.unknownerror2 = Das Programm könnte instabil sein, speichern Sie Ihr Design und starten Sie OpenRocket neu!\r
+\r
+\r
+\r
+! SimulationExportPanel\r
+SimExpPan.desc = Komma getrennte Werte (*.csv)\r
+SimExpPan.border.Vartoexport = zu exportierende Variablen\r
+SimExpPan.but.Selectall = Alle auswählen\r
+SimExpPan.but.Selectnone = Keine auswählen\r
+SimExpPan.border.Fieldsep = Feldtrennung\r
+SimExpPan.lbl.Fieldsepstr = Trennzeichen\r
+SimExpPan.lbl.longA1 = <html>Das Trennzeichen wird benutzt, um die Felder in der exportierten Datei voneinander zu trennen.<br>\r
+SimExpPan.lbl.longA2 = Für eine CSV-Datei (Comma Separated Values) ein ',' benutzen.\r
+SimExpPan.checkbox.Includesimudesc = Simulationsbeschreibung einfügen\r
+SimExpPan.checkbox.ttip.Includesimudesc = Fügt einen Kommentar mit einer Simulationsbeschreibung am Anfang der Datei ein.\r
+SimExpPan.border.Comments = Kommentare\r
+SimExpPan.checkbox.Includefielddesc = Feldbeschreibungen einfügen\r
+SimExpPan.checkbox.ttip.Includefielddesc = Fügt eine Kommentarzeile mit der Beschreibung der exportierten Variablen ein.\r
+SimExpPan.checkbox.Incflightevents = Flugereignisse einfügen\r
+SimExpPan.checkbox.ttip.Incflightevents = Fügt eine Kommentarzeile für jedes Flugereignis ein.\r
+SimExpPan.lbl.Commentchar = Kommentarzeichen:\r
+SimExpPan.lbl.ttip.Commentchar = Zeichen, das einen Kommentar in der exportierten Datei kennzeichnet.\r
+SimExpPan.but.Exporttofile = In Datei exportieren...\r
+SimExpPan.Fileexists.desc1 = File \"",Datei \«"\r
+SimExpPan.Fileexists.desc2 = \" existiert bereits. Überschreiben?"\r
+SimExpPan.Fileexists.title = Datei existiert bereits\r
+SimExpPan.ExportingVar.desc1 = Exportiere Variable 1 aus\r
+SimExpPan.ExportingVar.desc2 = Exportiere\r
+SimExpPan.ExportingVar.desc3 = Variablen aus\r
+SimExpPan.Col.Variable = Variable\r
+SimExpPan.Col.Unit = Einheit\r
+\r
+\r
+CsvOptionPanel.separator.space = SPACE\r
+CsvOptionPanel.separator.tab = TAB\r
+\r
+\r
+\r
+! MotorPlot\r
+MotorPlot.title.Motorplot = Motorkurve\r
+MotorPlot.but.Select = Auswahl\r
+MotorPlot.Chart.Motorthrustcurve = Motorschubkurve\r
+MotorPlot.Chart.Time = Zeit / s\r
+MotorPlot.Chart.Thrust = Schub / N\r
+MotorPlot.txt.Designation = Bezeichnung:\r
+MotorPlot.txt.Manufacturer = Hersteller\r
+MotorPlot.txt.Type = Typ:\r
+MotorPlot.txt.Delays = Verzögerungen:\r
+MotorPlot.txt.Comment = Kommentare:\n\r
+\r
+\r
+\r
+! Simulation plot panel\r
+simplotpanel.lbl.Presetplotconf = Plotparameter setzen\r
+simplotpanel.lbl.Xaxistype = X-Achse:\r
+simplotpanel.lbl.Unit = Einheit:\r
+simplotpanel.lbl.Yaxistypes = Y-Achse:\r
+simplotpanel.lbl.Flightevents = Flugereignisse:\r
+simplotpanel.but.All = Alle auswählen\r
+simplotpanel.but.None = Keine\r
+simplotpanel.but.NewYaxisplottype = Neuer Y-Achsenplot-Typ\r
+simplotpanel.but.Plotflight = Flug plotten\r
+simplotpanel.lbl.Axis = Achsen:\r
+simplotpanel.but.ttip.Removethisplot = Diesen Plot löschen\r
+simplotpanel.Desc = Die Daten werden in zeitlicher Reihenfolge geplottet, auch wenn der X-Achsen-Typ nicht Zeit ist.\r
+simplotpanel.OptionPane.lbl1 = Es sind maximal 15 Plots erlaubt.\r
+simplotpanel.OptionPane.lbl2 = Plot konnte nicht hinzugefügt werden\r
+simplotpanel.AUTO_NAME = Auto\r
+simplotpanel.LEFT_NAME = Links\r
+simplotpanel.RIGHT_NAME = Rechts\r
+simplotpanel.CUSTOM = Benutzerdefiniert\r
+\r
+! Component add buttons\r
+compaddbuttons.Bodycompandfinsets = Körperteile und Leitwerke\r
+compaddbuttons.Nosecone = Spitze\r
+compaddbuttons.Bodytube = Körperrohr\r
+compaddbuttons.Transition = Übergang\r
+compaddbuttons.Trapezoidal = Trapeziod\r
+compaddbuttons.Elliptical = Elliptisch\r
+compaddbuttons.Freeform = Freiform\r
+compaddbuttons.Launchlug = Leit-\nröhrchen\r
+compaddbuttons.Innercomponent = Innenteile\r
+compaddbuttons.Innertube = Innenrohr\r
+compaddbuttons.Coupler = Koppler\r
+compaddbuttons.Centeringring = Zentrier-\nring\r
+compaddbuttons.Bulkhead = Schott\r
+compaddbuttons.Engineblock = Motor-\nblock\r
+compaddbuttons.Massobjects = Massenobjekte\r
+compaddbuttons.Parachute = Fallschirm\r
+compaddbuttons.Streamer = Strömer\r
+compaddbuttons.Shockcord = Gummiband\r
+compaddbuttons.Masscomponent = Massen-\nobjekt\r
+compaddbuttons.Donotaskmeagain = Nicht wieder fragen\r
+compaddbuttons.Selectcomppos = Komponentenposition auswählen\r
+compaddbuttons.lbl.Youcanchange = Die Standardaktion kann in den Einstellungen geändert werden.\r
+compaddbuttons.lbl.insertcomp = Die Komponente nach der aktuellen Komponente oder als letzte Komponente einfügen?\r
+compaddbuttons.askPosition.Inserthere = Hier einfügen\r
+compaddbuttons.askPosition.Addtotheend = Zum Ende hinzufügen\r
+compaddbuttons.askPosition.Cancel = Abbrechen\r
+\r
+! Component Analysis Dialog\r
+componentanalysisdlg.componentanalysis = Component analysis\r
+componentanalysisdlg.lbl.winddir = Windrichtung\r
+componentanalysisdlg.TitledBorder.warnings = Warnungen:\r
+componentanalysisdlg.ToggleBut.worst = Worst\r
+componentanalysisdlg.lbl.angleofattack = Angriffswinkel:\r
+componentanalysisdlg.lbl.machnumber = Machzahl:\r
+componentanalysisdlg.lbl.rollrate = Rollrate:\r
+componentanalysisdlg.lbl.activestages = Aktive Stufen:\r
+componentanalysisdlg.lbl.motorconf = Motorkonfiguration:\r
+componentanalysisdlg.TabStability.Col = Komponente\r
+componentanalysisdlg.TabStability = Stabilität\r
+componentanalysisdlg.TabStability.ttip = Stabilitätsinformationen\r
+componentanalysisdlg.dragTableModel.Col.Component = Komponente\r
+componentanalysisdlg.dragTableModel.Col.Pressure = <html>Druck C<sub>D</sub>\r
+componentanalysisdlg.dragTableModel.Col.Base = <html>Base C<sub>D</sub>\r
+componentanalysisdlg.dragTableModel.Col.friction = <html>Reibung C<sub>D</sub>\r
+componentanalysisdlg.dragTableModel.Col.total = <html>Gesamt C<sub>D</sub>\r
+componentanalysisdlg.dragTabchar = Luftwiderstand\r
+componentanalysisdlg.dragTabchar.ttip = Luftwiderstands-Eigenschaften\r
+componentanalysisdlg.rollTableModel.Col.component = Komponente\r
+componentanalysisdlg.rollTableModel.Col.rollforc = Roll forcing coefficient\r
+componentanalysisdlg.rollTableModel.Col.rolldamp = Roll damping coefficient\r
+componentanalysisdlg.rollTableModel.Col.total = <html>Gesamt C<sub>l</sub>\r
+componentanalysisdlg.rollTableModel = Rolldynamik\r
+componentanalysisdlg.rollTableModel.ttip = Rolldynamik\r
+componentanalysisdlg.println.closingmethod = Closing method called:\r
+componentanalysisdlg.println.settingnam = SETTING NAN VALUES\r
+componentanalysisdlg.lbl.reflenght = Referenzlänge:\r
+componentanalysisdlg.lbl.refarea = Referenzfläche:\r
+!componentanalysisdlg.But.close =Close\r
+componentanalysisdlg.TabStability.Col.Component = Component\r
+\r
+! Custom Material dialog\r
+custmatdlg.title.Custommaterial = Benutzerdefiniertes Material\r
+custmatdlg.lbl.Materialname = Name des Materials:\r
+custmatdlg.lbl.Materialtype = Materialtyp\r
+custmatdlg.lbl.Materialdensity = Materialdichte:\r
+custmatdlg.checkbox.Addmaterial = Material zur Datenbank hinzufügen\r
+\r
+\r
+! Ring Component Config\r
+ringcompcfg.OuterRadius = Äußerer Radius\r
+ringcompcfg.Automatic = Automatisch\r
+ringcompcfg.InnerRadius = Innerer Radius\r
+ringcompcfg.Thickness = Wandstärke\r
+ringcompcfg.Length = Länge\r
+ringcompcfg.Positionrelativeto = Relative Position zu:\r
+ringcompcfg.plus = plus\r
+ringcompcfg.PositionValue = Positionswert\r
+ringcompcfg.Radialdistance = Radialer Abstand:\r
+ringcompcfg.Distancefrom = Abstand von der Raketenmittellinie\r
+ringcompcfg.Radialdirection = Radiale Richtung\r
+ringcompcfg.radialdirectionfrom = Die radiale Richtung von der Raketenmittellinie\r
+ringcompcfg.but.Reset = Zurücksetzen\r
+ringcompcfg.but.Resetcomponant = Komponente auf die Raketenmittellinie zurücksetzen\r
+ringcompcfg.EngineBlock.desc = <html>Eine <b>Motorhalterung</b> verhindert, dass der Motor sich im Rohr nach vorne bewegt.<br><br>Um einen Motor hinzuzufügen, ein <b>Körperrohr</b> oder ein <b>Innenrohr</b> hinzufügen und im Reiter <em>Motor</em> als Motorhalterung markieren.\r
+ringcompcfg.note.desc = Hinweis: Innenrohre beeinflussen die Aerodynamik der Rakete nicht, auch wenn sie außerhalb des Körperohres liegen.\r
+\r
+\r
+! Body Tube Config\r
+BodyTubecfg.lbl.Bodytubelength = Länge des Körperrohres:\r
+BodyTubecfg.lbl.Outerdiameter = Außendurchmesser:\r
+BodyTubecfg.lbl.Innerdiameter = Innendurchmesser:\r
+BodyTubecfg.lbl.Wallthickness = Wandstärke:\r
+BodyTubecfg.tab.General = Allgemein\r
+BodyTubecfg.tab.Generalproperties = Allgemeine Eigenschaften\r
+BodyTubecfg.tab.Motor = Motor\r
+BodyTubecfg.tab.Motormountconf = Motorkonfiguration\r
+BodyTubecfg.checkbox.Automatic = Automatisch\r
+BodyTubecfg.checkbox.Filled = Gefüllt\r
+\r
+! FinSetConfig\r
+FinSetConfig.tab.Fintabs = Leitwerke\r
+FinSetConfig.tab.Through-the-wall = Durchsteckbare Leitwerke\r
+FinSetConfig.but.Converttofreeform = In Freiform konvertieren\r
+FinSetConfig.but.Converttofreeform.ttip = Konvertiert diese Leitwerke in eine Freiform\r
+FinSetConfig.Convertfinset = Leitwerke konvertieren\r
+FinSetConfig.but.Splitfins = Geteilte Leitwerke\r
+FinSetConfig.but.Splitfins.ttip = Teilt den Leitwerkssatz in getrennte Leitwerke\r
+FinSetConfig.lbl.Through-the-wall = Durchsteckbare Leitwerke:\r
+FinSetConfig.lbl.Tablength = Länge:\r
+FinSetConfig.ttip.Tablength = Länge des Leitwerks.\r
+FinSetConfig.lbl.Tabheight = Höhe:\r
+FinSetConfig.ttip.Tabheight = Spannweite des Leitwerks.\r
+FinSetConfig.lbl.Tabposition = Position:\r
+FinSetConfig.ttip.Tabposition = Position des Leitwerks.\r
+FinSetConfig.lbl.relativeto = relativ zu\r
+\r
+! MotorDatabaseLoadingDialog\r
+MotorDbLoadDlg.title = Lade Motoren\r
+MotorDbLoadDlg.Loadingmotors = Lade Motoren...\r
+\r
+! RocketConfig\r
+RocketCfg.lbl.Designname = Name der Rakete:\r
+RocketCfg.lbl.Designer = Ersteller:\r
+RocketCfg.lbl.Comments = Kommentare:\r
+RocketCfg.lbl.Revisionhistory = Versionsgeschichte:\r
+RocketCfg.lbl.Material = Material:\r
+\r
+! ShockCordConfig\r
+ShockCordCfg.lbl.Shockcordlength = Gummibandlänge\r
+\r
+! RocketComponentConfig\r
+RocketCompCfg.lbl.Componentname = Komponentenname:\r
+RocketCompCfg.ttip.Thecomponentname = Name der Komponente.\r
+RocketCompCfg.tab.Override = Werte überschreiben\r
+RocketCompCfg.tab.MassandCGoverride = Massen- und Schwerpunktsoptionen\r
+RocketCompCfg.tab.Figure = Form\r
+RocketCompCfg.tab.Figstyleopt = Formoptionen\r
+RocketCompCfg.tab.Comment = Kommentar\r
+RocketCompCfg.tab.Specifyacomment = Kommentar zu dieser Komponente\r
+RocketCompCfg.lbl.Mass = Masse:\r
+RocketCompCfg.lbl.Componentmass = Masse der Komponente:\r
+RocketCompCfg.lbl.overriddento = (überschrieben auf\r
+RocketCompCfg.lbl.overriddenby = (überschrieben durch\r
+RocketCompCfg.lbl.Componentmaterial = Material:\r
+RocketCompCfg.lbl.Componentfinish = Oberfläche:\r
+RocketCompCfg.lbl.ttip.componentmaterialaffects = Das Material beeinflusst die Masse der Komponente.\r
+RocketCompCfg.combo.ttip.componentmaterialaffects = Das Material beeinflusst die Masse der Komponente.\r
+RocketCompCfg.lbl.longA1 = <html>Die Oberfläche beeinflusst den aerodynamischen Widerstand der Komponente.<br>\r
+RocketCompCfg.lbl.longA2 = Der angegebene Wert ist die durchschnittliche Rautiefe der Oberfläche.\r
+RocketCompCfg.but.Setforall = Für alle setzen\r
+RocketCompCfg.but.ttip.Setforall = Diese Oberflächen für alle Komponenten der Rakete setzen.\r
+RocketCompCfg.lbl.Overridemassorcenter = Überschreiben von Masse oder Schwerpunkts von \r
+RocketCompCfg.checkbox.Overridemass = Masse überschreiben:\r
+RocketCompCfg.checkbox.Overridecenterofgrav = Schwerpunkt überschreiben:\r
+RocketCompCfg.checkbox.OverridemassandCG = Masse und Schwerpunkt für alle Unterkomponenten überschreiben\r
+RocketCompCfg.lbl.longB1 = <html>Die überschriebene Masse enthält keine Motoren.<br>\r
+RocketCompCfg.lbl.longB2 = Die Messung des Schwerpunktes beginnt am Ende von\r
+RocketCompCfg.lbl.Commentsonthe = Kommentare zu\r
+RocketCompCfg.lbl.Figurestyle = Form:\r
+RocketCompCfg.lbl.Componentcolor = Farbe:\r
+RocketCompCfg.lbl.Choosecolor = Farbe auswählen\r
+RocketCompCfg.checkbox.Usedefaultcolor = Standardfarbe verwenden\r
+RocketCompCfg.lbl.Complinestyle = Linienstil:\r
+RocketCompCfg.but.Saveasdefstyle = Als Standardstil speichern\r
+RocketCompCfg.lbl.Diameter = Durchmesser:\r
+RocketCompCfg.lbl.Length = Länge:\r
+RocketCompCfg.lbl.Thickness = Wandstärke:\r
+RocketCompCfg.checkbox.Endcapped = Verschlossenes Ende\r
+RocketCompCfg.ttip.Endcapped = Gibt an, ob das Ende der Schulter geschlossen ist.\r
+RocketCompCfg.title.Noseconeshoulder = Spitzenschulter\r
+RocketCompCfg.title.Aftshoulder = Schulter hinten\r
+RocketCompCfg.border.Foreshoulder = Schulter vorn\r
+!RocketCompCfg.lbl.Length = Length:\r
+\r
+! BulkheadConfig\r
+BulkheadCfg.tab.Radius = Radius:\r
+BulkheadCfg.tab.Thickness = Wandstärke:\r
+BulkheadCfg.tab.General = Allgemein\r
+BulkheadCfg.tab.Generalproperties = Allgemeine Eigenschaften\r
+\r
+!CenteringRingConfig\r
+CenteringRingCfg.tab.Outerdiam = Außendurchmesser:\r
+CenteringRingCfg.tab.Innerdiam = Innendurchmesser:\r
+CenteringRingCfg.tab.Thickness = Wandstärke:\r
+CenteringRingCfg.tab.General = Allgemein\r
+CenteringRingCfg.tab.Generalproperties = Allgemeine Eigenschaften\r
+\r
+!ComponentConfigDialog\r
+ComponentCfgDlg.configuration = Konfiguration\r
+ComponentCfgDlg.configuration1 =\r
+ComponentCfgDlg.Modify = Verändern\r
+\r
+!EllipticalFinSetConfig\r
+EllipticalFinSetCfg.Nbroffins = Anzahl der Leitwerke\r
+EllipticalFinSetCfg.Rotation = Rotation:\r
+EllipticalFinSetCfg.Fincant = Neigung:\r
+EllipticalFinSetCfg.Rootchord = Blatttiefe:\r
+EllipticalFinSetCfg.Height = Höhe:\r
+EllipticalFinSetCfg.Positionrelativeto = Position relativ zu:\r
+EllipticalFinSetCfg.plus = plus\r
+EllipticalFinSetCfg.FincrossSection = Querschnitt:\r
+EllipticalFinSetCfg.Thickness = Wandstärke:\r
+EllipticalFinSetCfg.General = Allgemein\r
+EllipticalFinSetCfg.Generalproperties = Allgemeine Eigenschaften\r
+EllipticalFinSetCfg.ttip.Fincant = Der Winkel, in dem die Leitwerke zum Körperrohr geneigt sind.\r
+\r
+!FreeformFinSetConfig\r
+FreeformFinSetCfg.tab.General = Allgemein\r
+FreeformFinSetCfg.tab.ttip.General = Allgemeine Eigenschaften\r
+FreeformFinSetCfg.tab.Shape = Form\r
+FreeformFinSetCfg.tab.ttip.Finshape = Leitwerksform\r
+FreeformFinSetCfg.lbl.Numberoffins = Anzahl der Leitwerke\r
+FreeformFinSetCfg.lbl.Finrotation = Rotation:\r
+FreeformFinSetCfg.lbl.Fincant = Neigung:\r
+FreeformFinSetCfg.lbl.ttip.Fincant = Der Winkel, in dem die Leitwerke zum Körperrohr geneigt sind.\r
+FreeformFinSetCfg.lbl.Posrelativeto = Position relativ zu:\r
+FreeformFinSetCfg.lbl.plus = plus\r
+FreeformFinSetCfg.lbl.FincrossSection = Querschnitt:\r
+FreeformFinSetCfg.lbl.Thickness = Wandstärke:\r
+! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle\r
+FreeformFinSetConfig.lbl.doubleClick1 = Double-click\r
+FreeformFinSetConfig.lbl.doubleClick2 = to edit\r
+FreeformFinSetConfig.lbl.clickDrag = Click+drag: Add and move points\r
+FreeformFinSetConfig.lbl.ctrlClick = Ctrl+click: Remove point\r
+\r
+\r
+!InnerTubeConfig\r
+InnerTubeCfg.tab.Motor = Motor\r
+InnerTubeCfg.tab.ttip.Motor = Motorkonfiguration\r
+InnerTubeCfg.tab.Cluster = Cluster\r
+InnerTubeCfg.tab.ttip.Cluster = Cluster-Konfiguration\r
+InnerTubeCfg.tab.Radialpos = Radiale Position\r
+InnerTubeCfg.tab.ttip.Radialpos = Radiale Position\r
+InnerTubeCfg.lbl.Selectclustercfg = Cluster-Konfiguration auswählen:\r
+InnerTubeCfg.lbl.TubeSep = Rohrtrennung\r
+InnerTubeCfg.lbl.ttip.TubeSep = Die Trennung der Rohre, 1.0 = die Rohre berühren sich\r
+InnerTubeCfg.lbl.Rotation = Rotation:\r
+InnerTubeCfg.lbl.ttip.Rotation = Rotationswinkel der Cluster-Konfiguration\r
+InnerTubeCfg.lbl.Rotangle = Rotationswinkel der Cluster-Konfiguration\r
+InnerTubeCfg.but.Splitcluster = Cluster aufteilen\r
+InnerTubeCfg.lbl.longA1 = <html>Den Cluster in einzelne Komponenten aufteilen.<br>\r
+InnerTubeCfg.lbl.longA2 = Die dupliziert alle Komponenten innerhalb dieses Innenrohrs.\r
+InnerTubeCfg.but.Resetsettings = Einstellungen zurücksetzen\r
+InnerTubeCfg.but.ttip.Resetsettings = Setzt die Aufteilung und Rotation auf die Standardwerte zurück\r
+\r
+! LaunchLugConfig\r
+LaunchLugCfg.lbl.Length = Länge:\r
+LaunchLugCfg.lbl.Outerdiam = Außendurchmesser:\r
+LaunchLugCfg.lbl.Innerdiam = Innendurchmesser:\r
+LaunchLugCfg.lbl.Thickness = Wandstärke:\r
+LaunchLugCfg.lbl.Radialpos = Radiale Position:\r
+LaunchLugCfg.lbl.Posrelativeto = Position relativ zu:\r
+LaunchLugCfg.lbl.plus = plus\r
+LaunchLugCfg.tab.General = Allgemein\r
+LaunchLugCfg.tab.Generalprop = Allgemeine Eigenschaften\r
+\r
+! MassComponentConfig\r
+MassComponentCfg.lbl.Mass = Masse\r
+MassComponentCfg.lbl.Length = Länge\r
+MassComponentCfg.lbl.Diameter = Durchmesser\r
+MassComponentCfg.lbl.PosRelativeto = Position relativ zu:\r
+MassComponentCfg.lbl.plus = plus\r
+MassComponentCfg.tab.General = Allgemein\r
+MassComponentCfg.tab.ttip.General = Allgemeine Eigenschaften\r
+MassComponentCfg.tab.Radialpos = Radiale Position\r
+MassComponentCfg.tab.ttip.Radialpos = Konfiguration der radialen Position\r
+MassComponentCfg.lbl.Radialdistance = Radialer Abstand:\r
+MassComponentCfg.lbl.Radialdirection = radiale Richtung:\r
+MassComponentCfg.but.Reset = Zurücksetzen\r
+\r
+! MotorConfig\r
+MotorCfg.checkbox.compmotormount = Diese Komponente ist eine Motorhalterung\r
+MotorCfg.lbl.Motorcfg = Motorkonfiguration\r
+MotorCfg.but.New = Neu\r
+MotorCfg.lbl.Currentmotor = Aktueller Motor:\r
+MotorCfg.lbl.Motoroverhang = Motorüberstand:\r
+MotorCfg.lbl.Ignitionat = Zündung bei:\r
+MotorCfg.lbl.plus = plus\r
+MotorCfg.lbl.seconds = Sekunden\r
+MotorCfg.lbl.longA1 = Das aktuelle Design hat im Moment nur eine Stufe.\r
+MotorCfg.lbl.longA2 = Stufen können durch Klicken auf \«Neue Stufe\« hinzugefügt werden.\r
+MotorCfg.lbl.longB1 = Das aktuelle Design hat im Moment nur eine Stufe.\r
+MotorCfg.lbl.longB2 = Stufen.\r
+MotorCfg.but.Selectmotor = Motor auswählen\r
+MotorCfg.but.Removemotor = Motor entfernen\r
+MotorCfg.lbl.motorLabel = Keiner\r
+\r
+! NoseConeConfig\r
+NoseConeCfg.lbl.Noseconeshape = Spitzenform:\r
+NoseConeCfg.lbl.Shapeparam = Formparameter:\r
+NoseConeCfg.lbl.Noseconelength = Spitzenlänge:\r
+NoseConeCfg.lbl.Basediam = Basisdurchmesser:\r
+NoseConeCfg.checkbox.Automatic = Automatisch\r
+NoseConeCfg.lbl.Wallthickness = Wandstärke:\r
+NoseConeCfg.checkbox.Filled = gefüllt\r
+NoseConeCfg.tab.General = Allgemein\r
+NoseConeCfg.tab.ttip.General = Allgemeine Eigenschaften\r
+NoseConeCfg.tab.Shoulder = Schulter\r
+NoseConeCfg.tab.ttip.Shoulder = Schultereigenschaften\r
+\r
+! ParachuteConfig\r
+ParachuteCfg.lbl.Canopy = Fallschirmkappe:\r
+ParachuteCfg.lbl.Diameter = Durchmesser:\r
+ParachuteCfg.lbl.Material = Material:\r
+ParachuteCfg.combo.MaterialModel = Das Material beeinflusst die Masse der Komponente.\r
+ParachuteCfg.lbl.longA1 = <html>Luftwiderstandskoeffizient C<sub>D</sub>:\r
+ParachuteCfg.lbl.longB1 = <html>Der Luftwiderstandsbeiwert relativ zur Gesamtfläche des Fallschirms.<br>\r
+ParachuteCfg.lbl.longB2 = Ein größerer Luftwiderstand führt zu einer kleineren Sinkrate.\r
+ParachuteCfg.lbl.longB3 = Ein typischer Wert für Fallschirme ist 0,8.\r
+ParachuteCfg.but.Reset = Zurücksetzen\r
+ParachuteCfg.lbl.Shroudlines = Fangleinen:\r
+ParachuteCfg.lbl.Numberoflines = Anzahl der Leinen:\r
+ParachuteCfg.lbl.Linelength = Länge der Leinen:\r
+ParachuteCfg.lbl.Material = Material:\r
+ParachuteCfg.lbl.Posrelativeto = Position relativ zu:\r
+ParachuteCfg.lbl.plus = plus\r
+ParachuteCfg.lbl.Packedlength = gepackte Länge:\r
+ParachuteCfg.lbl.Packeddiam = gepackter Durchmesser:\r
+ParachuteCfg.lbl.Deploysat = Auswurf bei\r
+ParachuteCfg.lbl.seconds = Sekunden\r
+ParachuteCfg.lbl.Altitude = Höhe:\r
+ParachuteCfg.tab.General = Allgemein\r
+ParachuteCfg.tab.ttip.General = Allgemeine Eigenschaften\r
+ParachuteCfg.tab.Radialpos = Radiale Position\r
+ParachuteCfg.tab.ttip.Radialpos = Konfiguration der radialen Position\r
+ParachuteCfg.lbl.Radialdistance = Radialer Abstand:\r
+ParachuteCfg.lbl.Radialdirection = radiale Richtung:\r
+ParachuteCfg.but.Reset = Zurücksetzen\r
+ParachuteCfg.lbl.plusdelay = plus\r
+\r
+! ShockCordConfig \r
+ShockCordCfg.lbl.Shockcordlength = Länge des Gummibands\r
+ShockCordCfg.lbl.Shockcordmaterial = Material des Gummibands:\r
+ShockCordCfg.lbl.Posrelativeto = Position relativ zu:\r
+ShockCordCfg.lbl.plus = plus\r
+ShockCordCfg.lbl.Packedlength = gepackte Länge:\r
+ShockCordCfg.lbl.Packeddiam = gepackter Durchmesser:\r
+ShockCordCfg.tab.General = Allgemein\r
+ShockCordCfg.tab.ttip.General = Allgemeine Eigenschaften\r
+\r
+!SleeveConfig\r
+SleeveCfg.tab.Outerdiam = Außendurchmesser:\r
+SleeveCfg.tab.Innerdiam = Innendurchmesser:\r
+SleeveCfg.tab.Wallthickness = Wandstärke:\r
+SleeveCfg.tab.Length = Länge:\r
+SleeveCfg.tab.General = Allgemein\r
+SleeveCfg.tab.Generalproperties = Allgemeine Eigenschaften\r
+\r
+! StreamerConfig\r
+StreamerCfg.lbl.Striplength = Länge des Strömers:\r
+StreamerCfg.lbl.Stripwidth = Breite des Strömers:\r
+StreamerCfg.lbl.Striparea = Fläche des Strömers:\r
+StreamerCfg.lbl.Aspectratio = Seitenverhältnis:\r
+StreamerCfg.lbl.Material = Material:\r
+StreamerCfg.combo.ttip.MaterialModel = Das Material beeinflusst die Masse der Komponente.\r
+StreamerCfg.lbl.longA1 = <html>Widerstandskoeffizient C<sub>D</sub>:\r
+StreamerCfg.lbl.longB1 = <html>Der Widerstandskoeffizient des Strömers hängt von der Gesamtfläche ab.<br>\r
+StreamerCfg.lbl.longB2 = Ein größerer Luftwiderstandskoeffizient führt zu einer kleineren Sinkrate.\r
+StreamerCfg.lbl.Automatic = Automatisch\r
+StreamerCfg.lbl.longC1 = Der Luftwiderstandskoeffizient hängt von der Fläche des Strömers ab.\r
+StreamerCfg.lbl.Posrelativeto = Position relativ zu:\r
+StreamerCfg.lbl.plus = plus\r
+StreamerCfg.lbl.Packedlength = gepackte Länge:\r
+StreamerCfg.lbl.Packeddiam = gepackter Durchmesser:\r
+StreamerCfg.lbl.Deploysat = Auswurf bei\r
+StreamerCfg.lbl.seconds = Sekunden\r
+StreamerCfg.lbl.Altitude = Höhe:\r
+StreamerCfg.tab.General = Allgemein\r
+StreamerCfg.tab.ttip.General = Allgemeine Eigenschaften\r
+StreamerCfg.tab.Radialpos = Radiale Position\r
+StreamerCfg.tab.ttip.Radialpos = Konfiguration der radialen Position\r
+StreamerCfg.lbl.Radialdistance = Radialer Abstand:\r
+StreamerCfg.lbl.Radialdirection = radiale Richtung:\r
+StreamerCfg.but.Reset = Zurücksetzen\r
+StreamerCfg.lbl.plusdelay = plus\r
+\r
+! ThicknessRingComponentConfig\r
+ThicknessRingCompCfg.tab.Outerdiam = Außendurchmesser:\r
+ThicknessRingCompCfg.tab.Innerdiam = Innendurchmesser:\r
+ThicknessRingCompCfg.tab.Wallthickness = Wandstärke:\r
+ThicknessRingCompCfg.tab.Length = Länge:\r
+ThicknessRingCompCfg.tab.General = Allgemein\r
+ThicknessRingCompCfg.tab.Generalprop = Allgemeine Eigenschaften\r
+\r
+! TransitionConfig\r
+TransitionCfg.lbl.Transitionshape = Form des Übergangs\r
+TransitionCfg.checkbox.Clipped = geklemmt\r
+TransitionCfg.lbl.Shapeparam = Formparameter:\r
+TransitionCfg.lbl.Transitionlength = Länge des Übergangs:\r
+TransitionCfg.lbl.Forediam = Vorderer Durchmesser\r
+TransitionCfg.checkbox.Automatic = Automatisch\r
+TransitionCfg.lbl.Aftdiam = Hinterer Durchmesser\r
+TransitionCfg.lbl.Wallthickness = Wandstärke:\r
+TransitionCfg.checkbox.Filled = gefüllt\r
+TransitionCfg.tab.General = Allgemein\r
+TransitionCfg.tab.Generalproperties = Allgemeine Eigenschaften\r
+TransitionCfg.tab.Shoulder = Schulter\r
+TransitionCfg.tab.Shoulderproperties = Schultereigenschaften\r
+\r
+! TrapezoidFinSetConfig\r
+TrapezoidFinSetCfg.lbl.Nbroffins = Anzahl der Leitwerke\r
+TrapezoidFinSetCfg.lbl.ttip.Nbroffins = Anzahl der Leitwerke in diesem Satz\r
+TrapezoidFinSetCfg.lbl.Finrotation = Rotation der Leitwerke\r
+TrapezoidFinSetCfg.lbl.ttip.Finrotation = Winkel des ersten Leitwerks in diesem Satz\r
+TrapezoidFinSetCfg.lbl.Fincant = Neigung:\r
+TrapezoidFinSetCfg.lbl.ttip.Fincant = Der Winkel, in dem die Leitwerke zum Körperrohr geneigt sind.\r
+TrapezoidFinSetCfg.lbl.Rootchord = Blatttiefe:\r
+TrapezoidFinSetCfg.lbl.Tipchord = Blatttiefe (Spitze)\r
+TrapezoidFinSetCfg.lbl.Height = Höhe:\r
+TrapezoidFinSetCfg.lbl.Sweeplength = Blattbreite:\r
+TrapezoidFinSetCfg.lbl.Sweepangle = Pfeilungswinkel\r
+TrapezoidFinSetCfg.lbl.FincrossSection = Leitwerksquerschnitt\r
+TrapezoidFinSetCfg.lbl.Thickness = Wandstärke:\r
+TrapezoidFinSetCfg.lbl.Posrelativeto = Position relativ zu:\r
+TrapezoidFinSetCfg.lbl.plus = plus\r
+TrapezoidFinSetCfg.tab.General = Allgemein\r
+TrapezoidFinSetCfg.tab.Generalproperties = Allgemeine Eigenschaften\r
+\r
+!MotorConfigurationModel\r
+MotorCfgModel.Editcfg = Konfiguration bearbeiten\r
+\r
+! StorageOptionChooser\r
+StorageOptChooser.lbl.Simdatatostore = Zu speichernde Simulationsdaten:\r
+StorageOptChooser.rdbut.Allsimdata = Alle Simulationsdaten\r
+StorageOptChooser.lbl.longA1 = <html>Speichert alle Simulationsdaten.<br>\r
+StorageOptChooser.lbl.longA2 = Dies kann sehr große Dateien erzeugen!\r
+StorageOptChooser.rdbut.Every = Alle Simulationsdaten\r
+StorageOptChooser.lbl.longB1 = <html>Speicher plotbare Daten in etwa diesem Abstand.<br>\r
+StorageOptChooser.lbl.longB2 = Größere Werte erzeugen kleinere Dateien.\r
+StorageOptChooser.lbl.seconds = Sekunden\r
+StorageOptChooser.rdbut.Onlyprimfig = Nur die wichtigsten Werte\r
+StorageOptChooser.lbl.longC1 = <html>Speichert nur die Werte, die in der Zusammenfassung stehen.<br>\r
+StorageOptChooser.lbl.longC2 = Dies ergibt die kleinsten Dateien\r
+StorageOptChooser.checkbox.Compfile = Datei komprimieren\r
+StorageOptChooser.lbl.UsingComp = Kompression der Datei verringert die Größe signifikant.\r
+StorageOptChooser.lbl.longD1 = Eine Schätzung der Dateigröße mit den gegebenen Optionen.\r
+StorageOptChooser.ttip.Saveopt = Speicheroptionen\r
+StorageOptChooser.lbl.Estfilesize = Voraussichtliche Dateigröße:\r
+StorageOptChooser.lbl.Saveopt = Speicheroptionen\r
+\r
+! ThrustCurveMotorSelectionPanel\r
+TCMotorSelPan.lbl.Selrocketmotor = Raketenmotor auswählen:\r
+TCMotorSelPan.checkbox.hideSimilar = Ähnliche Schubkurven verbergen\r
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Alle Motoren anzeigen\r
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Motoren anzeigen, deren Durchmesser kleiner als der der Motorhalterung ist\r
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Motoren anzeigen, deren Durchmesser gleich der der Motorhalterung ist\r
+TCMotorSelPan.lbl.Motormountdia = Durchmesser der Motorhalterung\r
+TCMotorSelPan.lbl.Search = Suchen:\r
+TCMotorSelPan.lbl.Selectthrustcurve = Schubkurve auswählen:\r
+TCMotorSelPan.lbl.Ejectionchargedelay = Verzögerung der Ausstoßladung:\r
+TCMotorSelPan.equalsIgnoreCase.None = keine\r
+TCMotorSelPan.lbl.NumberofsecondsorNone = (Anzahl der Sekunden oder \«keine\«)\r
+TCMotorSelPan.lbl.Totalimpulse = Gesamtimpuls:\r
+TCMotorSelPan.lbl.Avgthrust = Durchschn. Schub:\r
+TCMotorSelPan.lbl.Maxthrust = max. Schub\r
+TCMotorSelPan.lbl.Burntime = Brenndauer:\r
+TCMotorSelPan.lbl.Launchmass = Startmasse:\r
+TCMotorSelPan.lbl.Emptymass = Leermasse:\r
+TCMotorSelPan.lbl.Datapoints = Datenpunkte:\r
+TCMotorSelPan.lbl.Digest = Übersicht:\r
+TCMotorSelPan.title.Thrustcurve = Schubkurve:\r
+TCMotorSelPan.title.Thrust = Schub:\r
+TCMotorSelPan.delayBox.None = keine\r
+\r
+\r
+! PlotDialog\r
+PlotDialog.title.Flightdataplot = Flugdatenplot\r
+PlotDialog.Chart.Simulatedflight = Simulierter Flug\r
+PlotDialog.CheckBox.Showdatapoints = Datenpunkte anzeigen\r
+PlotDialog.lbl.Chart = Klicken+ziehen: runter+rechts um hinein zu zoomen, hoch+links um heraus zu zoomen \r
+\r
+\r
+! "main" prefix is used for the main application dialog\r
+\r
+# FIXME: Rename the description keys \r
+\r
+main.menu.file = Datei\r
+main.menu.file.desc = File-handling related tasks\r
+main.menu.file.new = Neu\r
+main.menu.file.new.desc = Create a new rocket design\r
+main.menu.file.open = Öffnen..\r
+BasicFrame.item.Openrocketdesign = Raketendesign öffnen\r
+main.menu.file.openExample = Beispiel öffnen..\r
+BasicFrame.item.Openexamplerocketdesign = Beispieldesign öffnen\r
+main.menu.file.save = Speichern\r
+BasicFrame.item.SavecurRocketdesign = Aktuelles Raketendesign speichern\r
+main.menu.file.saveAs = Speichern unter...\r
+BasicFrame.item.SavecurRocketdesnewfile = Aktuelles Raketendesign in eine neue Datei speichern\r
+main.menu.file.print = Drucken / als PDF exportieren...\r
+BasicFrame.item.Printpart = Komponentenliste und Leitwerkschablone drucken\r
+main.menu.file.close = Schließen\r
+BasicFrame.item.Closedesign = Aktuelles Raketendesign schließen\r
+main.menu.file.quit = Beenden\r
+BasicFrame.item.Quitprogram = Programm beenden\r
+\r
+main.menu.edit = Bearbeiten\r
+BasicFrame.menu.Rocketedt = Rakete bearbeiten\r
+main.menu.edit.undo = Rückgängig\r
+main.menu.edit.undo.desc = Undo the previous operation\r
+main.menu.edit.redo = Wiederholen\r
+main.menu.edit.redo.desc = Redo the previously undone operation\r
+main.menu.edit.cut = Ausschneiden\r
+main.menu.edit.copy = Kopieren\r
+main.menu.edit.paste = Einfügen\r
+main.menu.edit.delete = Löschen\r
+main.menu.edit.resize = Scale...\r
+main.menu.edit.resize.desc = Scale parts of the rocket design\r
+main.menu.edit.preferences = Einstellungen\r
+main.menu.edit.preferences.desc = Setup the application preferences\r
+\r
+main.menu.analyze = Analysieren\r
+main.menu.analyze.desc = Rocket analysis\r
+main.menu.analyze.componentAnalysis = Komponente analysieren\r
+main.menu.analyze.componentAnalysis.desc = Analyze the rocket components separately\r
+main.menu.analyze.optimization = Rocket optimization\r
+main.menu.analyze.optimization.desc = General rocket design optimization\r
+\r
+main.menu.help = Hilfe\r
+main.menu.help.desc = Information about OpenRocket\r
+main.menu.help.license = Lizenz\r
+main.menu.help.license.desc = OpenRocket license information\r
+main.menu.help.bugReport = Fehlerbericht\r
+main.menu.help.bugReport.desc = Information about reporting bugs in OpenRocket\r
+main.menu.help.debugLog = Debug-Log\r
+main.menu.help.debugLog.desc = View the OpenRocket debug log\r
+main.menu.help.about = Über\r
+main.menu.help.about.desc = Copyright details about OpenRocket\r
+\r
+main.menu.debug = Debug\r
+main.menu.debug.whatisthismenu = Was macht diese Menü?\r
+main.menu.debug.createtestrocket = Eine Testrakete erstellen\r
+\r
+! database\r
+! Translate here all material database\r
+!\r
+\r
+! Material database\r
+! BULK_MATERIAL\r
+Databases.materials.Acrylic = Acryl\r
+Databases.materials.Balsa = Balsa\r
+Databases.materials.Birch = Birke\r
+Databases.materials.Cardboard = Karton\r
+Databases.materials.Carbonfiber = Kohlefaser\r
+Databases.materials.Cork = Kork\r
+Databases.materials.DepronXPS = Depron (XPS)\r
+Databases.materials.Fiberglass = Glasfaser\r
+Databases.materials.Kraftphenolic = Pertinax\r
+Databases.materials.Maple = Ahorn\r
+Databases.materials.Paperoffice = Papier (Büro)\r
+Databases.materials.Pine = Kiefer\r
+Databases.materials.Plywoodbirch = Sperrholz (Birke)\r
+Databases.materials.PolycarbonateLexan = Polycarbonat (Lexan)\r
+Databases.materials.Polystyrene = Polystyrène\r
+Databases.materials.PVC = PVC\r
+Databases.materials.Spruce = Fichte\r
+Databases.materials.StyrofoamgenericEPS = Styropor (EPS)\r
+Databases.materials.StyrofoamBluefoamXPS = Styrodur (XPS)\r
+Databases.materials.Quantumtubing = Quantum tubing\r
+Databases.materials.BlueTube = Blue tube\r
+!SURFACE_MATERIAL\r
+Databases.materials.Ripstopnylon = Ripstop Nylon\r
+Databases.materials.Mylar = Mylar\r
+Databases.materials.Polyethylenethin = Polyethylen (dünn)\r
+Databases.materials.Polyethyleneheavy = Polyethylen (schwer)\r
+Databases.materials.Silk = Seide\r
+Databases.materials.Paperoffice = Papier (Büro)\r
+Databases.materials.Cellophane = Zellophan\r
+Databases.materials.Crepepaper = Krepppapier\r
+! LINE_MATERIAL\r
+Databases.materials.Threadheavy-duty = Faden (stark)\r
+Databases.materials.Elasticcordround2mm = Elastikband (rund, 2mm, 1/16 in)\r
+Databases.materials.Elasticcordflat6mm = Elastikband (flach, 6mm, 1/4 in)\r
+Databases.materials.Elasticcordflat12mm = Elastikband (flach, 12mm, 1/2 in)\r
+Databases.materials.Elasticcordflat19mm = Elastikband (flach, 19mm, 3/4 in)\r
+Databases.materials.Elasticcordflat25mm = Elastikband (flach, 25mm, 1 in)\r
+Databases.materials.Braidednylon2mm = Nylonflachband (2 mm, 1/16 in)\r
+Databases.materials.Braidednylon3mm = Nylonflachband (3 mm, 1/8 in)\r
+Databases.materials.Tubularnylon11mm = Tubular Nylon (11 mm, 7/16 in)\r
+Databases.materials.Tubularnylon14mm = Tubular Nylon (14 mm, 9/16 in)\r
+Databases.materials.Tubularnylon25mm = Tubular Nylon (25 mm, 1 in)\r
+\r
+! ExternalComponent\r
+ExternalComponent.Rough = Rau\r
+ExternalComponent.Unfinished = unbehandelt\r
+ExternalComponent.Regularpaint = normale Farbe\r
+ExternalComponent.Smoothpaint = glatte Farbe\r
+ExternalComponent.Polished = poliert\r
+\r
+! LineStyle\r
+LineStyle.Solid = durchgehend\r
+LineStyle.Dashed = gestrichelt\r
+LineStyle.Dotted = gepunktet\r
+LineStyle.Dash-dotted = Strich-Punkt\r
+LineStyle.Defaultstyle = Standardstil\r
+\r
+! Shape\r
+Shape.Conical = Konisch\r
+Shape.Conical.desc1 = Eine konische Spitze hat ein dreieckiges Profil\r
+Shape.Conical.desc2 = Ein konischer Übergang hat gerade Kanten\r
+Shape.Ogive = Ogive\r
+Shape.Ogive.desc1 = Eine ogive Spitze hat das Profil eines Kreissegments. Der Formparamter 1 erzeugt eine <b>tangentiale Ogive</b>, die einen weichen Übergang zum Körperrohr hat, Werte kleiner 1 erzeugen eine <b>sekante Ogive<b>.\r
+Shape.Ogive.desc2 = Eine ogive Spitze hat das Profil eines Kreissegments. Der Formparamter 1 erzeugt eine <b>tangentiale Ogive</b>, die einen weichen Übergang zum Körperrohr am hinteren Ende hat, Werte kleiner 1 erzeugen eine <b>sekante Ogive<b>.\r
+Shape.Ellipsoid = Ellipsoid\r
+Shape.Ellipsoid.desc1 = Eine ellipsoide Spitze hat ein Profil einer Halbellipse mit der einer Hauptachsenlänge von 2×<i>Länge</i> und <i>Durchmesser</i> \r
+Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>. If the transition is not clipped, then the profile is extended at the center by the corresponding radius. \r
+Shape.Powerseries = Power series\r
+Shape.Powerseries.desc1 = A power series nose cone has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 this is a <b>\u00BD-power</b> or <b>parabolic</b> nose cone, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 a <b>conical</b> nose cone.\r
+Shape.Powerseries.desc2 = A power series transition has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 the transition is <b>\u00BD-power</b> or <b>parabolic</b>, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 <b>conical</b>.\r
+Shape.Parabolicseries = Parabolic series\r
+Shape.Parabolicseries.desc1 = A parabolic series nose cone has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> nose cone.\r
+Shape.Parabolicseries.desc2 = A parabolic series transition has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube at the aft end, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> transition.\r
+Shape.Haackseries = Haack series\r
+Shape.Haackseries.desc1 = The Haack series nose cones are designed to minimize drag. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> nose cone, which minimizes drag for fixed length and diameter, while a value of 0.333 produces an <b>LV-Haack</b> nose cone, which minimizes drag for fixed length and volume.\r
+Shape.Haackseries.desc2 = The Haack series <i>nose cones</i> are designed to minimize drag. These transition shapes are their equivalents, but do not necessarily produce optimal drag for transitions. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> shape, while a value of 0.333 produces an <b>LV-Haack</b> shape. \r
+\r
+\r
+! RocketComponent\r
+RocketComponent.Position.TOP = oberes Ende der übergeordneten Komponente\r
+RocketComponent.Position.MIDDLE = Mitte der übergeordneten Komponente\r
+RocketComponent.Position.BOTTOM = unteres Ende der übergeordneten Komponente\r
+RocketComponent.Position.AFTER = nach der übergeordneten Komponente\r
+RocketComponent.Position.ABSOLUTE = zur Spitze\r
+\r
+! LaunchLug\r
+LaunchLug.Launchlug = Leitröhrchen\r
+! NoseCone\r
+NoseCone.NoseCone = Spitze\r
+! Transition\r
+Transition.Transition = Übergang\r
+!Stage\r
+Stage.Stage = Stufe\r
+! BodyTube\r
+BodyTube.BodyTube = Körperrohr\r
+! TubeCoupler\r
+TubeCoupler.TubeCoupler = Koppler\r
+!InnerTube\r
+InnerTube.InnerTube = Innenrohr\r
+! TrapezoidFinSet\r
+TrapezoidFinSet.TrapezoidFinSet = Trapezoide Leitwerke\r
+! FreeformFinSet\r
+FreeformFinSet.FreeformFinSet = Frei geformte Leitwerke\r
+!MassComponent\r
+MassComponent.MassComponent = Masse\r
+! Parachute\r
+Parachute.Parachute = Fallschirm\r
+! ShockCord\r
+ShockCord.ShockCord = Gummiband\r
+! Bulkhead\r
+Bulkhead.Bulkhead = Schott\r
+\r
+!Rocket\r
+Rocket.motorCount.Nomotor = [Keine Motoren]\r
+Rocket.compname.Rocket = Rakete\r
+\r
+!MotorMount\r
+MotorMount.IgnitionEvent.AUTOMATIC = Automatisch (Start oder Ausstoßladung)\r
+MotorMount.IgnitionEvent.LAUNCH = Start\r
+MotorMount.IgnitionEvent.EJECTION_CHARGE = Erste Ausstoßladung der vorherigen Stufe\r
+MotorMount.IgnitionEvent.BURNOUT = Erster Brennschluss der vorherigen Stufe\r
+MotorMount.IgnitionEvent.NEVER = Nie\r
+\r
+!ComponentIcons \r
+ComponentIcons.Nosecone = Spitze\r
+ComponentIcons.Bodytube = Körperrohr\r
+ComponentIcons.Transition = Übergang\r
+ComponentIcons.Trapezoidalfinset = Trapezoide Leitwerke\r
+ComponentIcons.Ellipticalfinset = Elliptische Leitwerke\r
+ComponentIcons.Freeformfinset = Frei geformte Leitwerke\r
+ComponentIcons.Launchlug = Leitröhrchen\r
+ComponentIcons.Innertube = Innenrohr\r
+ComponentIcons.Tubecoupler = Koppler\r
+ComponentIcons.Centeringring = Zentrierring\r
+ComponentIcons.Bulkhead = Schott\r
+ComponentIcons.Engineblock = Motorhalterung\r
+ComponentIcons.Parachute = Fallschirm\r
+ComponentIcons.Streamer = Strömer\r
+ComponentIcons.Shockcord = Gummiband\r
+ComponentIcons.Masscomponent = Masse\r
+ComponentIcons.disabled = (deaktiviert)\r
+\r
+! StageAction\r
+StageAction.Stage = Stufe\r
+\r
+! RecoveryDevice\r
+RecoveryDevice.DeployEvent.LAUNCH = Start (plus NN Sekunden)\r
+RecoveryDevice.DeployEvent.EJECTION = Erste Ausstoßladung dieser Stufe\r
+RecoveryDevice.DeployEvent.APOGEE = Apogäum\r
+RecoveryDevice.DeployEvent.ALTITUDE = Spezifische Höhe während der Landephase\r
+RecoveryDevice.DeployEvent.NEVER = Nie\r
+\r
+! FlightEvent\r
+FlightEvent.Type.LAUNCH = Start\r
+FlightEvent.Type.IGNITION = Motorzündung\r
+FlightEvent.Type.LIFTOFF = Abheben\r
+FlightEvent.Type.LAUNCHROD = Verlassen der Startrampe\r
+FlightEvent.Type.BURNOUT = Motorbrennschluss\r
+FlightEvent.Type.EJECTION_CHARGE = Ausstoßladung\r
+FlightEvent.Type.STAGE_SEPARATION = Stufentrennung\r
+FlightEvent.Type.APOGEE = Apogäum\r
+FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Auslösung des Bergungssystems\r
+FlightEvent.Type.GROUND_HIT = Landung\r
+FlightEvent.Type.SIMULATION_END = Ende der Simulation\r
+FlightEvent.Type.ALTITUDE = Höhenänderung\r
+\r
+! ThrustCurveMotorColumns\r
+TCurveMotorCol.MANUFACTURER = Hersteller\r
+TCurveMotorCol.DESIGNATION = Bezeichnung\r
+TCurveMotorCol.TYPE = Typ\r
+TCurveMotorCol.DIAMETER = Durchmesser\r
+TCurveMotorCol.LENGTH = Länge\r
+\r
+! RocketInfo\r
+RocketInfo.lengthLine.Length = Länge\r
+RocketInfo.lengthLine.maxdiameter = , max. Durchmesser\r
+RocketInfo.massText1 = Masse mit Motoren\r
+RocketInfo.massText2 = Masse ohne Motoren\r
+RocketInfo.at = bei M=\r
+RocketInfo.cgText = CG:\r
+RocketInfo.cpText = CP:\r
+RocketInfo.stabText = Stabilität:\r
+RocketInfo.Warning = Warnung:\r
+RocketInfo.Calculating = Berechne...\r
+RocketInfo.Apogee = Apogäum:\r
+RocketInfo.Maxvelocity = max. Geschwindigkeit:\r
+RocketInfo.Maxacceleration = max. Beschleunigung:\r
+RocketInfo.apogeeValue = N/A\r
+RocketInfo.Mach = (Mach\r
+RocketInfo.velocityValue = N/A\r
+RocketInfo.accelerationValue = N/A\r
+\r
+! FinSet\r
+FinSet.CrossSection.SQUARE = Quadrat\r
+FinSet.CrossSection.ROUNDED = Abgerundet\r
+FinSet.CrossSection.AIRFOIL = Tragfläche\r
+FinSet.TabRelativePosition.FRONT = Root chord leading edge\r
+FinSet.TabRelativePosition.CENTER = Root chord midpoint\r
+FinSet.TabRelativePosition.END = Root chord trailing edge\r
+\r
+! FlightDataType\r
+FlightDataType.TYPE_TIME = Zeit\r
+FlightDataType.TYPE_ALTITUDE = Höhe\r
+FlightDataType.TYPE_VELOCITY_Z = Vertikalgeschwindigkeit\r
+FlightDataType.TYPE_ACCELERATION_Z = Vertikalbeschleunigung\r
+FlightDataType.TYPE_VELOCITY_TOTAL = Gesamtgeschwindigkeit\r
+FlightDataType.TYPE_ACCELERATION_TOTAL = Gesamtbeschleunigung\r
+FlightDataType.TYPE_POSITION_X = Position upwind\r
+FlightDataType.TYPE_POSITION_Y = Position parallel to wind\r
+FlightDataType.TYPE_POSITION_XY = Lateral distance\r
+FlightDataType.TYPE_POSITION_DIRECTION = Lateral direction\r
+FlightDataType.TYPE_VELOCITY_XY = Lateral velocity\r
+FlightDataType.TYPE_ACCELERATION_XY = Lateral acceleration\r
+FlightDataType.TYPE_AOA = Angriffswinkel\r
+FlightDataType.TYPE_ROLL_RATE = Rollrate\r
+FlightDataType.TYPE_PITCH_RATE = Nickrate\r
+FlightDataType.TYPE_YAW_RATE = Gierrate\r
+FlightDataType.TYPE_MASS = Masse\r
+FlightDataType.TYPE_LONGITUDINAL_INERTIA = Longitudinal moment of inertia\r
+FlightDataType.TYPE_ROTATIONAL_INERTIA = Rotational moment of inertia\r
+FlightDataType.TYPE_CP_LOCATION = Position vom CP\r
+FlightDataType.TYPE_CG_LOCATION = Position vom CG\r
+FlightDataType.TYPE_STABILITY = Stabilität in Kalibern\r
+FlightDataType.TYPE_MACH_NUMBER = Machzahl\r
+FlightDataType.TYPE_REYNOLDS_NUMBER = Reynoldszahl\r
+FlightDataType.TYPE_THRUST_FORCE = Schub\r
+FlightDataType.TYPE_DRAG_FORCE = Luftwiderstandskraft\r
+FlightDataType.TYPE_DRAG_COEFF = Luftwiderstandskoeffizient\r
+FlightDataType.TYPE_AXIAL_DRAG_COEFF = Axial drag coefficient\r
+FlightDataType.TYPE_FRICTION_DRAG_COEFF = Reibungskoeffizient\r
+FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Pressure drag coefficient\r
+FlightDataType.TYPE_BASE_DRAG_COEFF = Base drag coefficient\r
+FlightDataType.TYPE_NORMAL_FORCE_COEFF = Normal force coefficient\r
+FlightDataType.TYPE_PITCH_MOMENT_COEFF = Pitch moment coefficient\r
+FlightDataType.TYPE_YAW_MOMENT_COEFF = Yaw moment coefficient\r
+FlightDataType.TYPE_SIDE_FORCE_COEFF = Side force coefficient\r
+FlightDataType.TYPE_ROLL_MOMENT_COEFF = Roll moment coefficient\r
+FlightDataType.TYPE_ROLL_FORCING_COEFF = Roll forcing coefficient\r
+FlightDataType.TYPE_ROLL_DAMPING_COEFF = Roll damping coefficient\r
+FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Pitch damping coefficient\r
+FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Yaw damping coefficient\r
+FlightDataType.TYPE_REFERENCE_LENGTH = Referenzlänge\r
+FlightDataType.TYPE_REFERENCE_AREA = Referenzfläche\r
+FlightDataType.TYPE_ORIENTATION_THETA = Vertical orientation (zenith)\r
+FlightDataType.TYPE_ORIENTATION_PHI = Lateral orientation (azimuth)\r
+FlightDataType.TYPE_WIND_VELOCITY = Windgeschwindigkeit\r
+FlightDataType.TYPE_AIR_TEMPERATURE = Lufttemperatur\r
+FlightDataType.TYPE_AIR_PRESSURE = Luftdruck\r
+FlightDataType.TYPE_SPEED_OF_SOUND = Schallgeschwindigkeit\r
+FlightDataType.TYPE_TIME_STEP = Simulationsintervall\r
+FlightDataType.TYPE_COMPUTATION_TIME = Berechnnungszeit\r
+FlightDataType.TYPE_LATITUDE = Latitude\r
+FlightDataType.TYPE_LONGITUDE = Longitude\r
+FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration\r
+\r
+! PlotConfiguration\r
+PlotConfiguration.Verticalmotion = Vertikale Bewegung über Zeit\r
+PlotConfiguration.Totalmotion = Gesamte Bewegung über Zeit\r
+PlotConfiguration.Flightside = Flight side profile\r
+PlotConfiguration.Stability = Stabilität über Zeit\r
+PlotConfiguration.Dragcoef = Drag coefficients vs. Mach number\r
+PlotConfiguration.Rollcharacteristics = Roll characteristics\r
+PlotConfiguration.Angleofattack = Angle of attack and orientation vs. time\r
+PlotConfiguration.Simulationtime = Simulationszeitschritt und Berechnungszeit\r
+\r
+! Warning\r
+Warning.LargeAOA.str1 = Large angle of attack encountered.\r
+Warning.LargeAOA.str2 = Large angle of attack encountered (\r
+Warning.DISCONTINUITY = Unstetigkeit im Raketendurchmesser\r
+Warning.THICK_FIN = Dicke Leitwerke können nicht präzise modelliert werden.\r
+Warning.JAGGED_EDGED_FIN = Gezackte Ecken in Leitwerken können unpräzise Ergebnisse liefern.\r
+Warning.LISTENERS_AFFECTED = Simulationsempfänger haben die Simulation beeinflusst.\r
+Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Bergungssystem wurde ausgelöst während der Motor noch gebrannt hat.\r
+Warning.FILE_INVALID_PARAMETER = Ignoriere ungültigen Parameter.\r
+\r
+\r
+! Scale dialog\r
+ScaleDialog.lbl.scaleRocket = Entire rocket\r
+ScaleDialog.lbl.scaleSubselection = Selection and all subcomponents\r
+ScaleDialog.lbl.scaleSelection = Only selected component\r
+ScaleDialog.title = Scale design\r
+ScaleDialog.lbl.scale = Scale:\r
+ScaleDialog.lbl.scale.ttip = Select whether to scale the entire design or only the selected component\r
+ScaleDialog.lbl.scaling = Scaling to apply:\r
+ScaleDialog.lbl.scaling.ttip = Resulting size, values above 100% grow and values below 100% shrink the design.\r
+! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"\r
+ScaleDialog.lbl.scaleFrom = Scale from\r
+ScaleDialog.lbl.scaleTo = to\r
+ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and resulting length.\r
+ScaleDialog.checkbox.scaleMass = Update explicit mass values\r
+ScaleDialog.checkbox.scaleMass.ttip = Scale mass component and override mass values by the cube of the scaling factor\r
+ScaleDialog.button.scale = Scale\r
+ScaleDialog.undo.scaleRocket = Scale rocket\r
+ScaleDialog.undo.scaleComponent = Scale component\r
+ScaleDialog.undo.scaleComponents = Scale components\r
+\r
+!icons\r
+Icons.Undo = Undo\r
+Icons.Redo = Redo\r
+\r
+OpenRocketPrintable.Partsdetail = Parts detail\r
+OpenRocketPrintable.Fintemplates = Fin templates\r
+OpenRocketPrintable.DesignReport = Design Report\r
+\r
+OpenRocketDocument.Redo = Redo\r
+OpenRocketDocument.Undo = Undo\r
+\r
+!EllipticalFinSet\r
+EllipticalFinSet.Ellipticalfinset = Elliptical fin set\r
+\r
+! Optimization\r
+\r
+! Modifiers\r
+\r
+optimization.modifier.nosecone.length = Length\r
+optimization.modifier.nosecone.length.desc = Optimize the nose cone length.\r
+optimization.modifier.nosecone.diameter = Diameter\r
+optimization.modifier.nosecone.diameter.desc = Optimize the nose cone base diameter.\r
+optimization.modifier.nosecone.thickness = Thickness\r
+optimization.modifier.nosecone.thickness.desc = Optimize the nose cone wall thickness.\r
+optimization.modifier.nosecone.shapeparameter = Shape parameter\r
+optimization.modifier.nosecone.shapeparameter.desc = Optimize the nose cone shape parameter.\r
+\r
+optimization.modifier.transition.length = Length\r
+optimization.modifier.transition.length.desc = Optimize the transition length.\r
+optimization.modifier.transition.forediameter = Fore diameter\r
+optimization.modifier.transition.forediameter.desc = Optimize the transition fore diameter.\r
+optimization.modifier.transition.aftdiameter = Aft diameter\r
+optimization.modifier.transition.aftdiameter.desc = Optimize the transition aft diameter.\r
+optimization.modifier.transition.thickness = Thickness\r
+optimization.modifier.transition.thickness.desc = Optimize the transition wall thickness.\r
+optimization.modifier.transition.shapeparameter = Shape parameter\r
+optimization.modifier.transition.shapeparameter.desc = Optimize the transition shape parameter.\r
+\r
+optimization.modifier.bodytube.length = Length\r
+optimization.modifier.bodytube.length.desc = Optimize the body tube length.\r
+optimization.modifier.bodytube.outerDiameter = Outer diameter\r
+optimization.modifier.bodytube.outerDiameter.desc = Optimize the body tube outer diameter while maintaining the wall thickness.\r
+optimization.modifier.bodytube.thickness = Thickness\r
+optimization.modifier.bodytube.thickness.desc = Optimize the body tube wall thickness.\r
+\r
+optimization.modifier.trapezoidfinset.rootChord = Root chord\r
+optimization.modifier.trapezoidfinset.rootChord.desc = Optimize the root chord length of the fin set (length of fin at the rocket body).\r
+optimization.modifier.trapezoidfinset.tipChord = Tip chord\r
+optimization.modifier.trapezoidfinset.tipChord.desc = Optimize the tip chord length of the fin set (length of fin at outer edge).\r
+optimization.modifier.trapezoidfinset.sweep = Sweep\r
+optimization.modifier.trapezoidfinset.sweep.desc = Optimize the sweep of the fin set (distance that the leading edge sweeps backwards).\r
+optimization.modifier.trapezoidfinset.height = Height\r
+optimization.modifier.trapezoidfinset.height.desc = Optimize the height (semi-span) of the fin set.\r
+\r
+optimization.modifier.ellipticalfinset.length = Root chord\r
+optimization.modifier.ellipticalfinset.length.desc = Optimize the root chord length of the fin set.\r
+optimization.modifier.ellipticalfinset.height = Height\r
+optimization.modifier.ellipticalfinset.height.desc = Optimize the height (semi-span) of the fin set.\r
+\r
+optimization.modifier.finset.cant = Cant angle\r
+optimization.modifier.finset.cant.desc = Optimize the cant angle of the fin set.\r
+optimization.modifier.finset.position = Position\r
+optimization.modifier.finset.position.desc = Optimize the fin set position along the rocket body.\r
+\r
+optimization.modifier.launchlug.length = Length\r
+optimization.modifier.launchlug.length.desc = Optimize the launch lug length.\r
+optimization.modifier.launchlug.outerDiameter = Outer diameter\r
+optimization.modifier.launchlug.outerDiameter.desc = Optimize the outer diameter of the launch lug.\r
+optimization.modifier.launchlug.thickness = Thickness\r
+optimization.modifier.launchlug.thickness.desc = Optimize the launch lug thickness while keeping the outer diameter constant.\r
+optimization.modifier.launchlug.position = Position\r
+optimization.modifier.launchlug.position.desc = Optimize the launch lug position along the rocket body.\r
+\r
+\r
+optimization.modifier.internalcomponent.position = Position\r
+optimization.modifier.internalcomponent.position.desc = Optimize the position of the component relative to the parent component.\r
+\r
+optimization.modifier.masscomponent.mass = Mass\r
+optimization.modifier.masscomponent.mass.desc = Optimize the mass of the mass component.\r
+\r
+optimization.modifier.parachute.diameter = Diameter\r
+optimization.modifier.parachute.diameter.desc = Optimize the parachute canopy diameter.\r
+optimization.modifier.parachute.coefficient = Drag coefficient\r
+optimization.modifier.parachute.coefficient.desc = Optimize the drag coefficient of the parachute. Typical parachutes have a drag coefficient of about 0.8.\r
+\r
+optimization.modifier.streamer.length = Length\r
+optimization.modifier.streamer.length.desc = Optimize the length of the streamer.\r
+optimization.modifier.streamer.width = Width\r
+optimization.modifier.streamer.width.desc = Optimize the width of the streamer.\r
+optimization.modifier.streamer.aspectRatio = Aspect ratio\r
+optimization.modifier.streamer.aspectRatio.desc = Optimize the aspect ratio of the streamer (length/width). You should NOT select streamer length or width at the same time with the aspect ratio.\r
+optimization.modifier.streamer.coefficient = Drag coefficient\r
+optimization.modifier.streamer.coefficient.desc = Optimize the drag coefficient of the streamer.\r
+\r
+optimization.modifier.recoverydevice.deployDelay = Deployment delay\r
+optimization.modifier.recoverydevice.deployDelay.desc = Optimize the deployment delay of the recovery device.\r
+optimization.modifier.recoverydevice.deployAltitude = Deployment altitude\r
+optimization.modifier.recoverydevice.deployAltitude.desc = Optimize the deployment altitude of the recovery device.\r
+\r
+optimization.modifier.rocketcomponent.overrideMass = Override mass\r
+optimization.modifier.rocketcomponent.overrideMass.desc = Optimize the overridden mass of the component.\r
+optimization.modifier.rocketcomponent.overrideCG = Override CG\r
+optimization.modifier.rocketcomponent.overrideCG.desc = Optimize the overridden center of gravity of the component.\r
+\r
+optimization.modifier.motormount.overhang = Motor overhang\r
+optimization.modifier.motormount.overhang.desc = Optimize the motor overhang.\r
+optimization.modifier.motormount.delay = Motor ignition delay\r
+optimization.modifier.motormount.delay.desc = Optimize the motor ignition delay.\r
+\r
+\r
+\r
+\r
+! General rocket design optimization dialog\r
+\r
+GeneralOptimizationDialog.title = Rocket optimization\r
+GeneralOptimizationDialog.goal.maximize = Maximize value\r
+GeneralOptimizationDialog.goal.minimize = Minimize value\r
+GeneralOptimizationDialog.goal.seek = Seek value of\r
+GeneralOptimizationDialog.btn.start = Start optimization\r
+GeneralOptimizationDialog.btn.stop = Stop optimization\r
+GeneralOptimizationDialog.lbl.paramsToOptimize = Parameters to optimize:\r
+GeneralOptimizationDialog.btn.add = Add\r
+GeneralOptimizationDialog.btn.add.ttip = Add the selected parameter to the optimization\r
+GeneralOptimizationDialog.btn.remove = Remove\r
+GeneralOptimizationDialog.btn.remove.ttip = Remove the selected parameter from the optimization\r
+GeneralOptimizationDialog.btn.removeAll = Remove all\r
+GeneralOptimizationDialog.btn.removeAll.ttip = Remove all parameters from the optimization\r
+GeneralOptimizationDialog.lbl.availableParams = Available parameters:\r
+GeneralOptimizationDialog.lbl.optimizationOpts = Optimization options\r
+GeneralOptimizationDialog.lbl.optimizeSim = Optimize simulation:\r
+GeneralOptimizationDialog.lbl.optimizeSim.ttip = Select which simulation to optimize\r
+GeneralOptimizationDialog.lbl.optimizeValue = Optimized value:\r
+GeneralOptimizationDialog.lbl.optimizeValue.ttip = Select what value is to be optimized\r
+GeneralOptimizationDialog.lbl.optimizeGoal = Optimization goal:\r
+GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Select the goal of the optimization\r
+GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Custom value to seek\r
+GeneralOptimizationDialog.lbl.requireStability = Required stability\r
+GeneralOptimizationDialog.lbl.requireMinStability = Minimum stability:\r
+GeneralOptimizationDialog.lbl.requireMinStability.ttip = Require a minimum static stability margin for the design\r
+GeneralOptimizationDialog.lbl.requireMaxStability = Maximum stability:\r
+GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Require a maximum static stability margin for the design\r
+GeneralOptimizationDialog.status.bestValue = Best value:\r
+GeneralOptimizationDialog.status.bestValue.ttip = Best optimization value found so far.\r
+GeneralOptimizationDialog.status.stepCount = Step count:\r
+GeneralOptimizationDialog.status.stepCount.ttip = Number of optimization steps that have been performed.\r
+GeneralOptimizationDialog.status.evalCount = Evaluations:\r
+GeneralOptimizationDialog.status.evalCount.ttip = Total number of function evaluations (simulations) that have been performed.\r
+GeneralOptimizationDialog.status.stepSize = Step size:\r
+GeneralOptimizationDialog.status.stepSize.ttip = Current optimization step size (relative to the optimization parameter ranges)\r
+GeneralOptimizationDialog.btn.plotPath = Plot path\r
+GeneralOptimizationDialog.btn.plotPath.ttip = Plot the optimization path (one and two dimensional optimization only)\r
+GeneralOptimizationDialog.btn.save = Save path\r
+GeneralOptimizationDialog.btn.save.ttip = Save the results of the function evaluations (simulations) as a CSV file.\r
+GeneralOptimizationDialog.btn.apply = Apply optimization\r
+GeneralOptimizationDialog.btn.apply.ttip = Apply the optimization results to the rocket design\r
+GeneralOptimizationDialog.btn.reset = Reset\r
+GeneralOptimizationDialog.btn.reset.ttip = Reset the rocket design to the current rocket design\r
+GeneralOptimizationDialog.btn.close = Close\r
+GeneralOptimizationDialog.btn.close.ttip = Close the dialog without modifying the rocket design\r
+GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters.\r
+GeneralOptimizationDialog.error.selectParams.title = Select optimization parameters\r
+GeneralOptimizationDialog.error.optimizationFailure.text = The optimization failed to run:\r
+GeneralOptimizationDialog.error.optimizationFailure.title = Optimization failed\r
+GeneralOptimizationDialog.undoText = Apply optimization\r
+GeneralOptimizationDialog.basicSimulationName = Basic simulation\r
+GeneralOptimizationDialog.noSimulationName = No simulation\r
+GeneralOptimizationDialog.table.col.parameter = Parameter\r
+GeneralOptimizationDialog.table.col.current = Current\r
+GeneralOptimizationDialog.table.col.min = Minimum\r
+GeneralOptimizationDialog.table.col.max = Maximum\r
+GeneralOptimizationDialog.export.header = Include header line\r
+GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions.\r
+GeneralOptimizationDialog.export.stability = Stability\r
+\r
+\r
+! Dialog for plotting optimization results\r
+OptimizationPlotDialog.title = Optimization results\r
+OptimizationPlotDialog.lbl.zoomInstructions = Click and drag down+right to zoom in, up+left to zoom out\r
+OptimizationPlotDialog.plot1d.title = Optimization result\r
+OptimizationPlotDialog.plot1d.series = Optimization result\r
+OptimizationPlotDialog.plot2d.title = Optimization path\r
+OptimizationPlotDialog.plot2d.path = Optimization path\r
+OptimizationPlotDialog.plot2d.evals = Evaluations\r
+OptimizationPlotDialog.plot.ttip.stability = Stability:\r
+OptimizationPlotDialog.plot.label.optimum = Optimum\r
+\r
+! Optimization parameters\r
+MaximumAltitudeParameter.name = Apogee altitude\r
+MaximumVelocityParameter.name = Maximum velocity\r
+MaximumAccelerationParameter.name = Maximum acceleration\r
+StabilityParameter.name = Stability\r
+GroundHitVelocityParameter.name = Ground hit speed\r
+LandingDistanceParameter.name = Landing distance\r
+TotalFlightTimeParameter.name = Total flight time\r
+DeploymentVelocityParameter.name = Velocity at parachute deployment\r
+\r
+\r
+! Compass directions drawn on a compass rose.\r
+CompassRose.lbl.north = N\r
+CompassRose.lbl.east = E\r
+CompassRose.lbl.south = S\r
+CompassRose.lbl.west = W\r
+\r
+! Compass directions with subdirections. These might not be localized even if the directions on the compass rose are.\r
+CompassSelectionButton.lbl.N = N\r
+CompassSelectionButton.lbl.NE = NE\r
+CompassSelectionButton.lbl.E = E\r
+CompassSelectionButton.lbl.SE = SE\r
+CompassSelectionButton.lbl.S = S\r
+CompassSelectionButton.lbl.SW = SW\r
+CompassSelectionButton.lbl.W = W\r
+CompassSelectionButton.lbl.NW = NW\r
+\r
+\r
+SlideShowDialog.btn.next = Next\r
+SlideShowDialog.btn.prev = Previous\r
+\r
+GuidedTourSelectionDialog.title = Guided tours\r
+GuidedTourSelectionDialog.lbl.selectTour = Select guided tour:\r
+GuidedTourSelectionDialog.lbl.description = Tour description:\r
+GuidedTourSelectionDialog.lbl.length = Number of slides:\r
+GuidedTourSelectionDialog.btn.start = Start tour!\r
--- /dev/null
+#
+# Spanish base translation file
+# translations provided by Tripoli Spain
+#
+# Should you need to add new logical keys here is the proposed method
+#
+# className.ComponantType.componantName
+#
+#
+# Text tokens within braces should not be translated, e.g.
+# "The file '{filename}' exists."
+# They are pieces that are inserted dynamically.
+#
+
+
+! Set to the name of the current translation file (used for debugging purposes)
+debug.currentFile = messages_es.properties
+
+! RocketActions
+RocketActions.checkbox.Donotaskmeagain = No volver a preguntarme
+RocketActions.lbl.Youcanchangedefop = Puede modificar la operación por defecto con sus preferencias
+RocketActions.showConfirmDialog.lbl1 = ¿Borrar las simulaciones seleccionadas?
+RocketActions.showConfirmDialog.lbl2 = <html><i>Esta operación no puede deshacerse.</i>
+RocketActions.showConfirmDialog.title = Borrar simulaciones
+RocketActions.DelCompAct.Delete = Borrar
+RocketActions.DelCompAct.ttip.Delete = Borrar el componente seleccionado
+RocketActions.DelSimuAct.Delete = Borrar
+RocketActions.DelSimuAct.ttip.Delete = Borrar la simulación seleccionada
+RocketActions.DelAct.Delete = Borrar
+RocketActions.DelAct.ttip.Delete = Eliminar elemento seleccionado
+RocketActions.CutAction.Cut = Cortar
+RocketActions.CutAction.ttip.Cut = Quitar y copiar al portapapeles
+RocketActions.CopyAct.Copy = Copiar
+RocketActions.CopyAct.ttip.Copy = Copiar al portapapeles
+RocketActions.PasteAct.Paste = Pegar
+RocketActions.PasteAct.ttip.Paste = Pegar al portapapeles
+RocketActions.EditAct.Edit = Editar componente
+RocketActions.EditAct.ttip.Edit = Editar valores del componente seleccionado
+RocketActions.NewStageAct.Newstage = Nueva etapa
+RocketActions.NewStageAct.ttip.Newstage = Añadir una nueva etapa al diseño del cohete
+RocketActions.ActBoosterstage = Etapa booster
+RocketActions.MoveUpAct.Moveup = Mover hacia arriba
+RocketActions.MoveUpAct.ttip.Moveup = Mover este componente hacia arriba
+RocketActions.MoveDownAct.Movedown = Mover hacia abajo
+RocketActions.MoveDownAct.ttip.Movedown = Mover este componente hacia abajo
+
+! RocketPanel
+RocketPanel.FigTypeAct.Sideview = Vista lateral
+RocketPanel.FigTypeAct.ttip.Sideview = Vista desde un lateral
+RocketPanel.FigTypeAct.Backview = Vista trasera
+RocketPanel.FigTypeAct.ttip.Backview = Vista desde atrás
+RocketPanel.lbl.Motorcfg = Configuración del motor
+RocketPanel.lbl.infoMessage = <html>Click para seleccionar Mayúsculas+click para seleccionar otro Doble-click para mostrar Click+arrastrar para mover
+
+! BasicFrame
+BasicFrame.SimpleFileFilter1 = Todos los diseños de cohete(*.ork; *.rkt)
+BasicFrame.SimpleFileFilter2 = Diseños OpenRocket (*.ork)
+BasicFrame.SimpleFileFilter3 = Diseños RockSim (*.rkt)
+BasicFrame.tab.Rocketdesign = Diseño del cohete
+BasicFrame.tab.Flightsim = Simulaciones de vuelo
+BasicFrame.title.Addnewcomp = Añadir un nuevo componente
+!BasicFrame.item.Openrocketdesign = Abrir un diseño de cohete
+!BasicFrame.item.Openexamplerocketdesign = Abrir un ejemplo de diseño de cohete
+!BasicFrame.item.SavecurRocketdesign = Guardar el diseño actual
+!BasicFrame.item.SavecurRocketdesnewfile = Guardar el diseño actual como un nuevo documento
+!BasicFrame.item.Printpart = Imprimir un listado de componentes y un esquema de aleta
+!BasicFrame.item.Closedesign = Cerrar el diseño actual
+!BasicFrame.item.Quitprogram = Abandonar el programa
+!BasicFrame.menu.Rocketedt = Mostrando el cohete
+BasicFrame.dlg.lbl1 = Diseño
+BasicFrame.dlg.lbl2 = No se ha guardado
+BasicFrame.dlg.lbl3 = ¿Quiere guardarlo?
+BasicFrame.dlg.title = Diseño no guardado
+BasicFrame.StageName.Sustainer = Etapa principal
+BasicFrame.WarningDialog.txt1 = Mientras se abría, se encontraron los siguiente problemas
+BasicFrame.WarningDialog.txt2 = Algunas configuraciones de diseño no pudieron cargarse correctamente.
+BasicFrame.WarningDialog.title = Precauciones mientras se abre el archivo
+
+
+! General error messages used in multiple contexts
+error.fileExists.title = El archivo ya existe
+error.fileExists.desc = El archivo con el nombre '{filename}' ya existe. ¿Desea sobrescribir la versión anterior?
+
+error.writing.title = Error al guardar el archivo
+error.writing.desc = Ha ocurrido un error al guardar el archivo:
+
+
+! Labels used in buttons of dialog windows
+# TODO: Rename these to "btn.xxx"
+button.ok = OK
+button.cancel = Cancelar
+button.close = Cerrar
+
+! Common labels used in buttons of dialog windows
+dlg.but.ok = OK
+dlg.but.cancel = Cancelar
+dlg.but.close = Cerrar
+
+! General file type names
+filetypes.pdf = Archivos PDF
+
+
+! About Dialog
+AboutDialog.lbl.version = Versión
+! The texts below provide additional credits for the translation maintainer
+! - In AboutDialog.lbl.translation replace "English" with the current language.
+! - AboutDialog.lbl.translator is the translator / group name (may be empty)
+! - AboutDialog.lbl.translatorWebsite is a URL to the translator / group (may be empty)
+! - AboutDialog.lbl.translatorIcon is the file name of an icon under pix/translators/ (may be empty)
+AboutDialog.lbl.translation = Traducido al español por:
+AboutDialog.lbl.translator = Tripoli Spain
+AboutDialog.lbl.translatorWebsite = http://www.tripoli-spain.org/
+AboutDialog.lbl.translatorIcon = logoTripoliSpain.png
+
+
+! Print dialog
+PrintDialog.title = Imprimir o exportar
+PrintDialog.but.previewAndPrint = Vista previa e Imprimir
+PrintDialog.checkbox.showByStage = Mostrar por etapas
+PrintDialog.lbl.selectElements = Seleccionar elementos a incluir:
+printdlg.but.saveaspdf = Guardar como PDF
+printdlg.but.preview = Previsualizar
+printdlg.but.settings = Configuración
+PrintDialog.error.preview.title = Imposible abrir vista previa
+PrintDialog.error.preview.desc1 = Imposible abrir vista previa en PDF.
+PrintDialog.error.preview.desc2 = Por favor use la opción Guardar como PDF.
+
+
+!PrintSettingsDialog
+PrintSettingsDialog.title = Imprimir puesta a punto
+PrintSettingsDialog.lbl.Templatefillcolor = Plantilla de colores:
+PrintSettingsDialog.lbl.Templatebordercolor = Color del borde de la plantilla:
+PrintSettingsDialog.lbl.Papersize = Tamaño del papel:
+PrintSettingsDialog.lbl.Paperorientation = Orientación del papel:
+PrintSettingsDialog.but.Reset = Reiniciar
+PrintSettingsDialog.but.Close = Cerrar
+
+
+! Bug Report dialog
+bugreport.dlg.title = Informe de errores
+bugreport.dlg.but.Sendbugreport = Enviar informe de error
+bugreport.dlg.but.Sendbugreport.Ttip = Enviar automáticamente un informe de error a los creadores de Open Rocket
+bugreport.dlg.successmsg1 = Informe de error enviado con éxito
+bugreport.dlg.successmsg2 = ¡Gracias por ayudar a mejorar Open Rocket!
+bugreport.dlg.successmsg3 = Informe de error enviado
+bugreport.dlg.connectedInternet = <html>Si está conectado a Internet, haga Clik en <em>Enviar informe de errores</em>.
+bugreport.dlg.otherwise = De otro modo, también puede copiar y enviar el texto a la dirección:
+bugreport.lbl.Theinformation = La información que ha detallado se incluirá en un informe de error público. Asegúrese de que no contiene ninguna información que usted no desee hacer pública.
+bugreport.dlg.failedmsg1 = OpenRocket fue incapaz de enviar el informe de error:
+bugreport.dlg.failedmsg2 = Por favor envíe manualmente el informe a
+bugreport.dlg.failedmsg3 = Error al enviar el informe
+bugreport.reportDialog.txt = <html><b>Puede realizar un informe de errores escribiendo en el formulario de abajo y enviarlo.</b><br>También puede informar de los errores adjuntando el archivo de su proyecto por email.
+bugreport.reportDialog.txt2 = <html><b>Por favor incluya una breve descripción de lo que estaba haciendo cuando ocurrió el error.</b>
+bugreport.dlg.provideDescription = Por favor, primero proporcione una descripción del error.
+bugreport.dlg.provideDescription.title = Descripción del error omitida
+
+
+! Debug log dialog
+debuglogdlg.but.clear = Limpiar
+debuglogdlg.OpenRocketdebuglog = Registro de sucesos
+debuglogdlg.Displayloglines = Mostrar líneas de registro:
+debuglogdlg.Follow = Seguir
+debuglogdlg.col.Time = Hora
+debuglogdlg.col.Level = Nivel
+debuglogdlg.col.Location = Localización
+debuglogdlg.col.Message = Mensaje
+debuglogdlg.lbl.Loglinenbr = Número de línea de registro:
+debuglogdlg.lbl.Time = Hora:
+debuglogdlg.lbl.Level = Nivel:
+debuglogdlg.lbl.Location = Localización:
+debuglogdlg.lbl.Logmessage = Texto del mensaje:
+debuglogdlg.lbl.Stacktrace = Trazabilidad de la pila:
+
+
+! Edit Motor configuration dialog
+edtmotorconfdlg.but.removemotor = Quitar motor
+edtmotorconfdlg.but.Selectmotor = Seleccionar motor
+edtmotorconfdlg.but.Removeconfiguration = Quitar configuración
+edtmotorconfdlg.but.Newconfiguration = Nueva configuración
+edtmotorconfdlg.lbl.Motormounts = <html><b>Porta motor:</b>
+edtmotorconfdlg.title.Editmotorconf = Mostrar las configuraciones de motor
+edtmotorconfdlg.selectcomp = <html>Seleccionar qué componentes tienen la función de porta motor:
+edtmotorconfdlg.lbl.Motorconfig = <html><b>Configuraciones del motor:</b>
+edtmotorconfdlg.lbl.Configname = Nombre de la configuración:
+edtmotorconfdlg.lbl.Leavenamedefault = Dejar el nombre por defecto.
+
+! Example design dialog
+exdesigndlg.but.open = Abrir
+exdesigndlg.lbl.Selectexample = Al abrir seleccione ejemplos de diseños:
+exdesigndlg.lbl.Openexampledesign = Abra un diseño como ejemplo
+exdesigndlg.lbl.Exampledesignsnotfound = Los ejemplos de diseño podrían no encontrarse.
+exdesigndlg.lbl.Examplesnotfound = Ejemplos no encontrados
+
+
+! Material edit panel
+matedtpan.but.new = Nuevo
+matedtpan.but.edit = Editar
+matedtpan.but.delete = Borrar
+matedtpan.but.revertall = Invertir todo
+matedtpan.col.Material = Material
+matedtpan.col.Type = Tipo
+matedtpan.col.Density = Densidad
+matedtpan.col.but.ttip.New = Añadir un nuevo material
+matedtpan.title.Addcustmaterial = Añadir un material hecho en casa
+matedtpan.but.ttip.edit = Editar un material existente
+matedtpan.title.Editmaterial = Editar material
+matedtpan.title2.Editmaterial = Los materiales construidos no se pueden modificar
+matedtpan.but.ttip.delete = Borrar un material predefinido
+matedtpan.but.ttip.revertall = Borrar todos los materiales predefinidos
+matedtpan.title.Deletealluser-defined = ¿Borrar todos los materiales predefinidos?
+matedtpan.title.Revertall = ¿Revertir todo?
+matedtpan.lbl.edtmaterials = Editar materiales que no afectaran los diseños existentes.
+
+!MaterialModel
+MaterialModel.title.Material = Material
+MaterialModel.title.Defcustmat = Definir material hecho en casa
+
+
+! Preference dialog
+pref.dlg.but.add = Agregar
+pref.dlg.but.reset = Reiniciar
+pref.dlg.but.checknow = Comprobar ahora
+pref.dlg.but.defaultmetric = Sistema Métrico por defecto
+pref.dlg.but.defaultimperial = Sistema Imperial por defecto
+pref.dlg.title.Preferences = Preferencias
+pref.dlg.tab.Units = Unidades
+pref.dlg.tab.Defaultunits = Unidades por defecto
+pref.dlg.tab.Materials = Materiales
+pref.dlg.tab.Custommaterials = Materiales hechos en casa
+pref.dlg.tab.Options = Opciones
+pref.dlg.tab.Miscellaneousoptions = Otras opciones
+pref.dlg.lbl.Positiontoinsert = Posición para introducir nuevos componentes del fuselaje:
+pref.dlg.lbl.Confirmdeletion = Confirmar borrar simulaciones:
+pref.dlg.lbl.User-definedthrust = Curvas de potencia definidas por el usuario:
+pref.dlg.Allthrustcurvefiles = Todos los ficheros de curvas de potencia (*.eng; *.rse; *.zip; directorios)
+pref.dlg.RASPfiles = Ficheros de motor RASP (*.eng)
+pref.dlg.RockSimfiles = Ficheros de motor Rocksim (*.rse)
+pref.dlg.ZIParchives = Archivos ZIP (*.zip)
+pref.dlg.checkbox.Checkupdates = Comprobar actualizaciones de software al arrancar
+pref.dlg.ttip.Checkupdatesnow = Comprobar actualizaciones de software ahora
+pref.dlg.lbl.Selectprefunits = Seleccione sus unidades preferidas:
+pref.dlg.lbl.Rocketdimensions = Dimensiones del cohete:
+pref.dlg.lbl.Linedensity = Densidad:
+pref.dlg.lbl.Motordimensions = Dimensiones del motor:
+pref.dlg.lbl.Surfacedensity = Densidad superficial:
+pref.dlg.lbl.Distance = Distancia:
+pref.dlg.lbl.Bulkdensity = Densidad media:
+pref.dlg.lbl.Velocity = Velocidad:
+pref.dlg.lbl.Surfaceroughness = Rugosidad de la superficie:
+pref.dlg.lbl.Acceleration = Aceleración:
+pref.dlg.lbl.Area = Área:
+pref.dlg.lbl.Mass = Masa:
+pref.dlg.lbl.Angle = Ángulo:
+pref.dlg.lbl.Force = Fuerza:
+pref.dlg.lbl.Rollrate = Valor de rotación:
+pref.dlg.lbl.Totalimpulse = Impulso total:
+pref.dlg.lbl.Temperature = Temperatura:
+pref.dlg.lbl.Momentofinertia = Momento de inercia:
+pref.dlg.lbl.Pressure = Presión:
+pref.dlg.lbl.Stability = Estabilidad:
+pref.dlg.lbl.FlightTime = Tiempo de vuelo:
+pref.dlg.lbl.effect1 = Los cambios tendrán efecto cuando se abra nuevamente una ventana.
+pref.dlg.lbl.Checkingupdates = Comprobando actualizaciones...
+pref.dlg.lbl.msg1 = Ocurrió un error mientras se comunicaba con el servidor.
+pref.dlg.lbl.msg2 = Incapaz de recuperar la información de las actualizaciones
+pref.dlg.lbl.msg3 = Usted está utilizando la última versión de Open Rocket.
+pref.dlg.lbl.msg4 = No hay actualizaciones disponibles
+pref.dlg.PrefChoiseSelector1 = Preguntar siempre
+pref.dlg.PrefChoiseSelector2 = Insertar en medio
+pref.dlg.PrefChoiseSelector3 = Añadir al final
+pref.dlg.PrefBooleanSelector1 = Borrar
+pref.dlg.PrefBooleanSelector2 = Confirmar
+pref.dlg.Add = Añadir
+pref.dlg.DescriptionArea.Adddirectories = Añadir directorios, archivos de motor RASP (*.eng), archivos de motor RockSim (*.rse) o archivos ZIP separados por punto y coma (;) para cargar curvas de empuje externas. Los cambios tendrán efecto la próxima vez que abra OpenRocket.
+
+PreferencesDialog.lbl.language = Idioma de la interfaz:
+PreferencesDialog.languages.default = Idioma por defecto
+PreferencesDialog.lbl.languageEffect = El idioma cambiará la próxima vez que abra OpenRocket.
+
+! Simulation edit dialog
+simedtdlg.but.runsimulation = Lanzar la simulación
+simedtdlg.but.resettodefault = Restaurar por defecto
+simedtdlg.but.add = Agregar
+simedtdlg.but.remove = Quitar
+simedtdlg.title.Editsim = Mostrar la simulación
+simedtdlg.lbl.Simname = Nombre de la simulación
+simedtdlg.tab.Launchcond = Condiciones del lanzamiento
+simedtdlg.tab.Simopt = Opciones de simulación
+simedtdlg.tab.Plotdata = Datos del gráfico
+simedtdlg.tab.Exportdata = Exportar datos
+simedtdlg.lbl.Motorcfg = Configuración del motor:
+simedtdlg.lbl.ttip.Motorcfg = Seleccionar la configuración del motor a usar
+simedtdlg.combo.ttip.motorconf = Seleccione la configuración del motor a usar
+simedtdlg.lbl.Wind = Viento
+simedtdlg.lbl.Averwindspeed = Velocidad media del viento
+simedtdlg.lbl.ttip.Averwindspeed = Velocidad media del viento en relación al suelo
+simedtdlg.lbl.Stddeviation = Desviación estándar
+simedtdlg.lbl.ttip.Stddeviation = <html>Desviación estándar de la velocidad del viento.<br>La velocidad del viento se encuentra dentro del doble de la desviación media en un 95% del tiempo.
+simedtdlg.lbl.Turbulenceintensity = Intensidad de la turbulencia
+simedtdlg.lbl.ttip.Turbulenceintensity1 = <html>La intensidad de la turbulencia es la desviación estándar dividida por la velocidad media del viento.<br>
+simedtdlg.lbl.ttip.Turbulenceintensity2 = Valores típicos en el campo
+simedtdlg.lbl.ttip.Turbulenceintensity3 = a
+simedtdlg.border.Atmoscond = Condiciones atmosféricas
+simedtdlg.checkbox.InterStdAtmosphere = Usar los patrones de Atmosfera Internacional
+simedtdlg.checkbox.ttip.InterStdAtmosphere1 = <html>Seleccionar para usar el modelo de la International Standard Atmosphere.<br>Este modelo tiene una temperatura de
+simedtdlg.checkbox.ttip.InterStdAtmosphere2 = Y una presión de
+simedtdlg.checkbox.ttip.InterStdAtmosphere3 = A nivel del mar.
+simedtdlg.lbl.Temperature = Temperatura:
+simedtdlg.lbl.ttip.Temperature = Temperatura en el lugar del lanzamiento.
+simedtdlg.lbl.Pressure = Presión:
+simedtdlg.lbl.ttip.Pressure = Presión atmosférica en el lugar del lanzamiento
+simedtdlg.lbl.Launchsite = Lugar del lanzamiento
+simedtdlg.lbl.Latitude = Latitud:
+simedtdlg.lbl.ttip.Latitude = <html>La latitud del lugar de lanzamiento afecta la atracción terrestre.<br>Los valores positivos se dan en el hemisferio Norte, los negativos en el hemisferio Sur.
+
+simedtdlg.lbl.Longitude = Longitud:
+simedtdlg.lbl.ttip.Longitude = <html>Requerido para modelos de elevación y predicción meteorológica.
+
+simedtdlg.lbl.Altitude = Altitud:
+simedtdlg.lbl.ttip.Altitude = <html>Los valores por encima del nivel del mar <br>afectan al modelado de las condicones atmosféricas.
+simedtdlg.border.Launchrod = Varilla para lanzar
+simedtdlg.lbl.Length = Longitud:
+simedtdlg.lbl.ttip.Length = Longitud de la varilla de lanzamiento
+simedtdlg.lbl.Angle = Ángulo:
+simedtdlg.lbl.ttip.Angle = El ángulo de la varilla de lanzamiento con respecto a la vertical.
+simedtdlg.lbl.Direction = Dirección:
+simedtdlg.lbl.ttip.Direction1 = <html>Dirección de la varilla de lanzamiento relativa al viento.<br>
+simedtdlg.lbl.ttip.Direction2 = Contra el viento
+simedtdlg.lbl.ttip.Direction3 = A favor del viento
+simedtdlg.border.Simopt = Opciones del simulador
+simedtdlg.lbl.Calcmethod = Método de cálculo
+simedtdlg.lbl.ttip.Calcmethod = <html>El método Barrowman extendido considera las fuerzas aerodinámicas <br>que actúan sobre cuerpos cilíndricos en cohetes que vuelan con un <br>ángulo de ataque (AOA) superior a 10 grados.
+simedtdlg.lbl.ExtBarrowman = Barrowman Extendido
+simedtdlg.lbl.Simmethod = Método de simulación:
+simedtdlg.lbl.ttip.Simmethod1 = <html>El simulador de seis-grados-de-libertad permite al cohete una total libertad durante el vuelo.<br>
+simedtdlg.lbl.ttip.Simmethod2 = La integración mejora usando el método de integración numérica Runge-Kutta de cuarto orden.
+simedtdlg.lbl.GeodeticMethod = Cálculos geodésicos:
+simedtdlg.lbl.ttip.GeodeticMethodTip = En relación al cálculo de las coordenadas terrestres. Esto también activa los cálculos del Efecto Coriolis.
+simedtdlg.lbl.Timestep = Duración de la etapa
+simedtdlg.lbl.ttip.Timestep1 = <html>Tiempo entre etapas de simulación.<br>Un tiempo mas corto de etapa origina una simulación mas exacta pero mas lenta.<br>
+simedtdlg.lbl.ttip.Timestep2 = Con 4<sup>th</sup> el método de ordenar en la simulación es bastante preciso con un tiempo de etapa de
+simedtdlg.but.ttip.resettodefault = Restituir el tiempo de etapa a su valor por defecto (
+simedtdlg.border.Simlist = Extensiones del simulador
+simedtdlg.txt.longA1 = <html><i>Extensiones del simulador</i> es una característica avanzada que permite que el código escrito por un usuario pueda conectar e interactuar con la simulación mientras ésta se está ejecutando.
+simedtdlg.txt.longA2 = Para más detalles sobre las Extensiones, vea la documentación técnica de Open Rocket.
+simedtdlg.lbl.Curlist = Extensiones actuales
+simedtdlg.lbl.Addsimlist = Añadir una Extensión al simulador
+simedtdlg.lbl.Noflightdata = No hay datos disponibles del vuelo.
+simedtdlg.lbl.runsimfirst = Por favor accione la simulación primero.
+simedtdlg.chart.Simflight = Vuelo simulado
+simedtdlg.dlg.Simres = Resultados de la simulación
+simedtdlg.IntensityDesc.None = Ninguno
+simedtdlg.IntensityDesc.Verylow = Muy pesado
+simedtdlg.IntensityDesc.Low = Pesado
+simedtdlg.IntensityDesc.Medium = Medio
+simedtdlg.IntensityDesc.High = Alto
+simedtdlg.IntensityDesc.Veryhigh = Muy alto
+simedtdlg.IntensityDesc.Extreme = Extremo
+
+GeodeticComputationStrategy.none.name = Ninguna
+GeodeticComputationStrategy.none.desc = No incluir computaciones geodésicas.
+GeodeticComputationStrategy.spherical.name = Aproximación esférica
+GeodeticComputationStrategy.spherical.desc = <html>Al incluir las computaciones geodésicas se considera una Tierra esférica.<br>Este aspecto es bastante preciso en la mayoría de los proyectos.
+GeodeticComputationStrategy.wgs84.name = Elipsoidal WGS84
+GeodeticComputationStrategy.wgs84.desc = <html>Incluye las computaciones geodésicas sobre la referencia elipsoidal WGS84 utilizando el método de Vicenty.<br>Este aspecto es lento e innecesario en la mayoría de los casos.
+
+
+
+
+! Simulation Panel
+simpanel.but.newsimulation = Nueva simulación
+simpanel.but.editsimulation = Editar la simulación
+simpanel.but.runsimulations = Lanzar las simulaciones
+simpanel.but.deletesimulations = Borrar las simulaciones
+simpanel.but.plotexport = Exportar / Gráfica
+simpanel.but.ttip.newsimulation = Añadir una nueva simulación
+simpanel.but.ttip.editsim = Mostrar la simulación seleccionada
+simpanel.but.ttip.runsimu = Ejecutar de nuevo las simulaciones seleccionadas
+simpanel.but.ttip.deletesim = Borrar las simulaciones seleccionadas
+simpanel.checkbox.donotask = No preguntarme de nuevo
+simpanel.lbl.defpref = Puede cambiar la operación por defecto por las preferencias
+simpanel.dlg.lbl.DeleteSim1 = ¿Borrar las simulaciones seleccionadas?
+simpanel.dlg.lbl.DeleteSim2 = <html><i>Esta operación no puede deshacerse.</i>
+simpanel.dlg.lbl.DeleteSim3 = Borrar las simulaciones
+simpanel.col.Name = Nombre
+simpanel.col.Motors = Motores
+simpanel.col.Apogee = Apogeo
+simpanel.col.Maxvelocity = Velocidad máxima
+simpanel.col.Maxacceleration = Aceleración máxima
+simpanel.col.Timetoapogee = Tiempo hasta el apogeo
+simpanel.col.Flighttime = Duración del vuelo
+simpanel.col.Groundhitvelocity = Velocidad de llegada a tierra
+
+! SimulationRunDialog
+SimuRunDlg.title.RunSim = Ejecutar simulaciones
+SimuRunDlg.lbl.Running = Ejecutar
+SimuRunDlg.lbl.Simutime = Duración de la simulación:
+SimuRunDlg.lbl.Altitude = Altitud:
+SimuRunDlg.lbl.Velocity = Velocidad:
+SimuRunDlg.msg.Unabletosim = Incapaz de simular:
+SimuRunDlg.msg.errorOccurred = Ha ocurrido un error durante la simulación:
+SimuRunDlg.msg.AnException1 = Ha ocurrido una excepción durante la simulación:
+SimuRunDlg.msg.AnException2 = Por favor anote esto debajo como un error con todos los detalles.
+SimuRunDlg.msg.AssertionError1 = Se ha producido un error informático durante la simulación.
+SimuRunDlg.msg.AssertionError2 = Por favor anote esto debajo como un error con todos los detalles.
+SimuRunDlg.msg.unknownerror1 = Se ha detectado un error desconocido durante la simulación.
+SimuRunDlg.msg.unknownerror2 = El programa puede ser inestable, Guarde todos sus diseños y reinicie OpenRocket
+
+
+! SimulationExportPanel
+SimExpPan.desc = Documentos separados por comas (*.csv)
+SimExpPan.border.Vartoexport = Variables para exportar
+SimExpPan.but.Selectall = Seleccionar todo
+SimExpPan.but.Selectnone = No seleccionar nada
+SimExpPan.border.Fieldsep = Separador de campo
+SimExpPan.lbl.Fieldsepstr = Caracter separador de campo
+SimExpPan.lbl.longA1 = <html>Caracter para separar campos en el documento exportado.<br>
+SimExpPan.lbl.longA2 = Para valores separados en archivo (CSV) use comas ','.
+SimExpPan.checkbox.Includesimudesc = Incluir descripción de la simulación
+SimExpPan.checkbox.ttip.Includesimudesc = Incluye un comentario en el inicio del documento describiendo la simulación.
+SimExpPan.border.Comments = Comentarios
+SimExpPan.checkbox.Includefielddesc = Incluir descripciones del campo
+SimExpPan.checkbox.ttip.Includefielddesc = Incluye una línea de comentario con las descripciones de las variables exportadas.
+SimExpPan.checkbox.Incflightevents = Incluir los eventos del vuelo
+SimExpPan.checkbox.ttip.Incflightevents = Incluye una línea de comentario para cada evento del vuelo
+SimExpPan.lbl.Commentchar = Carácter de comentario
+SimExpPan.lbl.ttip.Commentchar = Características que marcan una línea de comentario.
+SimExpPan.but.Exporttofile = Exportar al documento ...
+SimExpPan.Fileexists.desc1 = Archivo \"
+SimExpPan.Fileexists.desc2 = \" ya existe. ¿Desea sobrescribir?
+SimExpPan.Fileexists.title = El archivo ya existe
+SimExpPan.ExportingVar.desc1 = Exportar variables
+SimExpPan.ExportingVar.desc2 = Exportar
+SimExpPan.ExportingVar.desc3 = variables de
+SimExpPan.Col.Variable = Variable
+SimExpPan.Col.Unit = Unidad
+
+
+CsvOptionPanel.separator.space = SPACE
+CsvOptionPanel.separator.tab = TAB
+
+
+
+! MotorPlot
+MotorPlot.title.Motorplot = Curva del motor
+MotorPlot.but.Select = Seleccionar la configuración del motor a usar
+MotorPlot.Chart.Motorthrustcurve = Curva de empuje del motor
+MotorPlot.Chart.Time = Tiempo / s
+MotorPlot.Chart.Thrust = Empuje / N
+MotorPlot.txt.Designation = Designación:
+MotorPlot.txt.Manufacturer = Fabricante:
+MotorPlot.txt.Type = Tipo:
+MotorPlot.txt.Delays = Retardos:
+MotorPlot.txt.Comment = Comentario:\n
+
+
+
+! Simulation plot panel
+simplotpanel.lbl.Presetplotconf = Configuración de la gráfica:
+simplotpanel.lbl.Xaxistype = Tipo de eje X:
+simplotpanel.lbl.Unit = Unidad:
+simplotpanel.lbl.Yaxistypes = Tipo de eje Y:
+simplotpanel.lbl.Flightevents = Eventos del vuelo:
+simplotpanel.but.All = Todo
+simplotpanel.but.None = Ninguno
+simplotpanel.but.NewYaxisplottype = Añadir nuevo eje Y en la gráfica
+simplotpanel.but.Plotflight = Ver gráfica
+simplotpanel.lbl.Axis = Ejes:
+simplotpanel.but.ttip.Removethisplot = Eliminar esta curva
+simplotpanel.Desc = Si no hay línea de tiempo, los datos aparecerán en el eje X según el instante en que se producen.
+simplotpanel.OptionPane.lbl1 = Se permite un máximo de 15 impresiones
+simplotpanel.OptionPane.lbl2 = No puede añadirse la curva
+simplotpanel.AUTO_NAME = Auto
+simplotpanel.LEFT_NAME = Izquierda
+simplotpanel.RIGHT_NAME = Derecha
+simplotpanel.CUSTOM = Personalizado
+
+! Component add buttons
+compaddbuttons.Bodycompandfinsets = Componentes del fuselaje y aletas
+compaddbuttons.Nosecone = Ojiva
+compaddbuttons.Bodytube = Cuerpo\ntubular
+compaddbuttons.Transition = Transición
+compaddbuttons.Trapezoidal = Trapezoidal
+compaddbuttons.Elliptical = Elíptica
+compaddbuttons.Freeform = Forma libre
+compaddbuttons.Launchlug = Soporte\npara guía
+compaddbuttons.Innercomponent = Componentes internos
+compaddbuttons.Innertube = Tubo\ninterior
+compaddbuttons.Coupler = Acoplador
+compaddbuttons.Centeringring = Anillo\nde centrado
+compaddbuttons.Bulkhead = Disco\nde enganche
+compaddbuttons.Engineblock = Retén\nde motor
+compaddbuttons.Massobjects = Accesorios
+compaddbuttons.Parachute = Paracaídas
+compaddbuttons.Streamer = Banderola
+compaddbuttons.Shockcord = Tirante de\nsuspensión
+compaddbuttons.Masscomponent = Componente\nmasa
+compaddbuttons.Donotaskmeagain = No me pregunte de nuevo
+compaddbuttons.Selectcomppos = Seleccionar la posición del componente
+compaddbuttons.lbl.Youcanchange = Puede cambiar la operación con las preferencias por defecto
+compaddbuttons.lbl.insertcomp = ¿Insertar el componente después del actual o al final?
+compaddbuttons.askPosition.Inserthere = Insertar aquí
+compaddbuttons.askPosition.Addtotheend = Añadir al final
+compaddbuttons.askPosition.Cancel = Cancelar
+
+! Component Analysis Dialog
+componentanalysisdlg.componentanalysis = Análisis de los componentes
+componentanalysisdlg.lbl.winddir = Dirección del viento:
+componentanalysisdlg.TitledBorder.warnings = Advertencias:
+componentanalysisdlg.ToggleBut.worst = Peor
+componentanalysisdlg.lbl.angleofattack = Ángulo de ataque:
+componentanalysisdlg.lbl.machnumber = Número Mach:
+componentanalysisdlg.lbl.rollrate = Valor de rotación:
+componentanalysisdlg.lbl.activestages = Etapas activas:
+componentanalysisdlg.lbl.motorconf = Configuración del Motor:
+componentanalysisdlg.TabStability.Col = Componente
+componentanalysisdlg.TabStability = Estabilidad
+componentanalysisdlg.TabStability.ttip = Información de Estabilidad
+componentanalysisdlg.dragTableModel.Col.Component = Componente
+componentanalysisdlg.dragTableModel.Col.Pressure = <html>Presión C<sub>D</sub>
+componentanalysisdlg.dragTableModel.Col.Base = <html>Base C<sub>D</sub>
+componentanalysisdlg.dragTableModel.Col.friction = <html>Rozamiento C<sub>D</sub>
+componentanalysisdlg.dragTableModel.Col.total = <html>Total C<sub>D</sub>
+componentanalysisdlg.dragTabchar = Características de rozamiento
+componentanalysisdlg.dragTabchar.ttip = Coeficientes de arrastre de los componentes.
+componentanalysisdlg.rollTableModel.Col.component = Componente
+componentanalysisdlg.rollTableModel.Col.rollforc = Coeficiente de rotación
+componentanalysisdlg.rollTableModel.Col.rolldamp = Coeficiente de corrección
+componentanalysisdlg.rollTableModel.Col.total = <html>Total C<sub>l</sub>
+componentanalysisdlg.rollTableModel = Dinámica de rotación
+componentanalysisdlg.rollTableModel.ttip = Dinámica del movimiento de rotación del cohete (spin)
+componentanalysisdlg.println.closingmethod = Llamar al método de cierre:
+componentanalysisdlg.println.settingnam = CONFIGURANDO VALORES NAN
+componentanalysisdlg.lbl.reflenght = Diámetro de referencia:
+componentanalysisdlg.lbl.refarea = Área de referencia:
+!componentanalysisdlg.But.close = Cerrar
+componentanalysisdlg.TabStability.Col.Component = Componente
+
+! Custom Material dialog
+custmatdlg.title.Custommaterial = Material hecho en casa
+custmatdlg.lbl.Materialname = Nombre del material:
+custmatdlg.lbl.Materialtype = Tipo de material:
+custmatdlg.lbl.Materialdensity = Densidad del material:
+custmatdlg.checkbox.Addmaterial = Agregar este material a la base de datos
+
+
+! Ring Component Config
+ringcompcfg.OuterRadius = Radio exterior:
+ringcompcfg.Automatic = Automático
+ringcompcfg.InnerRadius = Radio interior:
+ringcompcfg.Thickness = Espesor:
+ringcompcfg.Length = Longitud:
+ringcompcfg.Positionrelativeto = Posición relativa a:
+ringcompcfg.plus = Localización:
+ringcompcfg.PositionValue = Valor de posición:
+ringcompcfg.Radialdistance = Distancia radial:
+ringcompcfg.Distancefrom = Distancia desde la línea central del cohete:
+ringcompcfg.Radialdirection = Dirección radial:
+ringcompcfg.radialdirectionfrom = En dirección radial desde la línea central del cohete
+ringcompcfg.but.Reset = Reiniciar
+ringcompcfg.but.Resetcomponant = Reubicar el componente en la línea central del cohete
+ringcompcfg.EngineBlock.desc = <html>Un <b>retén de motor</b> impide que el motor se desplace hacia delante, por dentro del tubo porta motor.<br><br>Para añadir un motor, cree un <b>Cuerpo tubular</b> o <b>Tubo interior</b> y desígnelo como porta motor en el casillero <em>Motor</em>.
+ringcompcfg.note.desc = Nota: El tubo interior no afectará a la aerodinámica del cohete salvo que esté situado fuera del fuselaje.
+
+
+! Body Tube Config
+BodyTubecfg.lbl.Bodytubelength = Longitud del tubo:
+BodyTubecfg.lbl.Outerdiameter = Diámetro exterior:
+BodyTubecfg.lbl.Innerdiameter = Diámetro interior:
+BodyTubecfg.lbl.Wallthickness = Espesor de la pared:
+BodyTubecfg.tab.General = General
+BodyTubecfg.tab.Generalproperties = Propiedades generales
+BodyTubecfg.tab.Motor = Motor
+BodyTubecfg.tab.Motormountconf = Configuración del porta motor
+BodyTubecfg.checkbox.Automatic = Automático
+BodyTubecfg.checkbox.Filled = Sólido
+
+! FinSetConfig
+FinSetConfig.tab.Fintabs = Raíz de aleta
+FinSetConfig.tab.Through-the-wall = Parte de la aleta por dentro del fuselaje
+FinSetConfig.but.Converttofreeform = Convertir a forma libre
+FinSetConfig.but.Converttofreeform.ttip = Convertir esta forma de aleta a una forma libre
+FinSetConfig.Convertfinset = Convertir la configuración de aleta
+FinSetConfig.but.Splitfins = Separar las aletas
+FinSetConfig.but.Splitfins.ttip = Dividir la configuración de aleta en varias separadas
+FinSetConfig.lbl.Through-the-wall = Raíces de aleta a través de la pared:
+FinSetConfig.lbl.Tablength = Longitud de la raíz:
+FinSetConfig.ttip.Tablength = La longitud de la raíz de aleta.
+FinSetConfig.lbl.Tabheight = Altura de la raíz:
+FinSetConfig.ttip.Tabheight = Envergadura en altura de la raíz de aleta.
+FinSetConfig.lbl.Tabposition = Posición de la raíz:
+FinSetConfig.ttip.Tabposition = Posición de la raíz de aleta.
+FinSetConfig.lbl.relativeto = Relativo a
+
+! MotorDatabaseLoadingDialog
+MotorDbLoadDlg.title = Carga de motores
+MotorDbLoadDlg.Loadingmotors = Cargando motores...
+
+! RocketConfig
+RocketCfg.lbl.Designname = Nombre del proyecto:
+RocketCfg.lbl.Designer = Proyectista:
+RocketCfg.lbl.Comments = Comentarios:
+RocketCfg.lbl.Revisionhistory = Histórico de la revisión:
+RocketCfg.lbl.Material = Material:
+
+! ShockCordConfig
+ShockCordCfg.lbl.Shockcordlength = Longitud del tirante de suspensión
+
+! RocketComponentConfig
+RocketCompCfg.lbl.Componentname = Nombre del componente:
+RocketCompCfg.ttip.Thecomponentname = El nombre del componente.
+RocketCompCfg.tab.Override = Masa y CG
+RocketCompCfg.tab.MassandCGoverride = Especificar la Masa y el CG del componente.
+RocketCompCfg.tab.Figure = Estilo
+RocketCompCfg.tab.Figstyleopt = Opciones de estilo de la figura
+RocketCompCfg.tab.Comment = Comentarios
+RocketCompCfg.tab.Specifyacomment = Especifique un comentario para el componente
+RocketCompCfg.lbl.Mass = Masa:
+RocketCompCfg.lbl.Componentmass = Masa del componente:
+RocketCompCfg.lbl.overriddento = (Elegido para
+RocketCompCfg.lbl.overriddenby = (Elegido por
+RocketCompCfg.lbl.Componentmaterial = Material del componente:
+RocketCompCfg.lbl.Componentfinish = Acabado:
+RocketCompCfg.lbl.ttip.componentmaterialaffects = El material del componente afecta su peso.
+RocketCompCfg.combo.ttip.componentmaterialaffects = El material del componente afecta su peso.
+RocketCompCfg.lbl.longA1 = <html>El acabado del componente afecta a su coeficiente de rozamiento.<br>
+RocketCompCfg.lbl.longA2 = El valor indicado es el promedio de la rugosidad en altura de la superficie.
+RocketCompCfg.but.Setforall = Aplicar a todos
+RocketCompCfg.but.ttip.Setforall = Aplicar este acabado a todos los componentes del cohete.
+RocketCompCfg.lbl.Overridemassorcenter = Especificar la masa y el CG del componente
+RocketCompCfg.checkbox.Overridemass = Especificar la masa:
+RocketCompCfg.checkbox.Overridecenterofgrav = Especificar el CG:
+RocketCompCfg.checkbox.OverridemassandCG = Incluir la masa y el CG de todos los subcomponentes
+RocketCompCfg.lbl.longB1 = <html>En la masa especificada no se incluye la de los motores.<br>
+RocketCompCfg.lbl.longB2 = El CG se mide desde el extremo frontal del componente
+RocketCompCfg.lbl.Commentsonthe = Comentarios sobre
+RocketCompCfg.lbl.Figurestyle = Estilo de dibujo:
+RocketCompCfg.lbl.Componentcolor = Color del componente:
+RocketCompCfg.lbl.Choosecolor = Elija color
+RocketCompCfg.checkbox.Usedefaultcolor = Usar color por defecto
+RocketCompCfg.lbl.Complinestyle = Estilo de línea del componente:
+RocketCompCfg.but.Saveasdefstyle = Guardar como estilo por defecto
+RocketCompCfg.lbl.Diameter = Diámetro:
+RocketCompCfg.lbl.Length = Longitud:
+RocketCompCfg.lbl.Thickness = Espesor:
+RocketCompCfg.checkbox.Endcapped = Extremo truncado
+RocketCompCfg.ttip.Endcapped = Si el extremo del soporte está truncado.
+RocketCompCfg.title.Noseconeshoulder = Acople de la ojiva
+RocketCompCfg.title.Aftshoulder = Trasera del acople
+RocketCompCfg.border.Foreshoulder = Delantera del acople
+!RocketCompCfg.lbl.Length = Longitud:
+
+! BulkheadConfig
+BulkheadCfg.tab.Diameter = Diámetro:
+BulkheadCfg.tab.Thickness = Espesor:
+BulkheadCfg.tab.General = General
+BulkheadCfg.tab.Generalproperties = Propiedades generales
+
+!CenteringRingConfig
+CenteringRingCfg.tab.Outerdiam = Diámetro exterior:
+CenteringRingCfg.tab.Innerdiam = Diámetro interior:
+CenteringRingCfg.tab.Thickness = Espesor:
+CenteringRingCfg.tab.General = General
+CenteringRingCfg.tab.Generalproperties = Propiedades generales
+
+!ComponentConfigDialog
+ComponentCfgDlg.configuration =
+ComponentCfgDlg.configuration1 = Configuración
+ComponentCfgDlg.Modify = Modificar
+
+!EllipticalFinSetConfig
+EllipticalFinSetCfg.Nbroffins = Número de aletas:
+EllipticalFinSetCfg.Rotation = Rotación de las aletas:
+EllipticalFinSetCfg.Fincant = Inclinación de las aletas:
+EllipticalFinSetCfg.Rootchord = Longitud línea base:
+EllipticalFinSetCfg.Height = Altura:
+EllipticalFinSetCfg.Positionrelativeto = Posición relativa a:
+EllipticalFinSetCfg.plus = Localización:
+EllipticalFinSetCfg.FincrossSection = Borde de la aleta:
+EllipticalFinSetCfg.Thickness = Espesor:
+EllipticalFinSetCfg.General = General
+EllipticalFinSetCfg.Generalproperties = Propiedades generales
+EllipticalFinSetCfg.ttip.Fincant = El ángulo de inclinación de las aletas respecto al eje central del fuselaje.
+
+!FreeformFinSetConfig
+FreeformFinSetCfg.tab.General = General
+FreeformFinSetCfg.tab.ttip.General = Propiedades generales
+FreeformFinSetCfg.tab.Shape = Forma
+FreeformFinSetCfg.tab.ttip.Finshape = Forma de la aleta
+FreeformFinSetCfg.lbl.Numberoffins = Número de aletas:
+FreeformFinSetCfg.lbl.Finrotation = Rotación de las aletas:
+FreeformFinSetCfg.lbl.Fincant = Inclinación de las aletas:
+FreeformFinSetCfg.lbl.ttip.Fincant = El ángulo de inclinación de las aletas respecto al eje central del fuselaje.
+FreeformFinSetCfg.lbl.Posrelativeto = Posición relativa a:
+FreeformFinSetCfg.lbl.plus = Localización:
+FreeformFinSetCfg.lbl.FincrossSection = Borde de la aleta:
+FreeformFinSetCfg.lbl.Thickness = Espesor:
+!DobleClic 1 + 2 en el mensaje "Doble-Click para editar", corta aproximadamente por la mitad
+FreeformFinSetCfg.lbl.doubleClick1 = Doble Click en la lista
+FreeformFinSetCfg.lbl.doubleClick2 = para editar
+FreeformFinSetCfg.lbl.clickDrag = Click (sobre línea)+arrastrar: Agregar punto
+FreeformFinSetCfg.lbl.ctrlClick = Control+Click (sobre punto): Eliminar punto
+
+
+!InnerTubeConfig
+InnerTubeCfg.tab.Motor = Motor
+InnerTubeCfg.tab.ttip.Motor = Configuración del porta motor
+InnerTubeCfg.tab.Cluster = Cluster
+InnerTubeCfg.tab.ttip.Cluster = Configuración del cluster
+InnerTubeCfg.tab.Radialpos = Posición radial
+InnerTubeCfg.tab.ttip.Radialpos = Posición radial
+InnerTubeCfg.lbl.Selectclustercfg = Elija la configuración del cluster:
+InnerTubeCfg.lbl.TubeSep = Separación del tubo:
+InnerTubeCfg.lbl.ttip.TubeSep = Una separación de los tubos con valor 1.0 indica que están tocándose unos con otros
+InnerTubeCfg.lbl.Rotation = Rotación:
+InnerTubeCfg.lbl.ttip.Rotation = Configuración del ángulo de rotación del cluster
+InnerTubeCfg.lbl.Rotangle = Angulo de rotación del cluster
+InnerTubeCfg.but.Splitcluster = Tubos independientes
+InnerTubeCfg.lbl.longA1 = <html>Separar los tubos del cluster para convertirlos en componentes internos independientes.<br>
+InnerTubeCfg.lbl.longA2 = Esto también duplica todos los componentes unidos a este tubo interior.
+InnerTubeCfg.but.Resetsettings = Reiniciar configuración
+InnerTubeCfg.but.ttip.Resetsettings = Reiniciar la separación y la rotación con los valores predeterminados
+
+! LaunchLugConfig
+LaunchLugCfg.lbl.Length = Longitud:
+LaunchLugCfg.lbl.Outerdiam = Diámetro exterior:
+LaunchLugCfg.lbl.Innerdiam = Diámetro interior:
+LaunchLugCfg.lbl.Thickness = Espesor:
+LaunchLugCfg.lbl.Radialpos = Posición radial:
+LaunchLugCfg.lbl.Posrelativeto = Posición relativa a:
+LaunchLugCfg.lbl.plus = Localización:
+LaunchLugCfg.tab.General = General
+LaunchLugCfg.tab.Generalprop = Propiedades generales
+
+! MassComponentConfig
+MassComponentCfg.lbl.Mass = Masa:
+MassComponentCfg.lbl.Length = Longitud:
+MassComponentCfg.lbl.Diameter = Diámetro:
+MassComponentCfg.lbl.PosRelativeto = Posición relativa a:
+MassComponentCfg.lbl.plus = Localización:
+MassComponentCfg.tab.General = General
+MassComponentCfg.tab.ttip.General = Propiedades generales
+MassComponentCfg.tab.Radialpos = Posición radial
+MassComponentCfg.tab.ttip.Radialpos = Configuración de la posición radial
+MassComponentCfg.lbl.Radialdistance = Distancia radial:
+MassComponentCfg.lbl.Radialdirection = Dirección radial:
+MassComponentCfg.but.Reset = Reiniciar
+
+! MotorConfig
+MotorCfg.checkbox.compmotormount = Este componente es un porta motor
+MotorCfg.lbl.Motorcfg = Configuración del motor:
+MotorCfg.but.New = Nuevo
+MotorCfg.lbl.Currentmotor = Motor actual:
+MotorCfg.lbl.Motoroverhang = Sobresalida del motor:
+MotorCfg.lbl.Ignitionat = Encendido en:
+MotorCfg.lbl.plus = Retardo:
+MotorCfg.lbl.seconds = segundos.
+MotorCfg.lbl.longA1 = El diseño actual tiene una sola etapa.
+MotorCfg.lbl.longA2 = Pueden agregarse etapas haciendo Click en \"Nueva etapa\".
+MotorCfg.lbl.longB1 = El diseño actual tiene
+MotorCfg.lbl.longB2 = etapas.
+MotorCfg.but.Selectmotor = Seleccionar motor
+MotorCfg.but.Removemotor = Quitar motor
+MotorCfg.lbl.motorLabel = Ninguno
+
+! NoseConeConfig
+NoseConeCfg.lbl.Noseconeshape = Forma:
+NoseConeCfg.lbl.Shapeparam = Valor de forma:
+NoseConeCfg.lbl.Noseconelength = Longitud:
+NoseConeCfg.lbl.Basediam = Diámetro de la base:
+NoseConeCfg.checkbox.Automatic = Automático
+NoseConeCfg.lbl.Wallthickness = Espesor de la pared:
+NoseConeCfg.checkbox.Filled = Sólido
+NoseConeCfg.tab.General = General
+NoseConeCfg.tab.ttip.General = Propiedades generales
+NoseConeCfg.tab.Shoulder = Acoplamiento
+NoseConeCfg.tab.ttip.Shoulder = Propiedades del acople
+
+! ParachuteConfig
+ParachuteCfg.lbl.Canopy = Pabellón
+ParachuteCfg.lbl.Diameter = Diámetro:
+ParachuteCfg.lbl.Material = Material:
+ParachuteCfg.combo.MaterialModel = El material del componente afecta a su peso.
+ParachuteCfg.lbl.longA1 = <html>Coeficiente de arrastre C<sub>D</sub>:
+ParachuteCfg.lbl.longB1 = <html>Coeficiente de rozamiento relativo al área total del paracaídas.<br>
+ParachuteCfg.lbl.longB2 = Un mayor coeficiente de rozamiento genera un valor de descenso más lento.
+ParachuteCfg.lbl.longB3 = Un valor típico para los paracaídas es 0,8.
+ParachuteCfg.but.Reset = Reiniciar
+ParachuteCfg.lbl.Shroudlines = Cuerdas:
+ParachuteCfg.lbl.Numberoflines = Número de cuerdas:
+ParachuteCfg.lbl.Linelength = Longitud de cuerda:
+ParachuteCfg.lbl.Material = Material:
+ParachuteCfg.lbl.Posrelativeto = Posición relativa a:
+ParachuteCfg.lbl.plus = Localización:
+ParachuteCfg.lbl.Packedlength = Longitud empaquetado:
+ParachuteCfg.lbl.Packeddiam = Diámetro del empaquetado:
+ParachuteCfg.lbl.Deploysat = Despliegue en:
+ParachuteCfg.lbl.seconds = segundos.
+ParachuteCfg.lbl.Altitude = Altitud:
+ParachuteCfg.tab.General = General
+ParachuteCfg.tab.ttip.General = Propiedades generales
+ParachuteCfg.tab.Radialpos = Posición radial
+ParachuteCfg.tab.ttip.Radialpos = Configuración de la posición radial
+ParachuteCfg.lbl.Radialdistance = Distancia radial:
+ParachuteCfg.lbl.Radialdirection = Dirección radial:
+ParachuteCfg.but.Reset = Reiniciar
+ParachuteCfg.lbl.plusdelay = Retardo:
+
+
+! ShockCordConfig
+ShockCordCfg.lbl.Shockcordlength = Longitud del tirante de suspensión
+ShockCordCfg.lbl.Shockcordmaterial = Material del tirante de suspensión:
+ShockCordCfg.lbl.Posrelativeto = Posición relativa a:
+ShockCordCfg.lbl.plus = Localización:
+ShockCordCfg.lbl.Packedlength = Longitud del empaquetado:
+ShockCordCfg.lbl.Packeddiam = Diámetro del empaquetado:
+ShockCordCfg.tab.General = General
+ShockCordCfg.tab.ttip.General = Propiedades generales
+
+!SleeveConfig
+SleeveCfg.tab.Outerdiam = Diámetro exterior:
+SleeveCfg.tab.Innerdiam = Diámetro interior:
+SleeveCfg.tab.Wallthickness = Espesor de la pared:
+SleeveCfg.tab.Length = Longitud:
+SleeveCfg.tab.General = General
+SleeveCfg.tab.Generalproperties = Propiedades generales
+
+! StreamerConfig
+StreamerCfg.lbl.Striplength = Longitud de la cinta:
+StreamerCfg.lbl.Stripwidth = Ancho de la cinta:
+StreamerCfg.lbl.Striparea = Área de la cinta:
+StreamerCfg.lbl.Aspectratio = Relación de aspecto:
+StreamerCfg.lbl.Material = Material:
+StreamerCfg.combo.ttip.MaterialModel = El material del componente afecta a su peso.
+StreamerCfg.lbl.longA1 = <html>Coeficiente de rozamiento C<sub>D</sub>:
+StreamerCfg.lbl.longB1 = <html>Coeficiente de rozamiento relativo al área total de la banderola.<br>
+StreamerCfg.lbl.longB2 = Un mayor coeficiente de rozamiento genera un valor de descenso más lento.
+StreamerCfg.lbl.Automatic = Automático
+StreamerCfg.lbl.longC1 = El coeficiente de rozamiento depende del área de la banderola.
+StreamerCfg.lbl.Posrelativeto = Posición relativa a:
+StreamerCfg.lbl.plus = Localización:
+StreamerCfg.lbl.Packedlength = Longitud de empaquetado:
+StreamerCfg.lbl.Packeddiam = Diámetro de empaquetado:
+StreamerCfg.lbl.Deploysat = Despliegue en:
+StreamerCfg.lbl.seconds = segundos.
+StreamerCfg.lbl.Altitude = Altitud:
+StreamerCfg.tab.General = General
+StreamerCfg.tab.ttip.General = Propiedades generales
+StreamerCfg.tab.Radialpos = Posición radial
+StreamerCfg.tab.ttip.Radialpos = Configuración de posición radial
+StreamerCfg.lbl.Radialdistance = Distancia radial:
+StreamerCfg.lbl.Radialdirection = Dirección radial:
+StreamerCfg.but.Reset = Reiniciar
+StreamerCfg.lbl.plusdelay = Retardo:
+
+! ThicknessRingComponentConfig
+ThicknessRingCompCfg.tab.Outerdiam = Diámetro exterior:
+ThicknessRingCompCfg.tab.Innerdiam = Diámetro Interior:
+ThicknessRingCompCfg.tab.Wallthickness = Espesor de la pared:
+ThicknessRingCompCfg.tab.Length = Longitud:
+ThicknessRingCompCfg.tab.General = General
+ThicknessRingCompCfg.tab.Generalprop = Propiedades generales
+
+! TransitionConfig
+TransitionCfg.lbl.Transitionshape = Forma de la transición:
+TransitionCfg.checkbox.Clipped = Acortado
+TransitionCfg.lbl.Shapeparam = Valor de forma:
+TransitionCfg.lbl.Transitionlength = Longitud de la transición:
+TransitionCfg.lbl.Forediam = Diámetro delantero:
+TransitionCfg.checkbox.Automatic = Automático
+TransitionCfg.lbl.Aftdiam = Diámetro trasero:
+TransitionCfg.lbl.Wallthickness = Espesor de la pared:
+TransitionCfg.checkbox.Filled = Sólido
+TransitionCfg.tab.General = General
+TransitionCfg.tab.Generalproperties = Propiedades generales
+TransitionCfg.tab.Shoulder = Acoplamiento
+TransitionCfg.tab.Shoulderproperties = Propiedades del acople
+
+! TrapezoidFinSetConfig
+TrapezoidFinSetCfg.lbl.Nbroffins = Número de aletas:
+TrapezoidFinSetCfg.lbl.ttip.Nbroffins = Número de aletas en la base de aletas.
+TrapezoidFinSetCfg.lbl.Finrotation = Rotación de las aletas:
+TrapezoidFinSetCfg.lbl.ttip.Finrotation = Posición de las aletas alrededor del fuselaje.
+TrapezoidFinSetCfg.lbl.Fincant = Inclinación de las aletas:
+TrapezoidFinSetCfg.lbl.ttip.Fincant = El ángulo de inclinación de las aletas respecto al eje central del fuselaje.
+TrapezoidFinSetCfg.lbl.Rootchord = Longitud de la línea base:
+TrapezoidFinSetCfg.lbl.Tipchord = Longitud del borde superior:
+TrapezoidFinSetCfg.lbl.Height = Altura:
+TrapezoidFinSetCfg.lbl.Sweeplength = Desplazamiento borde superior:
+TrapezoidFinSetCfg.lbl.Sweepangle = Ángulo del borde de ataque:
+TrapezoidFinSetCfg.lbl.FincrossSection = Borde de la aleta:
+TrapezoidFinSetCfg.lbl.Thickness = Espesor:
+TrapezoidFinSetCfg.lbl.Posrelativeto = Posición relativa a:
+TrapezoidFinSetCfg.lbl.plus = Localización:
+TrapezoidFinSetCfg.tab.General = General
+TrapezoidFinSetCfg.tab.Generalproperties = Propiedades generales
+
+!MotorConfigurationModel
+MotorCfgModel.Editcfg = Editar configuraciones
+
+! StorageOptionChooser
+StorageOptChooser.lbl.Simdatatostore = Almacenar datos simulados
+StorageOptChooser.rdbut.Allsimdata = Todos los datos simulados
+StorageOptChooser.lbl.longA1 = <html>Almacenar todos los datos simulados.<br>
+StorageOptChooser.lbl.longA2 = puede generar archivos muy grandes
+StorageOptChooser.rdbut.Every = Cada
+StorageOptChooser.lbl.longB1 = <html>Almacenar los valores de impresión de este apartado.<br>
+StorageOptChooser.lbl.longB2 = Genera valores grandes en archivos más pequeños.
+StorageOptChooser.lbl.seconds = Segundos
+StorageOptChooser.rdbut.Onlyprimfig = Sólo figuras principales
+StorageOptChooser.lbl.longC1 = <html>Almacenar sólo los valores en la tabla resumen.<br>
+StorageOptChooser.lbl.longC2 = Estos resultados se guardan en archivos mas pequeños.
+StorageOptChooser.checkbox.Compfile = Archivo comprimido
+StorageOptChooser.lbl.UsingComp = Usando la compresión reducimos el tamaño de los archivos.
+StorageOptChooser.lbl.longD1 = Una estimación de cuan grande será un archivo podría tenerse con las presentes opciones.
+StorageOptChooser.ttip.Saveopt = Guardar opciones
+StorageOptChooser.lbl.Estfilesize = Estimación del tamaño del archivo:
+StorageOptChooser.lbl.Saveopt = Guardar opciones
+
+! ThrustCurveMotorSelectionPanel
+TCMotorSelPan.lbl.Selrocketmotor = Seleccione el motor del cohete:
+TCMotorSelPan.checkbox.hideSimilar = Borrar las curvas muy similares
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Mostrar todos los motores
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Mostrar motores con diámetro inferior al del tubo portamotor
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Mostrar motores con diámetro igual al del tubo portamotor
+TCMotorSelPan.lbl.Motormountdia = Diámetro del portamotor:
+TCMotorSelPan.lbl.Search = Buscar:
+TCMotorSelPan.lbl.Selectthrustcurve = Seleccione curva de empuje:
+TCMotorSelPan.lbl.Ejectionchargedelay = Retardo de la carga de eyección:
+TCMotorSelPan.equalsIgnoreCase.None = Ninguno
+TCMotorSelPan.lbl.NumberofsecondsorNone = (Número de segundos o \"Ninguno\")
+TCMotorSelPan.lbl.Totalimpulse = Impulso total:
+TCMotorSelPan.lbl.Avgthrust = Empuje medio:
+TCMotorSelPan.lbl.Maxthrust = Empuje máximo:
+TCMotorSelPan.lbl.Burntime = Tiempo de quemado:
+TCMotorSelPan.lbl.Launchmass = Masa total:
+TCMotorSelPan.lbl.Emptymass = Masa carcasa:
+TCMotorSelPan.lbl.Datapoints = Datos de los puntos:
+TCMotorSelPan.lbl.Digest = Resumen:
+TCMotorSelPan.title.Thrustcurve = Curva de empuje:
+TCMotorSelPan.title.Thrust = Empuje
+TCMotorSelPan.delayBox.None = Ninguno
+
+
+! PlotDialog
+PlotDialog.title.Flightdataplot = Representar los datos de vuelo
+PlotDialog.Chart.Simulatedflight = Vuelo simulado
+PlotDialog.CheckBox.Showdatapoints = Mostrar los datos de los puntos
+PlotDialog.lbl.Chart = Click+bajar el rozamiento+derecha ampliar, arriba+izquierda disminuir
+
+
+! "main" prefix is used for the main application dialog
+
+# FIXME: Rename the description keys
+
+main.menu.file = Archivo
+main.menu.file.desc = Tareas relacionadas con el manejo de archivos
+main.menu.file.new = Nuevo
+main.menu.file.new.desc = Crear un nuevo diseño de cohete
+main.menu.file.open = Abrir ...
+BasicFrame.item.Openrocketdesign = Abrir un diseño de cohete
+main.menu.file.openExample = Abrir ejemplo ...
+BasicFrame.item.Openexamplerocketdesign = Abrir un ejemplo de diseño de cohete
+main.menu.file.save = Guardar
+BasicFrame.item.SavecurRocketdesign = Guardar el diseño actual
+main.menu.file.saveAs = Guardar como ...
+BasicFrame.item.SavecurRocketdesnewfile = Guardar el diseño actual como un nuevo documento
+main.menu.file.print = Imprimir ...
+BasicFrame.item.Printpart = Imprimir un listado de componentes y un esquema de aleta
+main.menu.file.close = Cerrar
+BasicFrame.item.Closedesign = Cerrar el diseño actual
+main.menu.file.quit = Salir
+BasicFrame.item.Quitprogram = Salir del programa
+
+main.menu.edit = Edición
+BasicFrame.menu.Rocketedt = Mostrar el cohete
+main.menu.edit.undo = Deshacer
+main.menu.edit.undo.desc = Deshacer la operación anterior
+main.menu.edit.redo = Rehacer
+main.menu.edit.redo.desc = Rehacer la operación anterior
+main.menu.edit.cut = Cortar
+main.menu.edit.copy = Copiar
+main.menu.edit.paste = Pegar
+main.menu.edit.delete = Borrar
+main.menu.edit.resize = Dimensionar...
+main.menu.edit.resize.desc = Dimensionar las partes del diseño del cohete
+main.menu.edit.preferences = Preferencias
+main.menu.edit.preferences.desc = Configurar las preferencias de la aplicación
+
+main.menu.analyze = Analizar
+main.menu.analyze.desc = Análisis del cohete
+main.menu.analyze.componentAnalysis = Análisis de los componentes
+main.menu.analyze.componentAnalysis.desc = Analiza los componentes del cohete por separado
+main.menu.analyze.optimization = Optimización del diseño
+main.menu.analyze.optimization.desc = Optimización global del diseño del cohete
+main.menu.help = Ayuda
+main.menu.help.desc = Información acerca del cohete
+main.menu.help.license = Licencia
+main.menu.help.license.desc = Información de la licencia de OpenRocket
+main.menu.help.bugReport = Informe de errores
+main.menu.help.bugReport.desc = Informar sobre errores encontrados en OpenRocket
+main.menu.help.debugLog = Registro de sucesos
+main.menu.help.debugLog.desc = Visualizar el registro de depuración de OpenRocket
+main.menu.help.about = Acerca de
+main.menu.help.about.desc = Detalles del Copyright de OpenRocket
+
+main.menu.debug = Recuperación
+main.menu.debug.whatisthismenu = ¿Que es este menú?
+main.menu.debug.createtestrocket = Crear una prueba de modelo
+
+! database
+! Translate here all material database
+!
+
+! Material database
+! BULK_MATERIAL
+Databases.materials.Acrylic = Acrílico
+Databases.materials.Balsa = Balsa
+Databases.materials.Birch = Abedul
+Databases.materials.Cardboard = Cartón
+Databases.materials.Carbonfiber = Fibra de Carbono
+Databases.materials.Cork = Corcho
+Databases.materials.DepronXPS = Depron (XPS)
+Databases.materials.Fiberglass = Fibra de vidrio
+Databases.materials.Kraftphenolic = Cartón fenólico
+Databases.materials.Maple = Arce
+Databases.materials.Paperoffice = Papel (oficina)
+Databases.materials.Pine = Pino
+Databases.materials.Plywoodbirch = Contrachapado
+Databases.materials.PolycarbonateLexan = Policarbonato (Lexan)
+Databases.materials.Polystyrene = Poliestireno
+Databases.materials.PVC = PVC
+Databases.materials.Spruce = Pícea (Abeto común)
+Databases.materials.StyrofoamgenericEPS = Porex (generico EPS)
+Databases.materials.StyrofoamBluefoamXPS = Porex \"Foam azul\" (XPS)
+Databases.materials.Quantumtubing = Quantum tubing
+Databases.materials.BlueTube = Tubo azul (PML)
+!SURFACE_MATERIAL
+Databases.materials.Ripstopnylon = Ripstop nylon
+Databases.materials.Mylar = Mylar
+Databases.materials.Polyethylenethin = Polietileno (delgado)
+Databases.materials.Polyethyleneheavy = Polietileno (grueso)
+Databases.materials.Silk = Seda
+Databases.materials.Paperoffice = Papel (oficina)
+Databases.materials.Cellophane = Celofán
+Databases.materials.Crepepaper = Crespón de papel
+! LINE_MATERIAL
+Databases.materials.Threadheavy-duty = Trenzado (Alta resistencia)
+Databases.materials.Elasticcordround2mm = Cordón elástico (aprox. 2mm, 1/16 in)
+Databases.materials.Elasticcordflat6mm = Cordón elástico plano (6mm, 1/4 in)
+Databases.materials.Elasticcordflat12mm = Cordón elástico plano (12mm, 1/2 in)
+Databases.materials.Elasticcordflat19mm = Cordón elástico plano (19mm, 3/4 in)
+Databases.materials.Elasticcordflat25mm = Cordón elástico plano (25mm, 1 in)
+Databases.materials.Braidednylon2mm = Nylon trenzado (2 mm, 1/16 in)
+Databases.materials.Braidednylon3mm = Nylon trenzado (3 mm, 1/8 in)
+Databases.materials.Tubularnylon11mm = Nylon tubular (11 mm, 7/16 in)
+Databases.materials.Tubularnylon14mm = Nylon tubular (14 mm, 9/16 in)
+Databases.materials.Tubularnylon25mm = Nylon tubular (25 mm, 1 in)
+
+! ExternalComponent
+ExternalComponent.Rough = Rugoso
+ExternalComponent.Unfinished = Inacabado
+ExternalComponent.Regularpaint = Pintura normal
+ExternalComponent.Smoothpaint = Pintura fina
+ExternalComponent.Polished = Pulido
+
+! LineStyle
+LineStyle.Solid = Sólido
+LineStyle.Dashed = Discontinuo
+LineStyle.Dotted = Punteado
+LineStyle.Dash-dotted = Discontinuo con puntos
+LineStyle.Defaultstyle = Estilo por defecto
+
+! Shape
+Shape.Conical = Cónico
+Shape.Conical.desc1 = Una ojiva cónica de perfil triangular
+Shape.Conical.desc2 = Transición cónica de lados rectos
+Shape.Ogive = Ojival
+Shape.Ogive.desc1 = Ojiva con perfil de arco de circunferencia. Un valor de forma igual a 1 produce una <b>Ojiva tangente</b>, mientras que un valor inferior a 1 produce una <b>Ojiva secante</b> con un perfil más afilado.
+Shape.Ogive.desc2 = Transición con perfil de arco de circunferencia. Un valor de forma igual a 1 produce una <b>Transición tangente</b>, mientras que un valor inferior a 1 produce una <b>Transición secante</b> con un perfil más afilado.
+Shape.Ellipsoid = Elíptica
+Shape.Ellipsoid.desc1 = Ojiva con perfil de media elipse. Por defecto, una elipse de <i>longitud</i> igual al triple de su <i>diámetro</i>.
+Shape.Ellipsoid.desc2 = Transición con perfil de media elipse. Por defecto, una elipse de <i>longitud</i> igual al triple de su <i>diámetro</i>.
+Shape.Powerseries = Serie potencial
+Shape.Powerseries.desc1 = Ojiva cuyo perfil es una curva obtenida a partir de una función potencial f(<i>x</i>)<sup><i>k</i></sup>. Un valor de forma k=0.5 produce una ojiva con perfil de parábola, para k=0.75 se produce una ojiva con <b>perfil potencial</b>, y para k=1 se produce una ojiva con perfil recto u <b>Ojiva cónica</b>.
+Shape.Powerseries.desc2 = Transición cuyo perfil es una curva obtenida a partir de una función potencial de <i>Radio</i> =; (<i>x</i> / <i>L</i>)<sup><i>k</i></sup> donde <i>k</i> es el parámetro de forma. Para <i>k</i>=0.5 la transición es <b>\u00BD-potencial</b> o <b>parabólica</b>, para <i>k</i>=0.75 a <b>\u00BE-potencia</b>, y para <i>k</i>=1 <b>cónica</b>.
+Shape.Parabolicseries = Serie parabólica
+Shape.Parabolicseries.desc1 = Ojiva con perfil de arco de parábola. Un valor de forma igual a 1 produce una <b>Ojiva tangente</b>, un valor igual a 0.75 produce una <b>parábola de 3/4</b>, un valor igual a 0.5 produce una <b>parábola de 1/2</b>, y un valor igual a 0 produce un perfil recto u <b>Ojiva cónica</b>.
+Shape.Parabolicseries.desc2 = Una transición de serie parabólica tiene un perfil de parábola. El valor de forma defien el tipo de parábola a utilizar. Un valor de forma de 1.0 produce una parábola completa que es tangente al cuerpo tubular en el extremo trasero, un valor de 0.75 produce una <b>parábola de 3/4</b>, un valor de 0.5 produce una <b>parábola de 1/2</b>, y un valor de 0 produce una transición cónica.
+Shape.Haackseries = Haack series
+Shape.Haackseries.desc1 = Ojiva con perfil de mínimo arrastre aerodinámico recomendado para vuelos supersónicos. Un valor de forma igual a 0 produce una <b>Ojiva LD Haack</b> u <b>Ojiva Von Karman</b> que minimiza el arrastre aerodinámico para una determinada longitud y diámetro de la base, mientras que un valor igual a 0.333 produce una <b>Ojiva LV-Haack</b> que minimiza el arrastre aerodinámico para una determinada longitud y volumen de la ojiva.
+Shape.Haackseries.desc2 = Las transiciones Haack series están diseñadas para minimizar el arrastre aerodinámico. Estas transiciones poseen sus equivalentes, pero no necesariamente producen un arrastre óptimo. Un valor de forma 0 produce una transición <b>LD-Haack</b> o <b>Von Karman</b>, mientras que un valor de 0.333 produce una forma <b>LV-Haack</b>.
+
+
+! RocketComponent
+RocketComponent.Position.TOP = Parte superior del componente
+RocketComponent.Position.MIDDLE = Parte media del componente
+RocketComponent.Position.BOTTOM = Extremo inferior del componente
+RocketComponent.Position.AFTER = Después del componente
+RocketComponent.Position.ABSOLUTE = Extremo de la ojiva
+
+! LaunchLug
+LaunchLug.Launchlug = Soporte para Guía
+! NoseCone
+NoseCone.NoseCone = Ojiva
+! Transition
+Transition.Transition = Transición
+!Stage
+Stage.Stage = Etapa
+! BodyTube
+BodyTube.BodyTube = Cuerpo tubular
+! TubeCoupler
+TubeCoupler.TubeCoupler = Acoplador
+!InnerTube
+InnerTube.InnerTube = Tubo interior
+! TrapezoidFinSet
+TrapezoidFinSet.TrapezoidFinSet = Aleta trapezoidal
+! FreeformFinSet
+FreeformFinSet.FreeformFinSet = Aleta de forma libre
+!MassComponent
+MassComponent.MassComponent = Masa
+! Parachute
+Parachute.Parachute = Paracaídas
+! ShockCord
+ShockCord.ShockCord = Tirante de suspensión
+! Bulkhead
+Bulkhead.Bulkhead = Disco de enganche
+
+!Rocket
+Rocket.motorCount.Nomotor = [Sin motores]
+Rocket.compname.Rocket = Cohete
+
+!MotorMount
+MotorMount.IgnitionEvent.AUTOMATIC = Automático (Lanzamiento o carga de eyección)
+MotorMount.IgnitionEvent.LAUNCH = Lanzamiento
+MotorMount.IgnitionEvent.EJECTION_CHARGE = Primera carga de eyección de la etapa previa
+MotorMount.IgnitionEvent.BURNOUT = Primer encendido de la etapa previa
+MotorMount.IgnitionEvent.NEVER = Nunca
+
+!ComponentIcons
+ComponentIcons.Nosecone = Ojiva
+ComponentIcons.Bodytube = Cuerpo tubular
+ComponentIcons.Transition = Transición
+ComponentIcons.Trapezoidalfinset = Aleta trapezoidal
+ComponentIcons.Ellipticalfinset = Aleta elíptica
+ComponentIcons.Freeformfinset = Aleta de forma libre
+ComponentIcons.Launchlug = Tubo para Guía
+ComponentIcons.Innertube = Tubo interior
+ComponentIcons.Tubecoupler = Tubo de acoplamiento
+ComponentIcons.Centeringring = Anillo de centrado
+ComponentIcons.Bulkhead = Disco de enganche
+ComponentIcons.Engineblock = Retén de motor
+ComponentIcons.Parachute = Paracaídas
+ComponentIcons.Streamer = Banderola
+ComponentIcons.Shockcord = Tirante de suspensión
+ComponentIcons.Masscomponent = Componente masa
+ComponentIcons.disabled = (Desconectado)
+
+! StageAction
+StageAction.Stage = Etapa
+
+! RecoveryDevice
+RecoveryDevice.DeployEvent.LAUNCH = Lanzamiento (NN segundos)
+RecoveryDevice.DeployEvent.EJECTION = Primera carga de eyección de esta etapa
+RecoveryDevice.DeployEvent.APOGEE = Apogeo
+RecoveryDevice.DeployEvent.ALTITUDE = Altura específica durante el descenso
+RecoveryDevice.DeployEvent.NEVER = Nunca
+
+! FlightEvent
+FlightEvent.Type.LAUNCH = Lanzamiento
+FlightEvent.Type.IGNITION = Encendido del motor
+FlightEvent.Type.LIFTOFF = Despegue
+FlightEvent.Type.LAUNCHROD = Abandono de la Guía de lanzamiento
+FlightEvent.Type.BURNOUT = Apagado del motor
+FlightEvent.Type.EJECTION_CHARGE = Carga de eyección
+FlightEvent.Type.STAGE_SEPARATION = Separación de etapa
+FlightEvent.Type.APOGEE = Apogeo
+FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Despliegue del sistema de recuperación
+FlightEvent.Type.GROUND_HIT = Contacto con el suelo
+FlightEvent.Type.SIMULATION_END = Fin de la simulación
+FlightEvent.Type.ALTITUDE = Altitud
+
+! ThrustCurveMotorColumns
+TCurveMotorCol.MANUFACTURER = Fabricante
+TCurveMotorCol.DESIGNATION = Designación
+TCurveMotorCol.TYPE = Tipo
+TCurveMotorCol.DIAMETER = Diámetro
+TCurveMotorCol.LENGTH = Longitud
+
+! RocketInfo
+RocketInfo.lengthLine.Length = Longitud
+RocketInfo.lengthLine.maxdiameter = Diámetro máximo
+RocketInfo.massText1 = Masa con motores
+RocketInfo.massText2 = Masa sin motores
+RocketInfo.at = a M=
+RocketInfo.cgText = CG:
+RocketInfo.cpText = CP:
+RocketInfo.stabText = Estabilidad:
+RocketInfo.Warning = Peligro, cohete inestable.
+RocketInfo.Calculating = Calculando...
+RocketInfo.Apogee = Apogeo:
+RocketInfo.Maxvelocity = Velocidad Máx.:
+RocketInfo.Maxacceleration = Aceleración Máx.:
+RocketInfo.apogeeValue = N/A
+RocketInfo.Mach = Número Mach.
+RocketInfo.velocityValue = N/A
+RocketInfo.accelerationValue = N/A
+
+! FinSet
+FinSet.CrossSection.SQUARE = Cuadrado
+FinSet.CrossSection.ROUNDED = Redondeado
+FinSet.CrossSection.AIRFOIL = Aerodinámico
+FinSet.TabRelativePosition.FRONT = Borde principal del extremo de anclaje
+FinSet.TabRelativePosition.CENTER = Borde principal del anclaje
+FinSet.TabRelativePosition.END = Borde principal de tracción
+
+! FlightDataType
+FlightDataType.TYPE_TIME = Tiempo
+FlightDataType.TYPE_ALTITUDE = Altitud
+FlightDataType.TYPE_VELOCITY_Z = Velocidad vertical
+FlightDataType.TYPE_ACCELERATION_Z = Aceleración vertical
+FlightDataType.TYPE_VELOCITY_TOTAL = Velocidad total
+FlightDataType.TYPE_ACCELERATION_TOTAL = Aceleración total
+FlightDataType.TYPE_POSITION_X = Posición contra el viento
+FlightDataType.TYPE_POSITION_Y = Posición a favor del viento
+FlightDataType.TYPE_POSITION_XY = Distancia lateral
+FlightDataType.TYPE_POSITION_DIRECTION = Dirección lateral
+FlightDataType.TYPE_VELOCITY_XY = Velocidad lateral
+FlightDataType.TYPE_ACCELERATION_XY = Aceleración lateral
+FlightDataType.TYPE_AOA = Ángulo de ataque
+FlightDataType.TYPE_ROLL_RATE = Relación de rotación
+FlightDataType.TYPE_PITCH_RATE = Relación de pico
+FlightDataType.TYPE_YAW_RATE = Relación de desvío
+FlightDataType.TYPE_MASS = Masa
+FlightDataType.TYPE_LONGITUDINAL_INERTIA = Momento de inercia longitudinal
+FlightDataType.TYPE_ROTATIONAL_INERTIA = Momento de inercia rotacional
+FlightDataType.TYPE_CP_LOCATION = Situación del CP
+FlightDataType.TYPE_CG_LOCATION = Situación del CG
+FlightDataType.TYPE_STABILITY = Calibración del margen de estabilidad
+FlightDataType.TYPE_MACH_NUMBER = Número Mach
+FlightDataType.TYPE_REYNOLDS_NUMBER = Número de Reynolds
+FlightDataType.TYPE_THRUST_FORCE = Empuje
+FlightDataType.TYPE_DRAG_FORCE = Fuerza de rozamiento
+FlightDataType.TYPE_DRAG_COEFF = Coeficiente de rozamiento
+FlightDataType.TYPE_AXIAL_DRAG_COEFF = Coeficiente de rozamiento axial
+FlightDataType.TYPE_FRICTION_DRAG_COEFF = Coeficiente de rozamiento por fricción
+FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Presión del coeficiente de rozamiento
+FlightDataType.TYPE_BASE_DRAG_COEFF = Coeficiente de rozamiento base
+FlightDataType.TYPE_NORMAL_FORCE_COEFF = Coeficiente de rozamiento normal
+FlightDataType.TYPE_PITCH_MOMENT_COEFF = Pico del coeficiente de rozamiento
+FlightDataType.TYPE_YAW_MOMENT_COEFF = Coeficiente de rozamiento de desviación
+FlightDataType.TYPE_SIDE_FORCE_COEFF = Coeficiente de fuerza lateral
+FlightDataType.TYPE_ROLL_MOMENT_COEFF = Coeficiente del momento de rotación
+FlightDataType.TYPE_ROLL_FORCING_COEFF = Fuerza del coeficiente de rotación
+FlightDataType.TYPE_ROLL_DAMPING_COEFF = Disminución del coeficiente de rotación
+FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Disminución del coeficiente de pico
+FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Disminución del coeficiente de desviación
+FlightDataType.TYPE_REFERENCE_LENGTH = Longitud de referencia
+FlightDataType.TYPE_REFERENCE_AREA = Área de referencia
+FlightDataType.TYPE_ORIENTATION_THETA = Orientación vertical (zenit)
+FlightDataType.TYPE_ORIENTATION_PHI = Orientación lateral (azimut)
+FlightDataType.TYPE_WIND_VELOCITY = Velocidad del viento
+FlightDataType.TYPE_AIR_TEMPERATURE = Temperatura del aire
+FlightDataType.TYPE_AIR_PRESSURE = Presión del aire
+FlightDataType.TYPE_SPEED_OF_SOUND = Velocidad del sonido
+FlightDataType.TYPE_TIME_STEP = Simulación del tiempo de etapa
+FlightDataType.TYPE_COMPUTATION_TIME = Cálculo del tiempo
+FlightDataType.TYPE_LATITUDE = Latitud
+FlightDataType.TYPE_LONGITUDE = Longitud
+FlightDataType.TYPE_CORIOLIS_ACCELERATION = Aceleración Coriolis
+
+! PlotConfiguration
+PlotConfiguration.Verticalmotion = Movimiento vertical vs. Tiempo
+PlotConfiguration.Totalmotion = Movimiento total vs. Tiempo
+PlotConfiguration.Flightside = Perfil lateral de vuelo
+PlotConfiguration.Stability = Estabilidad vs. Tiempo
+PlotConfiguration.Dragcoef = Coeficiente de rozamiento vs. Número Mach
+PlotConfiguration.Rollcharacteristics = Características de rotación
+PlotConfiguration.Angleofattack = Ángulo de orientación y ataque vs. Tiempo
+PlotConfiguration.Simulationtime = Simulación del tiempo de etapa y cálculo del tiempo
+
+! Warning
+Warning.LargeAOA.str1 = Evaluación de la amplitud del ángulo de ataque.
+Warning.LargeAOA.str2 = La amplitud del ángulo de ataque es excesiva (
+Warning.DISCONTINUITY = Discontinuidad en el diámetro del fuselaje.
+Warning.THICK_FIN = Las aletas gruesas no están correctamente modeladas.
+Warning.JAGGED_EDGED_FIN = El perfil afilado de las aletas puede ser inexacto.
+Warning.LISTENERS_AFFECTED = Las Extensiones se ejecutaron con la simulación del vuelo
+Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Sistema de recuperación abierto en fase de impulso, mientras el motor aún empujaba
+Warning.FILE_INVALID_PARAMETER = Parámetro encontrado no válido. Ignorado.
+
+
+! Scale dialog
+ScaleDialog.lbl.scaleRocket = El Cohete entero
+ScaleDialog.lbl.scaleSubselection = Todos los componentes seleccionados
+ScaleDialog.lbl.scaleSelection = Sólo el componente seleccionado
+ScaleDialog.title = Dimensión del diseño
+ScaleDialog.lbl.scale = Dimensión:
+ScaleDialog.lbl.scale.ttip = Indique si desea dimensionar el diseño completo o sólo los componentes seleccionados
+ScaleDialog.lbl.scaling = Dimensión a aplicar:
+ScaleDialog.lbl.scaling.ttip = Tamaño resultante, valores por encima del 100% aumentan el tamaño, y valores por debajo de 100% reduce el diseño.
+! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"
+ScaleDialog.lbl.scaleFrom = Dimensionar desde
+ScaleDialog.lbl.scaleTo = hasta
+ScaleDialog.lbl.scaleFromTo.ttip = Definir la dimensión en base a una longitud conocida u original.
+ScaleDialog.checkbox.scaleMass = Actualizar valores de Masa especificada
+ScaleDialog.checkbox.scaleMass.ttip = Dimensionar la Masa del componente y recalcular los valores de Masa por el cubo del factor de la escala
+ScaleDialog.button.scale = Dimensionar
+ScaleDialog.undo.scaleRocket = Dimensionar el cohete
+ScaleDialog.undo.scaleComponent = Dimensionar el componente
+ScaleDialog.undo.scaleComponents = Dimensionar los componentes
+
+!icons
+Icons.Undo = Deshacer
+Icons.Redo = Rehacer
+
+OpenRocketPrintable.Partsdetail = Detalle de las partes
+OpenRocketPrintable.Fintemplates = Plantilla de las aletas
+OpenRocketPrintable.DesignReport = Informe del Diseño
+
+OpenRocketDocument.Redo = Rehacer
+OpenRocketDocument.Undo = Deshacer
+
+!EllipticalFinSet
+EllipticalFinSet.Ellipticalfinset = Grupo de aletas elípticas
+
+! Optimization
+
+! Modifiers
+
+optimization.modifier.nosecone.length = Longitud de la ojiva
+optimization.modifier.nosecone.length.desc = Optimizar la longitud de la ojiva.
+optimization.modifier.nosecone.diameter = Diámetro de la ojiva optimization.modifier.nosecone.diameter.desc = Optimizar el diámetro de la base de la ojiva.
+optimization.modifier.nosecone.thickness = Grosor de la ojiva
+optimization.modifier.nosecone.thickness.desc = Optimizar el grosor de la pared de la ojiva.
+optimization.modifier.nosecone.shapeparameter = Parámetro de forma
+optimization.modifier.nosecone.shapeparameter.desc = Optimiza el parámetro de forma de la ojiva.
+
+optimization.modifier.transition.length = Longitud
+optimization.modifier.transition.length.desc = Optimiza la longitud de la transición.
+optimization.modifier.transition.forediameter = Diámetro delantero
+optimization.modifier.transition.forediameter.desc = Optimiza el diámetro delantero de la transición.
+optimization.modifier.transition.aftdiameter = Diámetro trasero
+optimization.modifier.transition.aftdiameter.desc = Optimiza el diámetro trasero de la transición.
+optimization.modifier.transition.thickness = Grosor
+optimization.modifier.transition.thickness.desc = Optimiza el grosor de la pared de la transición.
+optimization.modifier.transition.shapeparameter = Parámetro de forma
+optimization.modifier.transition.shapeparameter.desc = Optimizar el parámetro de forma de la transición.
+
+optimization.modifier.bodytube.length = Longitud
+optimization.modifier.bodytube.length.desc = Optimizar la longitud del cuerpo.
+optimization.modifier.bodytube.outerDiameter = Diámetro exterior
+optimization.modifier.bodytube.outerDiameter.desc = Optimizar el diámetro exterior del cuerpo manteniendo el grosor de la pared.
+optimization.modifier.bodytube.thickness = Grosor
+optimization.modifier.bodytube.thickness.desc = Optimizar el grosor de la pared del cuerpo.
+
+optimization.modifier.trapezoidfinset.rootChord = Longitud línea base
+optimization.modifier.trapezoidfinset.rootChord.desc = Optiminizar la longitud de la línea base de las aletas (longitud de la aleta sobre la superficie del cuerpo).
+optimization.modifier.trapezoidfinset.tipChord = Longitud borde superior
+optimization.modifier.trapezoidfinset.tipChord.desc = Optimizar la longitud del borde superior de las aletas (longitd del borde exterior de la aleta).
+optimization.modifier.trapezoidfinset.sweep = Desplazamiento borde superior
+optimization.modifier.trapezoidfinset.sweep.desc = Optimiza el desplazamiento del borde superior de las aletas (desplazamiento del borde superior de la aleta respecto del extremo delantero de la línea base).
+optimization.modifier.trapezoidfinset.height = Altura
+optimization.modifier.trapezoidfinset.height.desc = Optimizar la altura de las aletas (semi-spam).
+
+optimization.modifier.ellipticalfinset.length = Longitud línea base
+optimization.modifier.ellipticalfinset.length.desc = Optiminizar la longitud de la línea base de las aletas
+optimization.modifier.ellipticalfinset.height = Altura
+optimization.modifier.ellipticalfinset.height.desc = Optimizar la altura de las aletas (semi-spam).
+
+optimization.modifier.finset.cant = Angulo de ataque
+optimization.modifier.finset.cant.desc = Optimiza el ángulo de ataque de las aletas.
+optimization.modifier.finset.position = Posición
+optimization.modifier.finset.position.desc = Optimiza la posición de las aletas a lo largo del cuerpo del cohete.
+
+optimization.modifier.launchlug.length = Longitud
+optimization.modifier.launchlug.length.desc = Optimiza la longitud del tubo para la Guía.
+optimization.modifier.launchlug.outerDiameter = Diámetro exterior
+optimization.modifier.launchlug.outerDiameter.desc = Optimiza el diámetro exterior del tubo para la Guía.
+optimization.modifier.launchlug.thickness = Grosor
+optimization.modifier.launchlug.thickness.desc = Optimiza el grosor del tubo para la Guía manteniendo el diámetro exterior.
+optimization.modifier.launchlug.position = Posición
+optimization.modifier.launchlug.position.desc = Optimiza la posición del soporte para la guía a lo largo del cuerpo del cohete.
+
+
+optimization.modifier.internalcomponent.position = Posición
+optimization.modifier.internalcomponent.position.desc = Optimiza la posición del componente interno respecto del componente que lo contiene.
+
+optimization.modifier.masscomponent.mass = Masa
+optimization.modifier.masscomponent.mass.desc = Optimiza la masa del componente Masa.
+
+optimization.modifier.parachute.diameter = Diámetro
+optimization.modifier.parachute.diameter.desc = Optimiza el diámetro del pabellón del paracaídas.
+optimization.modifier.parachute.coefficient = Coeficiente de rozamiento
+optimization.modifier.parachute.coefficient.desc = Optimiza el coeficiente de rozamiento del paracaídas. Un paracaídas típico posee un coeficiente de 0.8.
+
+optimization.modifier.streamer.length = Longitud
+optimization.modifier.streamer.length.desc = Optimiza la longitud de la banderola.
+optimization.modifier.streamer.width = Anchura
+optimization.modifier.streamer.width.desc = Optimiza la anchura de la banderola.
+optimization.modifier.streamer.aspectRatio = Relación de aspecto
+optimization.modifier.streamer.aspectRatio.desc = Optimiza la relación de aspecto de la banderola (longitud/anchura). Usted NO debe seleccionar una longitud o anchura de la banderola al mismo tiempo que una relación de aspecto.
+optimization.modifier.streamer.coefficient = Coeficiente de rozamiento
+optimization.modifier.streamer.coefficient.desc = Optimiza el coeficiente de rozamiento de la banderola.
+
+optimization.modifier.recoverydevice.deployDelay = Retardo de eyección
+optimization.modifier.recoverydevice.deployDelay.desc = Optimiza el tiempo de retardo de eyección del sistema de recuperación.
+optimization.modifier.recoverydevice.deployAltitude = Altitud de eyección
+optimization.modifier.recoverydevice.deployAltitude.desc = Optimiza la altitud de la eyección del sistema de recuperación.
+
+optimization.modifier.rocketcomponent.overrideMass = Masa especificada
+optimization.modifier.rocketcomponent.overrideMass.desc = Optimiza la Masa especificada del componente.
+optimization.modifier.rocketcomponent.overrideCG = CG especificado
+optimization.modifier.rocketcomponent.overrideCG.desc = Optimiza la localización del Centro de Gravedad especificado en el componente.
+
+optimization.modifier.motormount.overhang = Sobresalida del motor
+optimization.modifier.motormount.overhang.desc = Optimiza la sobresalida del motor hacia el exterior.
+optimization.modifier.motormount.delay = Retardo de ignición
+optimization.modifier.motormount.delay.desc = Optimiza el retardo de la ingnición del motor.
+
+
+
+
+! General rocket design optimization dialog
+
+GeneralOptimizationDialog.title = Optimización del cohete
+GeneralOptimizationDialog.goal.maximize = Maximizar el valor
+GeneralOptimizationDialog.goal.minimize = Minimizar el valor
+GeneralOptimizationDialog.goal.seek = Buscar el valor de
+GeneralOptimizationDialog.btn.start = Iniciar optimización
+GeneralOptimizationDialog.btn.stop = Detener optimización
+GeneralOptimizationDialog.lbl.paramsToOptimize = Parámetros de optimización:
+GeneralOptimizationDialog.btn.add = Agregar
+GeneralOptimizationDialog.btn.add.ttip = Agregar el parámetro de optimizacaión
+GeneralOptimizationDialog.btn.remove = Eliminar
+GeneralOptimizationDialog.btn.remove.ttip = Eliminar el parámetro seleccionado de la optimización.
+GeneralOptimizationDialog.btn.removeAll = Eliminar todo
+GeneralOptimizationDialog.btn.removeAll.ttip = Eliminar todos los parámetros de optimización.
+GeneralOptimizationDialog.lbl.availableParams = Parámetros disponibles:
+GeneralOptimizationDialog.lbl.optimizationOpts = Opciones de optimización
+GeneralOptimizationDialog.lbl.optimizeSim = Optimizar simulación:
+GeneralOptimizationDialog.lbl.optimizeSim.ttip = Seleccionar la simulación a optimizar.
+GeneralOptimizationDialog.lbl.optimizeValue = Valor optimizado:
+GeneralOptimizationDialog.lbl.optimizeValue.ttip = Seleccionar el valor a optimizar.
+GeneralOptimizationDialog.lbl.optimizeGoal = Objetivo de optimización:
+GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Seleccionar el objetivo de la optimización.
+GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Buscar valor personalizado
+GeneralOptimizationDialog.lbl.requireStability = Estabilidad requerida
+GeneralOptimizationDialog.lbl.requireMinStability = Mínima estabilidad:
+GeneralOptimizationDialog.lbl.requireMinStability.ttip = Requerir un margen mínimo de estabilidad para el diseño.
+GeneralOptimizationDialog.lbl.requireMaxStability = Máxima estabilidad:
+GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Requerir un margen máximo de estabilidad para el diseño.
+GeneralOptimizationDialog.status.bestValue = El mejor valor:
+GeneralOptimizationDialog.status.bestValue.ttip = El mejor valor de optimización encontrado.
+GeneralOptimizationDialog.status.stepCount = Número de pasos:
+GeneralOptimizationDialog.status.stepCount.ttip = Número de pasos que deben realizarse para la optimización.
+GeneralOptimizationDialog.status.evalCount = Evaluaciones:
+GeneralOptimizationDialog.status.evalCount.ttip = Número total de evaluaciones (simulaciones) que deben realizarse.
+GeneralOptimizationDialog.status.stepSize = Tamaño del paso:
+GeneralOptimizationDialog.status.stepSize.ttip = Tamaño actual del paso de optimización (respecto al rango de parámetros de optimización).
+GeneralOptimizationDialog.btn.plotPath = Gráfica del proceso
+GeneralOptimizationDialog.btn.plotPath.ttip = Gráfica del proceso de optimización (sólo para 1 o 2 dimensiones).
+GeneralOptimizationDialog.btn.save = Guardar resultados
+GeneralOptimizationDialog.btn.save.ttip = Guardar los resultados de las evaluaciones (simulaciones) en un archivo CSV.
+GeneralOptimizationDialog.btn.apply = Aplicar optimización
+GeneralOptimizationDialog.btn.apply.ttip = Aplicar los resultados de la optimización al diseño del cohete.
+GeneralOptimizationDialog.btn.reset = Reiniciar
+GeneralOptimizationDialog.btn.reset.ttip = Reiniciar el diseño actual del cohete con el diseño optimizado.
+GeneralOptimizationDialog.btn.close = Cerrar
+GeneralOptimizationDialog.btn.close.ttip = Cerrar el cuadro de diálogo sin modificar el diseño actual del cohete.
+GeneralOptimizationDialog.error.selectParams.text = Primero seleccione algunos parámetros a optimizar de entre todos los parámetros disponibles.
+GeneralOptimizationDialog.error.selectParams.title = Seleccionar los parámetros de optimización
+GeneralOptimizationDialog.error.optimizationFailure.text = Falló la ejecución de la optimización:
+GeneralOptimizationDialog.error.optimizationFailure.title = Fallo de la optimización
+GeneralOptimizationDialog.undoText = Aplicar la optimización
+GeneralOptimizationDialog.basicSimulationName = Simulación básica
+GeneralOptimizationDialog.noSimulationName = Sin simulación
+GeneralOptimizationDialog.table.col.parameter = Parámetro
+GeneralOptimizationDialog.table.col.current = Actual
+GeneralOptimizationDialog.table.col.min = Mínimo
+GeneralOptimizationDialog.table.col.max = Máximo
+GeneralOptimizationDialog.export.header = Incluir línea de cabecera
+GeneralOptimizationDialog.export.header.ttip = Incluir una línea de cabecera en la que se indican las descripciones.
+GeneralOptimizationDialog.export.stability = Estabilidad
+
+
+! Dialog for plotting optimization results
+OptimizationPlotDialog.title = Resultados de la optimización
+OptimizationPlotDialog.lbl.zoomInstructions = Click y arrastrar abajo+derecha para acercar Zoom, arriba+izquierda para alejar Zoom
+OptimizationPlotDialog.plot1d.title = Resultado de la optimización
+OptimizationPlotDialog.plot1d.series = Resultado de la optimización
+OptimizationPlotDialog.plot2d.title = Trazabilidad de la optimización
+OptimizationPlotDialog.plot2d.path = Trazabilidad de la optimización
+OptimizationPlotDialog.plot2d.evals = Evaluaciones
+OptimizationPlotDialog.plot.ttip.stability = Estabilidad:
+OptimizationPlotDialog.plot.label.optimum = Óptimo
+
+! Optimization parameters
+MaximumAltitudeParameter.name = Altitud en apogeo
+MaximumVelocityParameter.name = Velocidad máxima
+MaximumAccelerationParameter.name = Aceleración máxima
+StabilityParameter.name = Estabilidad
+GroundHitVelocityParameter.name = Velocidad de aterrizaje
+LandingDistanceParameter.name = Distancia de aterrizaje
+TotalFlightTimeParameter.name = Tiempo total de vuelo
+DeploymentVelocityParameter.name = Velocidad durante la eyección
+
+
+! Compass directions drawn on a compass rose.
+CompassRose.lbl.north = N
+CompassRose.lbl.east = E
+CompassRose.lbl.south = S
+CompassRose.lbl.west = W
+
+! Compass directions with subdirections. These might not be localized even if the directions on the compass rose are.
+CompassSelectionButton.lbl.N = N
+CompassSelectionButton.lbl.NE = NE
+CompassSelectionButton.lbl.E = E
+CompassSelectionButton.lbl.SE = SE
+CompassSelectionButton.lbl.S = S
+CompassSelectionButton.lbl.SW = SW
+CompassSelectionButton.lbl.W = W
+CompassSelectionButton.lbl.NW = NW
+
+
+SlideShowDialog.btn.next = Next
+SlideShowDialog.btn.prev = Previous
+
+GuidedTourSelectionDialog.title = Guided tours
+GuidedTourSelectionDialog.lbl.selectTour = Select guided tour:
+GuidedTourSelectionDialog.lbl.description = Tour description:
+GuidedTourSelectionDialog.lbl.length = Number of slides:
+GuidedTourSelectionDialog.btn.start = Start tour!
+
--- /dev/null
+\r
+#\r
+# French base translation file\r
+# Translated by Tripoli France\r
+# Should you need to add new logical keys here is the proposed method\r
+#\r
+# className.ComponentType.componentName\r
+#\r
+#\r
+# Text tokens within braces should not be translated, e.g.\r
+# "The file '{filename}' exists."\r
+# They are pieces that are inserted dynamically.\r
+#\r
+\r
+! Set to the name of the current translation file (used for debugging purposes)\r
+debug.currentFile = messages_fr.properties\r
+\r
+! RocketActions\r
+RocketActions.checkbox.Donotaskmeagain = Ne plus me demander\r
+RocketActions.lbl.Youcanchangedefop = Vous pouvez changer le mode opératoire par defaut dans les préferences.\r
+RocketActions.showConfirmDialog.lbl1 = Supprimer les simulations sélectionnées?\r
+RocketActions.showConfirmDialog.lbl2 = <html><i>Cette opération n'est pas réversible.</i>\r
+RocketActions.showConfirmDialog.title = Effacer les simulations\r
+RocketActions.DelCompAct.Delete = Effacer\r
+RocketActions.DelCompAct.ttip.Delete = Effacer la pièce sélectionnée.\r
+RocketActions.DelSimuAct.Delete = Effacer\r
+RocketActions.DelSimuAct.ttip.Delete = Effacer la simulation sélectionnée.\r
+RocketActions.DelAct.Delete = Effacer \r
+RocketActions.DelAct.ttip.Delete = Effacer la pièce ou la simulation sélectionnée.\r
+RocketActions.CutAction.Cut = Couper\r
+RocketActions.CutAction.ttip.Cut = Couper cette pièce ou simulation, l'ajouter au presse papier et l'enlever du projet\r
+RocketActions.CopyAct.Copy = Copier\r
+RocketActions.CopyAct.ttip.Copy = Copier les pièces (et les pièces liées) dans le presse papier.\r
+RocketActions.PasteAct.Paste = Coller\r
+RocketActions.PasteAct.ttip.Paste = Coller la pièce ou simulation présente dans le presse papier dans le projet.\r
+RocketActions.EditAct.Edit = Modifier\r
+RocketActions.EditAct.ttip.Edit = Modifier la pièce sélectionnée.\r
+RocketActions.NewStageAct.Newstage = Nouvel étage\r
+RocketActions.NewStageAct.ttip.Newstage = Ajouter un nouvel étage au projet.\r
+RocketActions.ActBoosterstage = Etage Booster\r
+RocketActions.MoveUpAct.Moveup = Monter\r
+RocketActions.MoveUpAct.ttip.Moveup = Monter la pièce.\r
+RocketActions.MoveDownAct.Movedown = Descendre\r
+RocketActions.MoveDownAct.ttip.Movedown = Descendre la pièce.\r
+\r
+! RocketPanel\r
+RocketPanel.FigTypeAct.Sideview = Vue de coté\r
+RocketPanel.FigTypeAct.ttip.Sideview = Vue de coté\r
+RocketPanel.FigTypeAct.Backview = Vue arrière\r
+RocketPanel.FigTypeAct.ttip.Backview = Vue arrière \r
+RocketPanel.lbl.Motorcfg = Configuration Moteur:\r
+RocketPanel.lbl.infoMessage = <html>Cliquer pour sélectionner Shift+cliquer pour sélectionner plusieurs Double-cliquer pour modifier Click+déplacer pour déplacer\r
+\r
+\r
+! BasicFrame\r
+BasicFrame.SimpleFileFilter1 = Tous les fichiers fusée (*.ork; *.rkt)\r
+BasicFrame.SimpleFileFilter2 = Fichiers OpenRocket (*.ork)\r
+BasicFrame.SimpleFileFilter3 = Fichiers RockSim (*.rkt)\r
+BasicFrame.tab.Rocketdesign = Projet fusée\r
+BasicFrame.tab.Flightsim = Simulations de vol\r
+BasicFrame.title.Addnewcomp = Ajouter une nouvelle pièce\r
+BasicFrame.dlg.lbl1 = Le projet '\r
+BasicFrame.dlg.lbl2 = ' N'a pas été sauvegardé.\r
+BasicFrame.dlg.lbl3 = Voulez vous le sauvegarder?\r
+BasicFrame.dlg.title = Projet non sauvegardé\r
+BasicFrame.StageName.Sustainer = Sustainer\r
+BasicFrame.WarningDialog.txt1 = Les problèmes suivant sont survenus lors de l'ouverture de\r
+BasicFrame.WarningDialog.txt2 = Certains éléments du projet n'ont peut être pas été chargé correctement.\r
+BasicFrame.WarningDialog.title = Avertissement lors de l'ouverture du fichier\r
+\r
+! General error messages used in multiple contexts\r
+error.fileExists.title = Le fichier existe déjà\r
+error.fileExists.desc = Le fichier '{filename}' existe déjà. Voulez vous l'ecraser?\r
+\r
+error.writing.title = Erreur d'éciture du fichier\r
+error.writing.desc = Une erreur est survenue lors de l'écriture dans le fichier:\r
+\r
+! Labels used in buttons of dialog windows\r
+button.ok = OK\r
+button.cancel = Annuler\r
+button.close = Fermer\r
+\r
+! Common labels used in buttons of dialog windows\r
+dlg.but.ok = Accepter\r
+dlg.but.cancel = Annuler\r
+dlg.but.close = Fermer\r
+\r
+\r
+! General file type names\r
+filetypes.pdf = fichier PDF\r
+\r
+\r
+! About Dialog\r
+AboutDialog.lbl.version = Version\r
+! The texts below provide additional credits for the translation maintainer\r
+! - In AboutDialog.lbl.translation replace "English" with the current language.\r
+! - AboutDialog.lbl.translator is the translator / group name (may be empty)\r
+! - AboutDialog.lbl.translatorWebsite is a URL to the translator / group (may be empty)\r
+! - AboutDialog.lbl.translatorIcon is the file name of an icon under pix/translators/ (may be empty)\r
+AboutDialog.lbl.translation = Traduit en français par:\r
+AboutDialog.lbl.translator = Tripoli France\r
+AboutDialog.lbl.translatorWebsite = http://tripoli.france.free.fr/\r
+AboutDialog.lbl.translatorIcon = logoTripoliFrance.png\r
+\r
+! Print dialog\r
+PrintDialog.title = Imprimer ou exporter\r
+PrintDialog.but.previewAndPrint = Pré-visualiser et imprimer\r
+PrintDialog.checkbox.showByStage = Montrer par étage\r
+PrintDialog.lbl.selectElements = Choisir les éléments à inclure:\r
+printdlg.but.saveaspdf = Sauvegarder en PDF\r
+printdlg.but.preview = Prévisualisation\r
+printdlg.but.settings = Configuration\r
+PrintDialog.error.preview.title = Impossible d'ouvrir la prévisualisation\r
+PrintDialog.error.preview.desc1 = Impossible d'ouvrir la prévisualisation PDF.\r
+PrintDialog.error.preview.desc2 = S'il vous plait utilisez l'option "Sauvegarder en PDF" à la place.\r
+\r
+\r
+!PrintSettingsDialog\r
+PrintSettingsDialog.title = Configuration impression\r
+PrintSettingsDialog.lbl.Templatefillcolor = Couleur de remplissage du modèle:\r
+PrintSettingsDialog.lbl.Templatebordercolor = Couleur des bords du modèle:\r
+PrintSettingsDialog.lbl.Papersize = Dimensions du papier:\r
+PrintSettingsDialog.lbl.Paperorientation = Orientation du papier:\r
+PrintSettingsDialog.but.Reset = Réinitialiser\r
+PrintSettingsDialog.but.Close = Fermer\r
+\r
+\r
+! Bug Report dialog\r
+bugreport.dlg.title = Rapport d'erreurs\r
+bugreport.dlg.but.Sendbugreport = Envoyer un rapport d'erreurs\r
+bugreport.dlg.but.Sendbugreport.Ttip = Envoyer automatiquement un rapport d'erreurs aux développeurs d'OpenRocket\r
+bugreport.dlg.successmsg1 = Rapport d'erreurs envoyé avec succès.\r
+bugreport.dlg.successmsg2 = Merci d'avoir contribué à l'amélioration d'OpenRocket!\r
+bugreport.dlg.successmsg3 = Rapport d'erreurs envoyé\r
+bugreport.dlg.connectedInternet = <html>Si vous êtes connecté sur Internet, vous pouvez tout simplement cliquer sur <em>Envoyer un rapport d'erreurs</em>.\r
+bugreport.dlg.otherwise = Sinon envoyez le texte ci-dessous à l'adresse:\r
+bugreport.lbl.Theinformation = Les informations ci-dessus sont susceptibles d'être incluse dans un rapport d'erreur publique. Assurez-vous qu'il ne contienne pas d'informations sensibles que vous ne voulez pas rendre publique.\r
+bugreport.dlg.failedmsg1 = OpenRocket n'a pas réussi à envoyer le rapport d'erreur:\r
+bugreport.dlg.failedmsg2 = S'il vous plait envoyez le rapport manuellement à\r
+bugreport.dlg.failedmsg3 = Erreur d'envoi du rapport\r
+bugreport.reportDialog.txt = <html><b>Vous pouvez signaler une erreur avec OpenRocket en remplissant et en envoyant le message ci-dessous.</b><br>Vous pouvez également signaler des erreurs et inclure des pièces jointes sur le site web du projet.\r
+bugreport.reportDialog.txt2 = <html><b>S'il vous plait ajoutez une courte description de ce que vous faisiez lorsque l'erreur s'est produite.</b>\r
+bugreport.dlg.provideDescription = S'il vous plait veuillez fournir d'abord une description du bug.\r
+bugreport.dlg.provideDescription.title = La description du bug est absente\r
+\r
+\r
+! Debug log dialog\r
+debuglogdlg.but.clear = Effacer\r
+debuglogdlg.OpenRocketdebuglog = Fichier debug d'OpenRocket\r
+debuglogdlg.Displayloglines = Afficher les numéros des lignes:\r
+debuglogdlg.Follow = Suivre\r
+debuglogdlg.col.Time = Heure\r
+debuglogdlg.col.Level = Niveau\r
+debuglogdlg.col.Location = Emplacement\r
+debuglogdlg.col.Message = Message\r
+debuglogdlg.lbl.Loglinenbr = Numéro de la ligne:\r
+debuglogdlg.lbl.Time = Heure:\r
+debuglogdlg.lbl.Level = Niveau:\r
+debuglogdlg.lbl.Location = Emplacement:\r
+debuglogdlg.lbl.Logmessage = Texte du message:\r
+debuglogdlg.lbl.Stacktrace = Stack trace:\r
+\r
+\r
+! Edit Motor configuration dialog\r
+edtmotorconfdlg.but.removemotor = Enlever le moteur\r
+edtmotorconfdlg.but.Selectmotor = Choisir le moteur\r
+edtmotorconfdlg.but.Removeconfiguration = Supprimer la configuration\r
+edtmotorconfdlg.but.Newconfiguration = Nouvelle configuration\r
+edtmotorconfdlg.lbl.Motormounts = <html><b>Portes moteur:</b>\r
+edtmotorconfdlg.title.Editmotorconf = Changer la configuration moteur\r
+edtmotorconfdlg.selectcomp = <html>Choisir les pièces utilisées par le porte moteur:\r
+edtmotorconfdlg.lbl.Motorconfig = <html><b>Configurations moteur:</b>\r
+edtmotorconfdlg.lbl.Configname = Nom de la configuration:\r
+edtmotorconfdlg.lbl.Leavenamedefault = Laisser le champ vide par défaut.\r
+\r
+! Example design dialog\r
+exdesigndlg.but.open = Ouvrir\r
+exdesigndlg.lbl.Selectexample = Choisir l'exemple de projet à ouvrir:\r
+exdesigndlg.lbl.Openexampledesign = Ouvrir un exemple de projet\r
+exdesigndlg.lbl.Exampledesignsnotfound = Impossible de trouver les exemples de projets.\r
+exdesigndlg.lbl.Examplesnotfound = Exemples non trouvés\r
+\r
+\r
+! Material edit panel\r
+matedtpan.but.new = Nouveau\r
+matedtpan.but.edit = Editer\r
+matedtpan.but.delete = Effacer\r
+matedtpan.but.revertall = Revenir aux valeurs précédentes\r
+matedtpan.col.Material = Matériaux\r
+matedtpan.col.Type = Type\r
+matedtpan.col.Density = Densité\r
+matedtpan.col.but.ttip.New = Ajouter un nouveau matériau\r
+matedtpan.title.Addcustmaterial = Ajouter un matériau personnalisé\r
+matedtpan.but.ttip.edit = Modifier un matériau existant\r
+matedtpan.title.Editmaterial = Modifier un matériau\r
+matedtpan.title2.Editmaterial = Les matériaux prédéfinis ne peuvent pas être modifiés.\r
+matedtpan.but.ttip.delete = Supprimer un matériau personnalisé\r
+matedtpan.but.ttip.revertall = Supprimer tous les matériaux personnalisés\r
+matedtpan.title.Deletealluser-defined = Effacer tous les matériaux personalisés?\r
+matedtpan.title.Revertall = Revenir aux valeurs précédentes?\r
+matedtpan.lbl.edtmaterials = Modifier les matériaux n'affectera pas les projets fusée existants.\r
+\r
+!MaterialModel\r
+MaterialModel.title.Material = Matériau\r
+MaterialModel.title.Defcustmat = Définir un matériau personnalisé\r
+\r
+\r
+! Preference dialog\r
+pref.dlg.but.add = Ajouter\r
+pref.dlg.but.reset = Réinitialiser\r
+pref.dlg.but.checknow = Vérifier maintenant\r
+pref.dlg.but.defaultmetric = Système métrique\r
+pref.dlg.but.defaultimperial = Système impérial\r
+pref.dlg.title.Preferences = Préférences \r
+pref.dlg.tab.Units = Unités\r
+pref.dlg.tab.Defaultunits = Unités par défaut\r
+pref.dlg.tab.Materials = Matériaux\r
+pref.dlg.tab.Custommaterials = Matériaux personnalisés\r
+pref.dlg.tab.Options = Options\r
+pref.dlg.tab.Miscellaneousoptions = Autres options\r
+pref.dlg.lbl.Positiontoinsert = Position pour insérer des composants internes:\r
+pref.dlg.lbl.Confirmdeletion = Confirmer l'effacement des simulations:\r
+pref.dlg.lbl.User-definedthrust = Courbes de poussée personnalisées:\r
+pref.dlg.Allthrustcurvefiles = Tous les fichiers de courbes de poussée (*.eng; *.rse; *.zip; répertoires)\r
+pref.dlg.RASPfiles = Fichiers moteur RASP (*.eng)\r
+pref.dlg.RockSimfiles = Fichiers moteur RockSim (*.rse)\r
+pref.dlg.ZIParchives = Archives ZIP (*.zip)\r
+pref.dlg.checkbox.Checkupdates = Rechercher les mises à jour au démarrage\r
+pref.dlg.ttip.Checkupdatesnow = Recherchez les mises à jour maintenant\r
+pref.dlg.lbl.Selectprefunits = Choisissez vos unités favorites:\r
+pref.dlg.lbl.Rocketdimensions = Dimensions de la fusée:\r
+pref.dlg.lbl.Linedensity = Epaisseur des lignes:\r
+pref.dlg.lbl.Motordimensions = Dimensions du moteur:\r
+pref.dlg.lbl.Surfacedensity = Densité de la Surface:\r
+pref.dlg.lbl.Distance = Distance:\r
+pref.dlg.lbl.Bulkdensity = Densité apparente:\r
+pref.dlg.lbl.Velocity = Vitesse:\r
+pref.dlg.lbl.Surfaceroughness = Rugosité de la Surface:\r
+pref.dlg.lbl.Acceleration = Accélération:\r
+pref.dlg.lbl.Area = Surface:\r
+pref.dlg.lbl.Mass = Masse:\r
+pref.dlg.lbl.Angle = Angle:\r
+pref.dlg.lbl.Force = Force:\r
+pref.dlg.lbl.Rollrate = Taux de roulis:\r
+pref.dlg.lbl.Totalimpulse = Impulsion totale:\r
+pref.dlg.lbl.Temperature = Température:\r
+pref.dlg.lbl.Momentofinertia = Moment d'inertie:\r
+pref.dlg.lbl.Pressure = Pression:\r
+pref.dlg.lbl.Stability = Stabilité:\r
+pref.dlg.lbl.FlightTime = Durée du vol:\r
+pref.dlg.lbl.effect1 = Les changements prendront effet la prochaine fois que vous ouvrirez une fenêtre.\r
+pref.dlg.lbl.Checkingupdates = Recherche des mises à jour...\r
+pref.dlg.lbl.msg1 = Une erreur est survenue durant la communication avec le serveur.\r
+pref.dlg.lbl.msg2 = Incapable de récupérer les informations de mise à jour\r
+pref.dlg.lbl.msg3 = Vous utilisez la dernière version d'OpenRocket.\r
+pref.dlg.lbl.msg4 = Pas de mises à jour disponible\r
+pref.dlg.PrefChoiseSelector1 = Toujours demander\r
+pref.dlg.PrefChoiseSelector2 = Insérer au milieu\r
+pref.dlg.PrefChoiseSelector3 = Ajouter à la fin\r
+pref.dlg.PrefBooleanSelector1 = Supprimer\r
+pref.dlg.PrefBooleanSelector2 = Confirmer\r
+pref.dlg.Add = Ajouter\r
+pref.dlg.DescriptionArea.Adddirectories = Ajouter des répertoires, des fichiers moteurs RASP (*.eng), des fichiers moteurs RockSim (*.rse) ou des fichiers archives ZIP séparés par un point virgule (;) pour charger des courbes de poussées externes. Les changements prendront effet au prochain démarrage d'OpenRocket.\r
+\r
+PreferencesDialog.lbl.language = Langue du programme:\r
+PreferencesDialog.languages.default = Valeur système par défaut\r
+PreferencesDialog.lbl.languageEffect = La langue sera changée après avoir redémarré OpenRocket.\r
+\r
+! Simulation edit dialog\r
+simedtdlg.but.runsimulation = Lancer la simulation\r
+simedtdlg.but.resettodefault = Restaurer les paramètres par défaut\r
+simedtdlg.but.add = Ajouter\r
+simedtdlg.but.remove = Enlever\r
+simedtdlg.title.Editsim = Modifier la simulation\r
+simedtdlg.lbl.Simname = Nom de la simulation:\r
+simedtdlg.tab.Launchcond = Conditions de lancement\r
+simedtdlg.tab.Simopt = Options de simulation\r
+simedtdlg.tab.Plotdata = Tracer les données\r
+simedtdlg.tab.Exportdata = Exporter les données\r
+simedtdlg.lbl.Motorcfg = Configuration moteur:\r
+simedtdlg.lbl.ttip.Motorcfg = Choisir la configuration moteur à utiliser.\r
+simedtdlg.combo.ttip.motorconf = Choisir la configuration moteur à utiliser.\r
+simedtdlg.lbl.Wind = Vent\r
+simedtdlg.lbl.Averwindspeed = Vitesse moyenne du vent:\r
+simedtdlg.lbl.ttip.Averwindspeed = Vitesse moyenne du vent par rapport au sol.\r
+simedtdlg.lbl.Stddeviation = Dérive standard:\r
+simedtdlg.lbl.ttip.Stddeviation = <html>La dérive standard de la vitesse du vent.<br>La vitesse du vent est le double de l'écart-type de la moyenne dans 95% des cas.\r
+simedtdlg.lbl.Turbulenceintensity = Intensité de la turbulence:\r
+simedtdlg.lbl.ttip.Turbulenceintensity1 = <html>L'intensité de la turbulence résulte de la division de la dérive par la vitesse moyenne de vent.<br>\r
+simedtdlg.lbl.ttip.Turbulenceintensity2 = Les valeurs typiques vont de \r
+simedtdlg.lbl.ttip.Turbulenceintensity3 = à\r
+simedtdlg.border.Atmoscond = Conditions atmosphériques\r
+simedtdlg.checkbox.InterStdAtmosphere = Utiliser les paramètres de l'Atmosphère Standard\r
+simedtdlg.checkbox.ttip.InterStdAtmosphere1 = <html>Sélectionner pour utiliser les paramètres de l'Atmosphère Standard.<br>Ce modèle à une température de\r
+simedtdlg.checkbox.ttip.InterStdAtmosphere2 = et une pression de \r
+simedtdlg.checkbox.ttip.InterStdAtmosphere3 = au niveau de la mer.\r
+simedtdlg.lbl.Temperature = Température:\r
+simedtdlg.lbl.ttip.Temperature = Température du site de lancement.\r
+simedtdlg.lbl.Pressure = Pression:\r
+simedtdlg.lbl.ttip.Pressure = Pression atmosphérique du site de lancement.\r
+simedtdlg.lbl.Launchsite = Site de lancement\r
+simedtdlg.lbl.Latitude = Latitude:\r
+simedtdlg.lbl.ttip.Latitude = <html>La latitude du site de lancement affecte l'attraction gravitationnelle de la Terre.<br>> Les valeurs positives sont dans l'hémisphère Nord, les valeurs négatives sur l'hémisphère Sud.\r
+\r
+simedtdlg.lbl.Longitude = Longitude:\r
+simedtdlg.lbl.ttip.Longitude = <html>Nécessaire pour les prédictions du temps and elevation models.\r
+\r
+simedtdlg.lbl.Altitude = Altitude:\r
+simedtdlg.lbl.ttip.Altitude = <html>Altitude du site de lancement par rapport au niveau de la mer.<br>Cela affecte la position de la fusée dans le modèle atmosphérique.\r
+simedtdlg.border.Launchrod = Rampe de lancement\r
+simedtdlg.lbl.Length = Longueur:\r
+simedtdlg.lbl.ttip.Length = Longueur de la rampe.\r
+simedtdlg.lbl.Angle = Angle:\r
+simedtdlg.lbl.ttip.Angle = Angle de la rampe de lancement par rapport à la verticale.\r
+simedtdlg.lbl.Direction = Direction:\r
+simedtdlg.lbl.ttip.Direction1 = <html>Direction de la rampe de lance par rapport au vent.<br>\r
+simedtdlg.lbl.ttip.Direction2 = = Face au vent,\r
+simedtdlg.lbl.ttip.Direction3 = = vent arrière.\r
+simedtdlg.border.Simopt = Options de simulation\r
+simedtdlg.lbl.Calcmethod = Méthode de calcul:\r
+simedtdlg.lbl.ttip.Calcmethod = <html>La méthode Barrowman étendue calcule les forces aérodynamique selon <br>les équations de Barrowman étendues pour arranger plus de pièces.\r
+simedtdlg.lbl.ExtBarrowman = Barrowman étendu\r
+simedtdlg.lbl.Simmethod = Méthode de Simulation:\r
+simedtdlg.lbl.ttip.Simmethod1 = <html>Le simulateur de six degrés de liberté permet la liberté totale de fusée en vol.<br>\r
+simedtdlg.lbl.ttip.Simmethod2 = Integration is performed using a 4<sup>th</sup> order Runge-Kutta 4 numerical integration.\r
+simedtdlg.lbl.GeodeticMethod = Calculs Geodetic:\r
+simedtdlg.lbl.ttip.GeodeticMethodTip = Relate to the calculation of coordinates on the earth. This also enables coriolis effect computations.\r
+simedtdlg.lbl.Timestep = Réglage du pas de temps:\r
+simedtdlg.lbl.ttip.Timestep1 = <html>Le temps entre les étapes de la simulation.<br>Avec un pas de temps plus petit la simulation est plus lente mais également plus précise.<br>\r
+simedtdlg.lbl.ttip.Timestep2 = The 4<sup>th</sup> order simulation method is quite accurate with a time step of\r
+simedtdlg.but.ttip.resettodefault = Réinitialiser le pas de temps à sa valeur par défaut (\r
+simedtdlg.border.Simlist = Auditeurs de simulation\r
+simedtdlg.txt.longA1 = <html><i>Les auditeurs de simulation</i> sont une fonction avancé qui permet à l'utilisateur d'écrire du code pour suivre et interagir avec la simulation. \r
+simedtdlg.txt.longA2 = Pour plus de détails sur les auditeurs de simulation, reférez vous à la documentation technique d'OpenRocket.\r
+simedtdlg.lbl.Curlist = Auditeurs de simulation actuel:\r
+simedtdlg.lbl.Addsimlist = Ajouter un "auditeur de simulation"\r
+simedtdlg.lbl.Noflightdata = Aucune donnée de vol disponible.\r
+simedtdlg.lbl.runsimfirst = S'il vous plait faites tourner la simulation d'abord.\r
+simedtdlg.chart.Simflight = Vol simulé\r
+simedtdlg.dlg.Simres = Résultats de la simulation\r
+simedtdlg.IntensityDesc.None = Aucune\r
+simedtdlg.IntensityDesc.Verylow = Très basse\r
+simedtdlg.IntensityDesc.Low = Basse\r
+simedtdlg.IntensityDesc.Medium = Moyenne\r
+simedtdlg.IntensityDesc.High = Haute\r
+simedtdlg.IntensityDesc.Veryhigh = Très haute\r
+simedtdlg.IntensityDesc.Extreme = Extrême\r
+\r
+GeodeticComputationStrategy.none.name = Aucune\r
+GeodeticComputationStrategy.none.desc = Ne pas faire de calculs geodetic.\r
+GeodeticComputationStrategy.spherical.name = Approximation sphérique\r
+GeodeticComputationStrategy.spherical.desc = <html>Perform geodetic computations assuming a spherical Earth.<br>This is sufficiently accurate for almost all purposes.\r
+GeodeticComputationStrategy.wgs84.name = ellipsoïde WGS84\r
+GeodeticComputationStrategy.wgs84.desc = <html>Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.<br>Slower and unnecessary in most cases.\r
+\r
+\r
+\r
+! Simulation Panel\r
+simpanel.but.newsimulation = Nouvelle simulation\r
+simpanel.but.editsimulation = Modifier la simulation\r
+simpanel.but.runsimulations = Lancer les simulations\r
+simpanel.but.deletesimulations = Effacer les simulations\r
+simpanel.but.plotexport = Tracer / exporter\r
+simpanel.but.ttip.newsimulation = Ajouter une nouvelle simulation\r
+simpanel.but.ttip.editsim = Modifier la simulation sélectionnée\r
+simpanel.but.ttip.runsimu = Recommencer la simulation sélectionnée\r
+simpanel.but.ttip.deletesim = Effacer les simulations sélectionnées\r
+simpanel.checkbox.donotask = Ne plus me demander\r
+simpanel.lbl.defpref = Vous pouvez changer le mode opératoire par défaut dans préférences.\r
+simpanel.dlg.lbl.DeleteSim1 = Effacer les simulations sélectionnées?\r
+simpanel.dlg.lbl.DeleteSim2 = <html><i>Cette opération n'est pas réversible.</i>\r
+simpanel.dlg.lbl.DeleteSim3 = Effacer les simulations\r
+simpanel.col.Name = Nom\r
+simpanel.col.Motors = Moteurs\r
+simpanel.col.Apogee = Apogée\r
+simpanel.col.Maxvelocity = Vitesse Max.\r
+simpanel.col.Maxacceleration = Accélération Max.\r
+simpanel.col.Timetoapogee = Temps pour atteindre l'apogée\r
+simpanel.col.Flighttime = Temps de vol\r
+simpanel.col.Groundhitvelocity = Vitesse à l'atterrissage\r
+\r
+! SimulationRunDialog\r
+SimuRunDlg.title.RunSim = Simulations en cour...\r
+SimuRunDlg.lbl.Running = En cour ...\r
+SimuRunDlg.lbl.Simutime = Temps de simulation:\r
+SimuRunDlg.lbl.Altitude = Altitude:\r
+SimuRunDlg.lbl.Velocity = Vitesse:\r
+SimuRunDlg.msg.Unabletosim = Simulation impossible:\r
+SimuRunDlg.msg.errorOccurred = Une erreur s'est produite durant la simulation:\r
+SimuRunDlg.msg.AnException1 = Une exception s'est produite lors de la simulation:\r
+SimuRunDlg.msg.AnException2 = S'il vous plaît faites un rapport d'erreurs avec les détails ci-dessous.\r
+SimuRunDlg.msg.AssertionError1 = Une erreur de calcul s'est produite lors de la simulation.\r
+SimuRunDlg.msg.AssertionError2 = S'il vous plaît faites un rapport d'erreurs avec les détails ci-dessous.\r
+SimuRunDlg.msg.unknownerror1 = Une erreur inconnue s'est produite lors de la simulation.\r
+SimuRunDlg.msg.unknownerror2 = Le programme peut être instable, vous devez enregistrer toutes vos créations et redémarrez OpenRocket maintenant!\r
+\r
+\r
+\r
+! SimulationExportPanel\r
+SimExpPan.desc = Fichiers dont les données sont séparées par une virgule (*.csv)\r
+SimExpPan.border.Vartoexport = Variables à exporter\r
+SimExpPan.but.Selectall = Tout sélectionner\r
+SimExpPan.but.Selectnone = Ne rien sélectionner\r
+SimExpPan.border.Fieldsep = Séparateur de champ\r
+SimExpPan.lbl.Fieldsepstr = Séparateur de champ:\r
+SimExpPan.lbl.longA1 = <html>La chaîne utilisée pour séparer les champs dans le fichier exporté.<br>\r
+SimExpPan.lbl.longA2 = Utiliser ',' pour un fichier (CSV).\r
+SimExpPan.checkbox.Includesimudesc = Inclure la description de la simulation\r
+SimExpPan.checkbox.ttip.Includesimudesc = Inclure un commentaire au début du fichier pour décrire la simulation.\r
+SimExpPan.border.Comments = Commentaires\r
+SimExpPan.checkbox.Includefielddesc = Inclure les descriptions des champs\r
+SimExpPan.checkbox.ttip.Includefielddesc = Inclure une ligne de commentaire avec la description des variables exportées.\r
+SimExpPan.checkbox.Incflightevents = Inclure les événements de vol\r
+SimExpPan.checkbox.ttip.Incflightevents = Inclure une ligne de commentaire pour chaque évènement de vol.\r
+SimExpPan.lbl.Commentchar = Symbole pour les commentaires:\r
+SimExpPan.lbl.ttip.Commentchar = Le symbole utilisé pour une ligne de commentaires.\r
+SimExpPan.but.Exporttofile = Exporter dans un fichier...\r
+SimExpPan.Fileexists.desc1 = Le fichier \"\r
+SimExpPan.Fileexists.desc2 = \" existe déjà. Ecraser?\r
+SimExpPan.Fileexists.title = Le fichier existe\r
+SimExpPan.ExportingVar.desc1 = Exporter 1 variable sur un total de\r
+SimExpPan.ExportingVar.desc2 = Exportation\r
+SimExpPan.ExportingVar.desc3 = variable sur un total de\r
+SimExpPan.Col.Variable = Variable\r
+SimExpPan.Col.Unit = Unité\r
+\r
+\r
+CsvOptionPanel.separator.space = SPACE\r
+CsvOptionPanel.separator.tab = TAB\r
+\r
+\r
+\r
+! MotorPlot\r
+MotorPlot.title.Motorplot = Courbe du moteur\r
+MotorPlot.but.Select = Sélection\r
+MotorPlot.Chart.Motorthrustcurve = Courbe de poussée moteur\r
+MotorPlot.Chart.Time = Temps / s\r
+MotorPlot.Chart.Thrust = Poussée / N\r
+MotorPlot.txt.Designation = Désignation:\r
+MotorPlot.txt.Manufacturer = Manufacturer:\r
+MotorPlot.txt.Type = Type:\r
+MotorPlot.txt.Delays = Retards:\r
+MotorPlot.txt.Comment = Commentaires:\n\r
+\r
+\r
+\r
+! Simulation plot panel\r
+simplotpanel.lbl.Presetplotconf = Prédéfinir les paramètres du tracé:\r
+simplotpanel.lbl.Xaxistype = Axe des X:\r
+simplotpanel.lbl.Unit = Unités:\r
+simplotpanel.lbl.Yaxistypes = Axe des Y:\r
+simplotpanel.lbl.Flightevents = Evénements du vol:\r
+simplotpanel.but.All = Tous\r
+simplotpanel.but.None = Aucun\r
+simplotpanel.but.NewYaxisplottype = Nouveau type de tracé de l'axe Y\r
+simplotpanel.but.Plotflight = Tracer le vol\r
+simplotpanel.lbl.Axis = Axes:\r
+simplotpanel.but.ttip.Removethisplot = Effacer le tracé\r
+simplotpanel.Desc = Les données seront tracées en fonction du temps même si le type d'Axe des abscisses n'est pas le temps.\r
+simplotpanel.OptionPane.lbl1 = Un maximum de 15 tracés est permis. \r
+simplotpanel.OptionPane.lbl2 = Impossible d'ajouter le tracé\r
+simplotpanel.AUTO_NAME = Auto\r
+simplotpanel.LEFT_NAME = Gauche\r
+simplotpanel.RIGHT_NAME = Droite\r
+simplotpanel.CUSTOM = Personnalisé\r
+\r
+! Component add buttons\r
+compaddbuttons.Bodycompandfinsets = Pièces du corps et ailerons\r
+compaddbuttons.Nosecone = Cône\r
+compaddbuttons.Bodytube = Tube du\ncorps\r
+compaddbuttons.Transition = Transition\r
+compaddbuttons.Trapezoidal = Trapézoïdale\r
+compaddbuttons.Elliptical = Elliptique\r
+compaddbuttons.Freeform = Forme libre\r
+compaddbuttons.Launchlug = Tube de\nguidage\r
+compaddbuttons.Innercomponent = Pièces internes\r
+compaddbuttons.Innertube = Tube interne\r
+compaddbuttons.Coupler = Coupleur\r
+compaddbuttons.Centeringring = Anneau de\ncentrage\r
+compaddbuttons.Bulkhead = Cloison\r
+compaddbuttons.Engineblock = Bague de\nrétention\nmoteur\r
+compaddbuttons.Massobjects = Pièces pleines\r
+compaddbuttons.Parachute = Parachute\r
+compaddbuttons.Streamer = Banderole\r
+compaddbuttons.Shockcord = Cordon\namortisseur\r
+compaddbuttons.Masscomponent = Poids\r
+compaddbuttons.Donotaskmeagain = Ne plus me poser la question\r
+compaddbuttons.Selectcomppos = Position de la pièce\r
+compaddbuttons.lbl.Youcanchange = Vous pouvez modifier le fonctionnement par défaut dans les préférences.\r
+compaddbuttons.lbl.insertcomp = Insérez la pièce après l'élément actuel ou en tant que dernier élément?\r
+compaddbuttons.askPosition.Inserthere = Ajouter ici\r
+compaddbuttons.askPosition.Addtotheend = Ajouter à la fin\r
+compaddbuttons.askPosition.Cancel = Annuler\r
+\r
+! Component Analysis Dialog\r
+componentanalysisdlg.componentanalysis = Analyse pièce\r
+componentanalysisdlg.lbl.winddir = Direction du vent:\r
+componentanalysisdlg.TitledBorder.warnings = Avertissements:\r
+componentanalysisdlg.ToggleBut.worst = Pire\r
+componentanalysisdlg.lbl.angleofattack = Angle d'attaque:\r
+componentanalysisdlg.lbl.machnumber = Mach number:\r
+componentanalysisdlg.lbl.rollrate = Taux de roulis:\r
+componentanalysisdlg.lbl.activestages = Etages actifs:\r
+componentanalysisdlg.lbl.motorconf = Configuration moteur:\r
+componentanalysisdlg.TabStability.Col.Component = Pièce\r
+componentanalysisdlg.TabStability = Stabilité\r
+componentanalysisdlg.TabStability.ttip = Information de stabilité\r
+componentanalysisdlg.dragTableModel.Col.Component = Pièce\r
+componentanalysisdlg.dragTableModel.Col.Pressure = <html>Pression C<sub>D</sub>\r
+componentanalysisdlg.dragTableModel.Col.Base = <html>Base C<sub>D</sub>\r
+componentanalysisdlg.dragTableModel.Col.friction = <html>Friction C<sub>D</sub>\r
+componentanalysisdlg.dragTableModel.Col.total = <html>Total C<sub>D</sub>\r
+componentanalysisdlg.dragTabchar = Caractéristiques de traînée\r
+componentanalysisdlg.dragTabchar.ttip = Caractéristiques de traînée\r
+componentanalysisdlg.rollTableModel.Col.component = Pièce\r
+componentanalysisdlg.rollTableModel.Col.rollforc = Coefficient de forçage de roulis\r
+componentanalysisdlg.rollTableModel.Col.rolldamp = Coefficient amortisseur de roulis\r
+componentanalysisdlg.rollTableModel.Col.total = <html>Total C<sub>l</sub>\r
+componentanalysisdlg.rollTableModel = Dynamique du roulis\r
+componentanalysisdlg.rollTableModel.ttip = Dynamique du roulis\r
+componentanalysisdlg.println.closingmethod = Méthode de clôture appelée:\r
+componentanalysisdlg.println.settingnam = SETTING NAN VALUES\r
+componentanalysisdlg.lbl.reflenght = Longueur de référence: \r
+componentanalysisdlg.lbl.refarea = Aire de référence: \r
+!componentanalysisdlg.but.close =Fermer\r
+componentanalysisdlg.TabStability.Col.Component = Pièce\r
+\r
+! Custom Material dialog\r
+custmatdlg.title.Custommaterial = Matériau personnalisé\r
+custmatdlg.lbl.Materialname = Nom du matériau: \r
+custmatdlg.lbl.Materialtype = Type de matériau:\r
+custmatdlg.lbl.Materialdensity = Densité du matériau:\r
+custmatdlg.checkbox.Addmaterial = Ajouter la pièce dans la base de données\r
+\r
+\r
+! Ring Component Config\r
+ringcompcfg.OuterRadius = Diamètre extérieur\r
+ringcompcfg.Automatic = Automatique\r
+ringcompcfg.InnerRadius = Diamètre intérieur\r
+ringcompcfg.Thickness = Epaisseur\r
+ringcompcfg.Length = Longueur\r
+ringcompcfg.Positionrelativeto = Position relative à:\r
+ringcompcfg.plus = plus\r
+!ringcompcfg.PositionValue = PositionValue\r
+ringcompcfg.Radialdistance = Rayon:\r
+ringcompcfg.Distancefrom = Distance de l'axe central de la fusée\r
+ringcompcfg.Radialdirection = Azimut\r
+ringcompcfg.radialdirectionfrom = Sens par rapport à l'axe central de la fusée\r
+ringcompcfg.but.Reset = Réinitialisation\r
+ringcompcfg.but.Resetcomponant = Réinitialiser la pièce à l'axe de la fusée\r
+ringcompcfg.EngineBlock.desc = <html>Un <b>bloc moteur </b> empêche le moteur de se déplacer vers l'avant dans le tube porte moteur.<br><br>Pour ajouter un moteur, créer un <b>tube</b> ou un <b>tube interne</b> et marquer le comme porte moteur dans l'onglet <em>Moteur</em>.\r
+ringcompcfg.note.desc = A noter: Un tube interne n'affectera pas l'aérodynamisme de la fusée même si il est situé en dehors du tube.\r
+\r
+\r
+! Body Tube Config\r
+BodyTubecfg.lbl.Bodytubelength = Longueur du tube:\r
+BodyTubecfg.lbl.Outerdiameter = Diamètre externe:\r
+BodyTubecfg.lbl.Innerdiameter = Diamètre interne:\r
+BodyTubecfg.lbl.Wallthickness = Epaisseur des parois:\r
+BodyTubecfg.tab.General = Général\r
+BodyTubecfg.tab.Generalproperties = Propriétés générales\r
+BodyTubecfg.tab.Motor = Moteur\r
+BodyTubecfg.tab.Motormountconf = Configuration du porte moteur\r
+BodyTubecfg.checkbox.Automatic = Automatique\r
+BodyTubecfg.checkbox.Filled = Aspérités bouchées\r
+\r
+! FinSetConfig\r
+FinSetConfig.tab.Fintabs = Pattes des ailerons\r
+FinSetConfig.tab.Through-the-wall = Ailerons traversant le fuselage\r
+FinSetConfig.but.Converttofreeform = Convertir en forme libre\r
+FinSetConfig.but.Converttofreeform.ttip = Convertir ce jeu d'ailerons en forme libre\r
+FinSetConfig.Convertfinset = Convertir le jeu d'ailerons\r
+FinSetConfig.but.Splitfins = Séparer les ailerons\r
+FinSetConfig.but.Splitfins.ttip = Diviser le jeu d'ailerons en aileron indépendant\r
+FinSetConfig.lbl.Through-the-wall = Ailerons traversant le fuselage:\r
+FinSetConfig.lbl.Tablength = Longueur de la patte:\r
+FinSetConfig.ttip.Tablength = La longueur de la patte de l'aileron.\r
+FinSetConfig.lbl.Tabheight = Hauteur de la patte:\r
+FinSetConfig.ttip.Tabheight = La hauteur de l'envergure de la patte de l'aileron.\r
+FinSetConfig.lbl.Tabposition = Position de la patte:\r
+FinSetConfig.ttip.Tabposition = La position de la patte de l'aileron.\r
+FinSetConfig.lbl.relativeto = relative à\r
+\r
+! MotorDatabaseLoadingDialog\r
+MotorDbLoadDlg.title = Chargement des moteurs\r
+MotorDbLoadDlg.Loadingmotors = Chargement des moteurs...\r
+\r
+! RocketConfig\r
+RocketCfg.lbl.Designname = Nom du projet:\r
+RocketCfg.lbl.Designer = Concepteur:\r
+RocketCfg.lbl.Comments = Commentaires:\r
+RocketCfg.lbl.Revisionhistory = Historique des modifications:\r
+RocketCfg.lbl.Material = Matériaux:\r
+\r
+! ShockCordConfig\r
+ShockCordCfg.lbl.Shockcordlength = Longueur du cordon amortisseur\r
+\r
+! RocketComponentConfig\r
+RocketCompCfg.lbl.Componentname = Nom de la pièce:\r
+RocketCompCfg.ttip.Thecomponentname = Le nom de la pièce.\r
+RocketCompCfg.tab.Override = Forcer la valeur\r
+RocketCompCfg.tab.MassandCGoverride = Forçage de la Masse et du CG\r
+RocketCompCfg.tab.Figure = Forme\r
+RocketCompCfg.tab.Figstyleopt = Options de la forme\r
+RocketCompCfg.tab.Comment = Commentaires\r
+RocketCompCfg.tab.Specifyacomment = Commentaires concernant la pièce\r
+RocketCompCfg.lbl.Mass = Masse:\r
+RocketCompCfg.lbl.Componentmass = Masse de la pièce:\r
+RocketCompCfg.lbl.overriddento = (forcé à\r
+RocketCompCfg.lbl.overriddenby = (forcé par\r
+RocketCompCfg.lbl.Componentmaterial = Matériaux composant la pièce:\r
+RocketCompCfg.lbl.Componentfinish = Finition de la pièce:\r
+RocketCompCfg.lbl.ttip.componentmaterialaffects = Les matériaux utilisés pour la pièce affectent le poids de la pièce.\r
+RocketCompCfg.combo.ttip.componentmaterialaffects = Les matériaux utilisés pour la pièce affectent le poids de la pièce.\r
+RocketCompCfg.lbl.longA1 = <html>La finition de la pièce affecte l'aérodynamisme de la pièce.<br>\r
+RocketCompCfg.lbl.longA2 = La valeur indiquée est la hauteur moyenne de la rugosité de la surface.\r
+RocketCompCfg.but.Setforall = Appliquer à tous\r
+RocketCompCfg.but.ttip.Setforall = Régler la finition pour tous les composants de la fusée.\r
+RocketCompCfg.lbl.Overridemassorcenter = Forcer la masse ou le centre de gravité du \r
+RocketCompCfg.checkbox.Overridemass = Forcer la masse:\r
+RocketCompCfg.checkbox.Overridecenterofgrav = Forcer le centre de gravité:\r
+RocketCompCfg.checkbox.OverridemassandCG = Forcer la masse et le centre de gravité de tous les sous composants\r
+RocketCompCfg.lbl.longB1 = <html>Le forçage de la masse n'inclus pas le ou les moteurs.<br>\r
+RocketCompCfg.lbl.longB2 = Le centre de gravité est mesuré à partir de l'extrémité avant de la fusée\r
+RocketCompCfg.lbl.Commentsonthe = Commentaires à propos du \r
+RocketCompCfg.lbl.Figurestyle = Modèle de forme:\r
+RocketCompCfg.lbl.Componentcolor = Couleur de la pièce:\r
+RocketCompCfg.lbl.Choosecolor = Choisir la couleur\r
+RocketCompCfg.checkbox.Usedefaultcolor = Utiliser la couleur par défaut\r
+RocketCompCfg.lbl.Complinestyle = Style de lignes pour les pièces:\r
+RocketCompCfg.but.Saveasdefstyle = Sauver le modèle par défaut\r
+RocketCompCfg.lbl.Diameter = Diamètre:\r
+RocketCompCfg.lbl.Length = Longueur:\r
+RocketCompCfg.lbl.Thickness = Epaisseur:\r
+RocketCompCfg.checkbox.Endcapped = Arrière clos \r
+RocketCompCfg.ttip.Endcapped = Précise si l'arrière du cône est clos.\r
+RocketCompCfg.title.Noseconeshoulder = Accotement du cône\r
+RocketCompCfg.title.Aftshoulder = Accotement arrière\r
+RocketCompCfg.border.Foreshoulder = Accotement avant \r
+!RocketCompCfg.lbl.Length = Length:\r
+\r
+! BulkheadConfig\r
+BulkheadCfg.tab.Radius = Rayon:\r
+BulkheadCfg.tab.Thickness = Epaisseur:\r
+BulkheadCfg.tab.General = Général\r
+BulkheadCfg.tab.Generalproperties = Propriétés générales\r
+\r
+!CenteringRingConfig\r
+CenteringRingCfg.tab.Outerdiam = Diamètre externe:\r
+CenteringRingCfg.tab.Innerdiam = Diamètre interne:\r
+CenteringRingCfg.tab.Thickness = Epaisseur:\r
+CenteringRingCfg.tab.General = Général\r
+CenteringRingCfg.tab.Generalproperties = Propriétés Générales\r
+\r
+!ComponentConfigDialog\r
+ComponentCfgDlg.configuration =\r
+ComponentCfgDlg.configuration1 = configuration\r
+ComponentCfgDlg.Modify = Modifier\r
+\r
+!EllipticalFinSetConfig\r
+EllipticalFinSetCfg.Nbroffins = Nombre d'ailerons:\r
+EllipticalFinSetCfg.Rotation = Rotation:\r
+EllipticalFinSetCfg.Fincant = Inclinaison de l'aileron:\r
+EllipticalFinSetCfg.Rootchord = Emplanture:\r
+EllipticalFinSetCfg.Height = Hauteur:\r
+EllipticalFinSetCfg.Positionrelativeto = Position relative à:\r
+EllipticalFinSetCfg.plus = plus\r
+EllipticalFinSetCfg.FincrossSection = Coupe de l'aileron:\r
+EllipticalFinSetCfg.Thickness = Epaisseur:\r
+EllipticalFinSetCfg.General = Général\r
+EllipticalFinSetCfg.Generalproperties = Propriétés Générales\r
+EllipticalFinSetCfg.ttip.Fincant = Angle d'inclinaison des ailerons par rapport au corps de la fusée\r
+\r
+!FreeformFinSetConfig\r
+FreeformFinSetCfg.tab.General = Général\r
+FreeformFinSetCfg.tab.ttip.General = Propriétés générales\r
+FreeformFinSetCfg.tab.Shape = Forme\r
+FreeformFinSetCfg.tab.ttip.Finshape = Forme de l'aileron\r
+FreeformFinSetCfg.lbl.Numberoffins = Nombre d'ailerons:\r
+FreeformFinSetCfg.lbl.Finrotation = Rotation des ailerons:\r
+FreeformFinSetCfg.lbl.Fincant = Inclinaison de l'aileron:\r
+FreeformFinSetCfg.lbl.ttip.Fincant = angle d'inclinaison des ailerons par rapport au corps de la fusée.\r
+FreeformFinSetCfg.lbl.Posrelativeto = Position par rapport à:\r
+FreeformFinSetCfg.lbl.plus = plus\r
+FreeformFinSetCfg.lbl.FincrossSection = Coupe de l'aileron:\r
+FreeformFinSetCfg.lbl.Thickness = Epaisseur:\r
+! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle\r
+FreeformFinSetCfg.lbl.doubleClick1 = Double-click\r
+FreeformFinSetCfg.lbl.doubleClick2 = pour éditer\r
+FreeformFinSetCfg.lbl.clickDrag = Cliquer+déplacer: Ajouter et déplacer des points\r
+FreeformFinSetCfg.lbl.ctrlClick = Ctrl+cliquer: Enlever un point\r
+\r
+\r
+!InnerTubeConfig\r
+InnerTubeCfg.tab.Motor = Moteur\r
+InnerTubeCfg.tab.ttip.Motor = Configuration du porte moteur\r
+InnerTubeCfg.tab.Cluster = Cluster\r
+InnerTubeCfg.tab.ttip.Cluster = Configuration du cluster\r
+InnerTubeCfg.tab.Radialpos = Position circulaire\r
+InnerTubeCfg.tab.ttip.Radialpos = Position circulaire\r
+InnerTubeCfg.lbl.Selectclustercfg = Choisir la configuration du cluster:\r
+InnerTubeCfg.lbl.TubeSep = Séparation du tube:\r
+InnerTubeCfg.lbl.ttip.TubeSep = La Séparation des tubes, 1.0 = chacun se touche\r
+InnerTubeCfg.lbl.Rotation = Rotation:\r
+InnerTubeCfg.lbl.ttip.Rotation = Angle de rotation du cluster\r
+InnerTubeCfg.lbl.Rotangle = Angle de rotation de la configuration du cluster\r
+InnerTubeCfg.but.Splitcluster = Séparer le cluster\r
+InnerTubeCfg.lbl.longA1 = <html>séparer le cluster en pièces distinctes.<br>\r
+InnerTubeCfg.lbl.longA2 = Cela duplique également tous les composants rattacher à ce tube interne.\r
+InnerTubeCfg.but.Resetsettings = Réinitialiser les réglages\r
+InnerTubeCfg.but.ttip.Resetsettings = Réinitialiser la séparation et la rotation aux valeurs par défauts\r
+\r
+! LaunchLugConfig\r
+LaunchLugCfg.lbl.Length = Longueur:\r
+LaunchLugCfg.lbl.Outerdiam = Diamètre externe:\r
+LaunchLugCfg.lbl.Innerdiam = Diamètre interne:\r
+LaunchLugCfg.lbl.Thickness = Epaisseur:\r
+LaunchLugCfg.lbl.Radialpos = Position circulaire:\r
+LaunchLugCfg.lbl.Posrelativeto = Position relative à:\r
+LaunchLugCfg.lbl.plus = plus\r
+LaunchLugCfg.tab.General = Général\r
+LaunchLugCfg.tab.Generalprop = Propriétés Générales\r
+\r
+! MassComponentConfig\r
+MassComponentCfg.lbl.Mass = Masse\r
+MassComponentCfg.lbl.Length = Longueur\r
+MassComponentCfg.lbl.Diameter = Diamètre\r
+MassComponentCfg.lbl.PosRelativeto = Position relative à:\r
+MassComponentCfg.lbl.plus = plus\r
+MassComponentCfg.tab.General = Général\r
+MassComponentCfg.tab.ttip.General = Propriétés Générales\r
+MassComponentCfg.tab.Radialpos = Position sur le périmètre\r
+MassComponentCfg.tab.ttip.Radialpos = Configuration de la position sur le périmètre\r
+MassComponentCfg.lbl.Radialdistance = Rayon:\r
+MassComponentCfg.lbl.Radialdirection = Azimut:\r
+MassComponentCfg.but.Reset = Réinitialiser\r
+\r
+! MotorConfig\r
+MotorCfg.checkbox.compmotormount = Cette pièce est un porte moteur\r
+MotorCfg.lbl.Motorcfg = Configuration du moteur:\r
+MotorCfg.but.New = Nouveau\r
+MotorCfg.lbl.Currentmotor = Moteur actuel:\r
+MotorCfg.lbl.Motoroverhang = Surplomb du moteur:\r
+MotorCfg.lbl.Ignitionat = Allumage à:\r
+MotorCfg.lbl.plus = plus\r
+MotorCfg.lbl.seconds = secondes\r
+MotorCfg.lbl.longA1 = Le projet actuel n'a qu'un étage.\r
+MotorCfg.lbl.longA2 = Des étages peuvent-être ajoutés en cliquant \"Nouvel étage\".\r
+MotorCfg.lbl.longB1 = Le projet actuel a\r
+MotorCfg.lbl.longB2 = étage(s).\r
+MotorCfg.but.Selectmotor = Choisir le moteur\r
+MotorCfg.but.Removemotor = Enlever le moteur\r
+MotorCfg.lbl.motorLabel = Aucun\r
+\r
+! NoseConeConfig\r
+NoseConeCfg.lbl.Noseconeshape = Forme du cône de la fusée:\r
+NoseConeCfg.lbl.Shapeparam = Paramètre de la forme:\r
+NoseConeCfg.lbl.Noseconelength = Longueur du cône de la fusée:\r
+NoseConeCfg.lbl.Basediam = Diamètre de la base:\r
+NoseConeCfg.checkbox.Automatic = Automatique\r
+NoseConeCfg.lbl.Wallthickness = Epaisseur de la paroi:\r
+NoseConeCfg.checkbox.Filled = Aspérités bouchées\r
+NoseConeCfg.tab.General = Général\r
+NoseConeCfg.tab.ttip.General = Propriétés générales\r
+NoseConeCfg.tab.Shoulder = Accotement\r
+NoseConeCfg.tab.ttip.Shoulder = Propriétés de l'accotement\r
+\r
+! ParachuteConfig\r
+ParachuteCfg.lbl.Canopy = Canopée:\r
+ParachuteCfg.lbl.Diameter = Diamètre:\r
+ParachuteCfg.lbl.Material = Matériau:\r
+ParachuteCfg.combo.MaterialModel = La nature du matériau affecte le poids de la pièce.\r
+ParachuteCfg.lbl.longA1 = <html>Coefficient de traînée C<sub>D</sub>:\r
+ParachuteCfg.lbl.longB1 = <html>Le coefficient de traînée dépend de la surface totale du parachute.<br>\r
+ParachuteCfg.lbl.longB2 = Un plus grand coefficient de trainée produit une descente plus lente. \r
+ParachuteCfg.lbl.longB3 = Une valeur standard pour le parachute est 0.8.\r
+ParachuteCfg.but.Reset = Réinitialiser\r
+ParachuteCfg.lbl.Shroudlines = Suspentes:\r
+ParachuteCfg.lbl.Numberoflines = Nombre de suspentes:\r
+ParachuteCfg.lbl.Linelength = Longueur des suspentes:\r
+ParachuteCfg.lbl.Material = Matériau:\r
+ParachuteCfg.lbl.Posrelativeto = Position relative à:\r
+ParachuteCfg.lbl.plus = plus\r
+ParachuteCfg.lbl.Packedlength = Longueur plié:\r
+ParachuteCfg.lbl.Packeddiam = Diamètre plié:\r
+ParachuteCfg.lbl.Deploysat = Déploiement à:\r
+ParachuteCfg.lbl.seconds = secondes\r
+ParachuteCfg.lbl.Altitude = Altitude:\r
+ParachuteCfg.tab.General = Général\r
+ParachuteCfg.tab.ttip.General = Propriétés générales\r
+ParachuteCfg.tab.Radialpos = Position sur le périmètre\r
+ParachuteCfg.tab.ttip.Radialpos = Configuration de la position radial\r
+ParachuteCfg.lbl.Radialdistance = Rayon:\r
+ParachuteCfg.lbl.Radialdirection = Azimut:\r
+ParachuteCfg.but.Reset = Réinitialiser\r
+ParachuteCfg.lbl.plusdelay = Retard\r
+\r
+! ShockCordConfig \r
+ShockCordCfg.lbl.Shockcordlength = Longueur du cordon amortisseur\r
+ShockCordCfg.lbl.Shockcordmaterial = Matériau du cordon amortisseur:\r
+ShockCordCfg.lbl.Posrelativeto = Position relative à:\r
+ShockCordCfg.lbl.plus = plus\r
+ShockCordCfg.lbl.Packedlength = Longueur emballé:\r
+ShockCordCfg.lbl.Packeddiam = Diamètre emballé:\r
+ShockCordCfg.tab.General = Général\r
+ShockCordCfg.tab.ttip.General = Propriétés générales\r
+\r
+!SleeveConfig\r
+SleeveCfg.tab.Outerdiam = Diamètre externe:\r
+SleeveCfg.tab.Innerdiam = Diamètre interne:\r
+SleeveCfg.tab.Wallthickness = Epaisseur des parois:\r
+SleeveCfg.tab.Length = Longueur:\r
+SleeveCfg.tab.General = Général\r
+SleeveCfg.tab.Generalproperties = Propriétés générales\r
+\r
+! StreamerConfig\r
+StreamerCfg.lbl.Striplength = Longueur de la bande:\r
+StreamerCfg.lbl.Stripwidth = Largeur de la bande:\r
+StreamerCfg.lbl.Striparea = Surface de la bande:\r
+StreamerCfg.lbl.Aspectratio = Proportions:\r
+StreamerCfg.lbl.Material = Matériau:\r
+StreamerCfg.combo.ttip.MaterialModel = La nature du matériau affecte le poids de la pièce.\r
+StreamerCfg.lbl.longA1 = <html>Coefficient de traînée C<sub>D</sub>:\r
+StreamerCfg.lbl.longB1 = <html>Le coefficient de trainée dépend de la surface totale de la banderole.<br>\r
+StreamerCfg.lbl.longB2 = Un plus grand coefficient de trainée produit une descente plus lente.\r
+StreamerCfg.lbl.Automatic = Automatique\r
+StreamerCfg.lbl.longC1 = le coefficient de trainée dépend de la surface totale de la banderole.\r
+StreamerCfg.lbl.Posrelativeto = Position relative à:\r
+StreamerCfg.lbl.plus = plus\r
+StreamerCfg.lbl.Packedlength = Longueur emballé:\r
+StreamerCfg.lbl.Packeddiam = Diamètre emballé:\r
+StreamerCfg.lbl.Deploysat = Déploiement à:\r
+StreamerCfg.lbl.seconds = secondes\r
+StreamerCfg.lbl.Altitude = Altitude:\r
+StreamerCfg.tab.General = Général\r
+StreamerCfg.tab.ttip.General = Propriétés générales\r
+StreamerCfg.tab.Radialpos = Position sur le périmètre\r
+StreamerCfg.tab.ttip.Radialpos = Configuration de la position sur le périmètre\r
+StreamerCfg.lbl.Radialdistance = Rayon:\r
+StreamerCfg.lbl.Radialdirection = Azimut:\r
+StreamerCfg.but.Reset = Réinitialiser\r
+StreamerCfg.lbl.plusdelay = Retard\r
+\r
+! ThicknessRingComponentConfig\r
+ThicknessRingCompCfg.tab.Outerdiam = Diamètre externe:\r
+ThicknessRingCompCfg.tab.Innerdiam = Diamètre interne:\r
+ThicknessRingCompCfg.tab.Wallthickness = Epaisseur de la paroi:\r
+ThicknessRingCompCfg.tab.Length = Longueur:\r
+ThicknessRingCompCfg.tab.General = Général\r
+ThicknessRingCompCfg.tab.Generalprop = Propriétés générales\r
+\r
+! TransitionConfig\r
+TransitionCfg.lbl.Transitionshape = Forme de la transition:\r
+TransitionCfg.checkbox.Clipped = Emboitée\r
+TransitionCfg.lbl.Shapeparam = Paramètre de la forme:\r
+TransitionCfg.lbl.Transitionlength = Longueur de la transition:\r
+TransitionCfg.lbl.Forediam = Diamètre avant:\r
+TransitionCfg.checkbox.Automatic = Automatique\r
+TransitionCfg.lbl.Aftdiam = Diamètre arrière:\r
+TransitionCfg.lbl.Wallthickness = Epaisseur de la paroi:\r
+TransitionCfg.checkbox.Filled = Aspérités bouchées\r
+TransitionCfg.tab.General = Général\r
+TransitionCfg.tab.Generalproperties = Propriétés Générales\r
+TransitionCfg.tab.Shoulder = Accotement\r
+TransitionCfg.tab.Shoulderproperties = Propriétés de l'accotement \r
+\r
+! TrapezoidFinSetConfig\r
+TrapezoidFinSetCfg.lbl.Nbroffins = Nombre d'ailerons:\r
+TrapezoidFinSetCfg.lbl.ttip.Nbroffins = Le nombre d'ailerons composant le jeu.\r
+TrapezoidFinSetCfg.lbl.Finrotation = Rotation de l'aileron:\r
+TrapezoidFinSetCfg.lbl.ttip.Finrotation = Angle du premier aileron dans le jeu.\r
+TrapezoidFinSetCfg.lbl.Fincant = Inclinaison de l'aileron:\r
+TrapezoidFinSetCfg.lbl.ttip.Fincant = Angle d'inclinaison des ailerons par rapport au tube du corps de la fusée.\r
+TrapezoidFinSetCfg.lbl.Rootchord = Longueur de la base de l'aileron:\r
+TrapezoidFinSetCfg.lbl.Tipchord = Longueur du bout de l'aileron:\r
+TrapezoidFinSetCfg.lbl.Height = Hauteur:\r
+TrapezoidFinSetCfg.lbl.Sweeplength = Longueur du bord d'attaque:\r
+TrapezoidFinSetCfg.lbl.Sweepangle = Angle du bord d'attaque:\r
+TrapezoidFinSetCfg.lbl.FincrossSection = Coupe de l'aileron:\r
+TrapezoidFinSetCfg.lbl.Thickness = Epaisseur:\r
+TrapezoidFinSetCfg.lbl.Posrelativeto = Position relative à:\r
+TrapezoidFinSetCfg.lbl.plus = plus\r
+TrapezoidFinSetCfg.tab.General = Général\r
+TrapezoidFinSetCfg.tab.Generalproperties = Propriétés générales\r
+\r
+!MotorConfigurationModel\r
+MotorCfgModel.Editcfg = Modifier les configurations\r
+\r
+! StorageOptionChooser\r
+StorageOptChooser.lbl.Simdatatostore = Données simulées à stocker:\r
+StorageOptChooser.rdbut.Allsimdata = Toutes les données des simulations\r
+StorageOptChooser.lbl.longA1 = <html>Enregistrer toutes les données des simulations.<br>\r
+StorageOptChooser.lbl.longA2 = Cela peut entraîner de très gros fichiers!\r
+StorageOptChooser.rdbut.Every = Every\r
+StorageOptChooser.lbl.longB1 = <html>Store plottable values approximately this far apart.<br>\r
+StorageOptChooser.lbl.longB2 = Des valeurs plus grandes produisent des fichiers plus petits.\r
+StorageOptChooser.lbl.seconds = secondes\r
+StorageOptChooser.rdbut.Onlyprimfig = Seuls les chiffres primaires\r
+StorageOptChooser.lbl.longC1 = <html>Stocker seulement les valeurs montrées dans le tableau récapitulatif.<br>\r
+StorageOptChooser.lbl.longC2 = Cela produira des fichiers plus petit.\r
+StorageOptChooser.checkbox.Compfile = Compresse le fichier\r
+StorageOptChooser.lbl.UsingComp = Utiliser la compression réduit significativement la taille du fichier.\r
+StorageOptChooser.lbl.longD1 = Une estimation sur la taille qu'aurait le fichier résultant avec les options actuelles.\r
+StorageOptChooser.ttip.Saveopt = Options de sauvegarde\r
+StorageOptChooser.lbl.Estfilesize = Taille estimée du fichier:\r
+StorageOptChooser.lbl.Saveopt = Options de sauvegarde\r
+\r
+! ThrustCurveMotorSelectionPanel\r
+TCMotorSelPan.lbl.Selrocketmotor = Choisir le moteur fusée:\r
+TCMotorSelPan.checkbox.hideSimilar = Cacher les courbes de poussées similaires\r
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Montrer tous les moteurs\r
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Montrer les moteurs avec un diamètre inferieur au porte moteur\r
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Montrer les moteurs avec un diamètre égale au porte moteur\r
+TCMotorSelPan.lbl.Motormountdia = Diamètre du tube porte moteur:\r
+TCMotorSelPan.lbl.Search = Rechercher:\r
+TCMotorSelPan.lbl.Selectthrustcurve = Choisir la courbe de poussée:\r
+TCMotorSelPan.lbl.Ejectionchargedelay = Retard de la charge d'éjection:\r
+TCMotorSelPan.equalsIgnoreCase.None = Aucun\r
+TCMotorSelPan.lbl.NumberofsecondsorNone = (Nombre de secondes ou \"Aucun\")\r
+TCMotorSelPan.lbl.Totalimpulse = Impulsion totale:\r
+TCMotorSelPan.lbl.Avgthrust = Poussée moyenne:\r
+TCMotorSelPan.lbl.Maxthrust = Poussée Max.:\r
+TCMotorSelPan.lbl.Burntime = Temps de combustion:\r
+TCMotorSelPan.lbl.Launchmass = Masse au lancement:\r
+TCMotorSelPan.lbl.Emptymass = Masse à vide:\r
+TCMotorSelPan.lbl.Datapoints = Points de données:\r
+TCMotorSelPan.lbl.Digest = Assimilation:\r
+TCMotorSelPan.title.Thrustcurve = Courbe de poussée:\r
+TCMotorSelPan.title.Thrust = Poussée\r
+TCMotorSelPan.delayBox.None = Aucun\r
+\r
+\r
+! PlotDialog\r
+PlotDialog.title.Flightdataplot = Tracé du vol\r
+PlotDialog.Chart.Simulatedflight = Simulation du vol\r
+PlotDialog.CheckBox.Showdatapoints = Afficher un point pour chaque valeur\r
+PlotDialog.lbl.Chart = Cliquer+déplacer en bas +droite pour agrandir, haut+gauche pour rétrécir\r
+\r
+\r
+! "main" prefix is used for the main application dialog\r
+\r
+# FIXME: Rename the description keys \r
+\r
+main.menu.file = Fichier\r
+main.menu.file.desc = File-handling related tasks\r
+main.menu.file.new = Nouveau\r
+main.menu.file.new.desc = Crée un nouveau projet fusée\r
+main.menu.file.open = Ouvrir...\r
+BasicFrame.item.Openrocketdesign = Ouvre un projet fusée\r
+main.menu.file.openExample = Ouvrir un exemple...\r
+BasicFrame.item.Openexamplerocketdesign = Ouvre un exemple de projet fusée\r
+main.menu.file.save = Sauvegarder\r
+BasicFrame.item.SavecurRocketdesign = Sauvegarde le projet fusée en cours\r
+main.menu.file.saveAs = Sauvegarder sous...\r
+BasicFrame.item.SavecurRocketdesnewfile = Sauvegarde le projet fusée en cour dans un nouveau fichier\r
+main.menu.file.print = Imprimer/Exporter en PDF...\r
+main.menu.file.print.desc = Imprimer ou sauvegarde en PDF la liste des pièces et les gabaries des ailerons\r
+main.menu.file.close = Fermer\r
+BasicFrame.item.Closedesign = Ferme le projet fusée en cour\r
+main.menu.file.quit = Quitter\r
+BasicFrame.item.Quitprogram = Quitte le programme\r
+\r
+main.menu.edit = Modifier\r
+BasicFrame.menu.Rocketedt = Modification de la fusée\r
+main.menu.edit.undo = Annuler modification\r
+main.menu.edit.undo.desc = Annuler l'opération précédente\r
+main.menu.edit.redo = Refaire modification\r
+main.menu.edit.redo.desc = Refaire l'opération precedente qui avait été défaite\r
+main.menu.edit.cut = Couper\r
+main.menu.edit.copy = Copier\r
+main.menu.edit.paste = Coller\r
+main.menu.edit.delete = Effacer\r
+main.menu.edit.resize = Redimensionner...\r
+main.menu.edit.resize.desc = Redimensionner certaines parties de la fusée\r
+main.menu.edit.preferences = Préférences\r
+main.menu.edit.preferences.desc = Configure les préférences de l'application\r
+\r
+main.menu.analyze = Analyse\r
+main.menu.analyze.desc = Analyses de la fusée\r
+main.menu.analyze.componentAnalysis = Analyse des Pièces\r
+main.menu.analyze.componentAnalysis.desc = Analyse séparé des pices de la fusée\r
+main.menu.analyze.optimization = Optimisation de la fusée\r
+main.menu.analyze.optimization.desc = Optimisation generale de la fusée\r
+\r
+main.menu.help = Aide\r
+main.menu.help.desc = Information à propos d'OpenRocket\r
+main.menu.help.license = Licence\r
+main.menu.help.license.desc = Information sur la license d'OpenRocket\r
+main.menu.help.bugReport = Rapport d'erreurs\r
+main.menu.help.bugReport.desc = Information pour pouvoir sgnaler les bugs dans OpenRocket\r
+main.menu.help.debugLog = Debug log\r
+main.menu.help.debugLog.desc = Visualiser le fichier log d'OpenRocket\r
+main.menu.help.about = A propos\r
+main.menu.help.about.desc = Détails du Copyright d'OpenRocket\r
+\r
+main.menu.debug = Debug\r
+main.menu.debug.whatisthismenu = Quel est ce menu?\r
+main.menu.debug.createtestrocket = Créer une fusée test\r
+\r
+! database\r
+! Translate here all material database\r
+!\r
+\r
+! Material database\r
+! BULK_MATERIAL\r
+Databases.materials.Acrylic = Acrylique\r
+Databases.materials.Balsa = Balsa\r
+Databases.materials.Birch = Bouleau\r
+Databases.materials.Cardboard = Carton\r
+Databases.materials.Carbonfiber = Fibre de carbone\r
+Databases.materials.Cork = Liège\r
+Databases.materials.DepronXPS = Depron (XPS)\r
+Databases.materials.Fiberglass = Fibre de verre\r
+Databases.materials.Kraftphenolic = Kraft phénolique\r
+Databases.materials.Maple = Érable\r
+Databases.materials.Paperoffice = Papier (bureau)\r
+Databases.materials.Pine = Pin\r
+Databases.materials.Plywoodbirch = Contre-plaqué (bouleau)\r
+Databases.materials.PolycarbonateLexan = Polycarbonate (Lexan)\r
+Databases.materials.Polystyrene = Polystyrène\r
+Databases.materials.PVC = PVC\r
+Databases.materials.Spruce = Sapin\r
+Databases.materials.StyrofoamgenericEPS = Polystyrène (générique EPS)\r
+Databases.materials.StyrofoamBluefoamXPS = \"Mousse Bleue\" de polystyrène (XPS)\r
+Databases.materials.Quantumtubing = Tube Quantum\r
+Databases.materials.BlueTube = Blue tube\r
+!SURFACE_MATERIAL\r
+Databases.materials.Ripstopnylon = Ripstop nylon\r
+Databases.materials.Mylar = Mylar\r
+Databases.materials.Polyethylenethin = Polyéthylène (fin)\r
+Databases.materials.Polyethyleneheavy = Polyéthylène (lourd)\r
+Databases.materials.Silk = Soie\r
+Databases.materials.Paperoffice = Papier (bureau)\r
+Databases.materials.Cellophane = Cellophane\r
+Databases.materials.Crepepaper = Papier crépon\r
+! LINE_MATERIAL\r
+Databases.materials.Threadheavy-duty = Fil(résistant)\r
+Databases.materials.Elasticcordround2mm = Corde Elastique (ronde 2mm, 1/16 in)\r
+Databases.materials.Elasticcordflat6mm = Corde Elastique (plate 6mm, 1/4 in)\r
+Databases.materials.Elasticcordflat12mm = Corde Elastique (plate 12mm, 1/2 in)\r
+Databases.materials.Elasticcordflat19mm = Corde Elastique (plate 19mm, 3/4 in)\r
+Databases.materials.Elasticcordflat25mm = Corde Elastique (plate 25mm, 1 in)\r
+Databases.materials.Braidednylon2mm = Nylon tressé (2 mm, 1/16 in)\r
+Databases.materials.Braidednylon3mm = Nylon tressé (3 mm, 1/8 in)\r
+Databases.materials.Tubularnylon11mm = Nylon tubulaire (11 mm, 7/16 in)\r
+Databases.materials.Tubularnylon14mm = Nylon tubulaire (14 mm, 9/16 in)\r
+Databases.materials.Tubularnylon25mm = Nylon tubulaire (25 mm, 1 in)\r
+\r
+! ExternalComponent\r
+ExternalComponent.Rough = Rugueuse\r
+ExternalComponent.Unfinished = Non peinte\r
+ExternalComponent.Regularpaint = Peinture classique\r
+ExternalComponent.Smoothpaint = Fine couche\r
+ExternalComponent.Polished = Polie\r
+\r
+! LineStyle\r
+LineStyle.Solid = Ligne pleine\r
+LineStyle.Dashed = Tiret\r
+LineStyle.Dotted = Ligne pointillée\r
+LineStyle.Dash-dotted = Ligne Pointillée et Tiret\r
+LineStyle.Defaultstyle = Style par défaut\r
+\r
+! Shape\r
+Shape.Conical = Conique\r
+Shape.Conical.desc1 = Un cône conique a un profil triangulaire.\r
+Shape.Conical.desc2 = Une transition conique a des côtés droits.\r
+Shape.Ogive = Ogive\r
+Shape.Ogive.desc1 = Un cône ogival a un profil qui est un segment de cercle. La valeur du paramètre de forme 1 produit une <b>ogive tangente</b>, qui a une transition en douceur vers le tube de la fusée, des valeurs inférieures à 1 produisent des <b>ogives sécantes</b>.\r
+Shape.Ogive.desc2 = Une transition en ogive a un profil qui est un segment de cercle. La valeur du paramètre de forme 1 produit une <b>ogive tangente</b>, qui a une transition en douceur vers le tube de la fusée à l'extrémité arrière, des valeurs inférieures à 1 produisent des <b>ogives sécantes</b>.\r
+Shape.Ellipsoid = Ellipsoïde\r
+Shape.Ellipsoid.desc1 = Un cône ellipsoïdal a un profil d'une demi ellipse dont les axes principaux sont de longueurs 2×<i>la longueur</i> et <i>diamètre</i>.\r
+Shape.Ellipsoid.desc2 = Une transition ellipsoïdale a un profil d'une demi ellipse dont les axes principaux sont de longueurs 2×<i>longueur</i> et <i>diamètre</i>. Si la transition n'est pas coupée alors le profil est étendu au centre par le rayon correspondant. \r
+Shape.Powerseries = Série Haute puissance\r
+Shape.Powerseries.desc1 = Un cône de puissance a un profil de <i>Rayon</i> × (<i>x</i> / <i>Longueur</i>)<sup><i>k</i></sup> ou <i>k</i> est le paramètre de la forme. Pour <i>k</i>=0,5 c'est une <b>\u00BD-puissance</b> ou une ogive <b>parabolique</b>, pour <i>k</i>=0,75 une <b>\u00BE-puissance</b>, et pour <i>k</i>=1 un cône <b>conique</b>.\r
+Shape.Powerseries.desc2 = Une transition de la série haute puissance a un profile de <i>Rayon</i> × (<i>x</i> / <i>Longueur</i>)<sup><i>k</i></sup> ou <i>k</i> est le paramètre de la forme. Pour <i>k</i>=0,5 la transition est <b>\u00BD-puissance</b> ou <b>parabolique</b>, pour <i>k</i>=0,75 une <b>\u00BE-puissance</b>, et pour <i>k</i>=1 <b>conique</b>.\r
+Shape.Parabolicseries = Série parabolique\r
+Shape.Parabolicseries.desc1 = Un cône parabolique a un profil d'une parabole. Le paramètre de forme définit le segment de la parabole à utiliser. Le paramètre 1 produit une <b>parabole pleine</b> qui est tangent au tube de la fusée, 0,75 produit un <b>3/4 de parabole</b>, 0,5 produit une <b>1/2 parabole</b> et 0 produit un cône <b>conique</b>.\r
+Shape.Parabolicseries.desc2 = Une transition de type parabolique a un profile en forme de parabole. Le paramètre de forme définit le segment de la parabole à utiliser. Le paramètre 1,0 produit une <b>parabole pleine</b> qui est tangent au tube de la fusée à l'extrémité arrière, 0,75 produit une <b>3/4 parabole</b>, 0,5 produit une <b>1/2 parabole</b> et 0 produit une transition <b>conique</b>.\r
+Shape.Haackseries = Série Haack\r
+Shape.Haackseries.desc1 = Les cônes du type Haack sont conçus pour minimiser la trainée. Le paramètre de forme égale à 0 produit une <b>LD-Haack</b> ou un cône <b>Von Karman</b>, ce qui a pour effet de minimiser la trainée pour une longueur et un diamètre fixe, tandis qu'une valeur de 0,333 produit un cône <b>LV-Haack</b>, ce qui minimise la trainée pour une longueur et un volume fixe.\r
+Shape.Haackseries.desc2 = Les <i>cônes</i> du type Haack sont conçus pour minimiser la trainée. Ces formes de transition sont leurs équivalents, mais ne produisent pas nécessairement des valeurs optimales. Le paramètre 0 produit une forme <b>LD-Haack</b> ou <b>Von Karman</b>, tandis qu'une valeur de 0,333 produit une forme <b>LV-Haack</b>. \r
+\r
+\r
+! RocketComponent\r
+RocketComponent.Position.TOP = Haut de la pièce parent\r
+RocketComponent.Position.MIDDLE = Milieu de la pièce parent(porteuse)\r
+RocketComponent.Position.BOTTOM = Bas de la pièce parent\r
+RocketComponent.Position.AFTER = Après la pièce parent\r
+RocketComponent.Position.ABSOLUTE = Pointe de l'ogive\r
+\r
+! LaunchLug\r
+LaunchLug.Launchlug = Tube de guidage\r
+! NoseCone\r
+NoseCone.NoseCone = Ogive\r
+! Transition\r
+Transition.Transition = Transition\r
+!Stage\r
+Stage.Stage = Etage\r
+! BodyTube\r
+BodyTube.BodyTube = Tube du corps\r
+! TubeCoupler\r
+TubeCoupler.TubeCoupler = Coupleur de tube\r
+!InnerTube\r
+InnerTube.InnerTube = Tube interne\r
+! TrapezoidFinSet\r
+TrapezoidFinSet.TrapezoidFinSet = Ailerons Trapézoïdaux\r
+! FreeformFinSet\r
+FreeformFinSet.FreeformFinSet = Ailerons personnalisés\r
+!MassComponent\r
+MassComponent.MassComponent = Poids\r
+! Parachute\r
+Parachute.Parachute = Parachute\r
+! ShockCord\r
+ShockCord.ShockCord = Cordon amortisseur\r
+! Bulkhead\r
+Bulkhead.Bulkhead = Cloison\r
+\r
+!Rocket\r
+Rocket.motorCount.Nomotor = [aucun moteurs]\r
+Rocket.compname.Rocket = Fusée\r
+\r
+!MotorMount\r
+MotorMount.IgnitionEvent.AUTOMATIC = Automatique (lancement ou charge d'éjection)\r
+MotorMount.IgnitionEvent.LAUNCH = Lancement\r
+MotorMount.IgnitionEvent.EJECTION_CHARGE = Première charge d'éjection ou étage précédent\r
+MotorMount.IgnitionEvent.BURNOUT = Première combustion totale de l'étage précédent\r
+MotorMount.IgnitionEvent.NEVER = Jamais\r
+\r
+!ComponentIcons \r
+ComponentIcons.Nosecone = Ogive\r
+ComponentIcons.Bodytube = Tube\r
+ComponentIcons.Transition = Transition\r
+ComponentIcons.Trapezoidalfinset = Jeu d'ailerons de forme trapézoïdale\r
+ComponentIcons.Ellipticalfinset = Jeu d'ailerons de forme elliptique \r
+ComponentIcons.Freeformfinset = Jeu d'ailerons de forme personnalisé\r
+ComponentIcons.Launchlug = Tube de guidage\r
+ComponentIcons.Innertube = Tube interne\r
+ComponentIcons.Tubecoupler = Coupleur de tube\r
+ComponentIcons.Centeringring = Anneau de centrage\r
+ComponentIcons.Bulkhead = Cloison\r
+ComponentIcons.Engineblock = Bague de retension moteur\r
+ComponentIcons.Parachute = Parachute\r
+ComponentIcons.Streamer = Banderolle\r
+ComponentIcons.Shockcord = Cordon amortisseur\r
+ComponentIcons.Masscomponent = Piéce Masse\r
+ComponentIcons.disabled = (désactivé)\r
+\r
+! StageAction\r
+StageAction.Stage = Etage\r
+\r
+! RecoveryDevice\r
+RecoveryDevice.DeployEvent.LAUNCH = Lancement(plus NN secondes)\r
+RecoveryDevice.DeployEvent.EJECTION = Première charge d'éjection de cet étage\r
+RecoveryDevice.DeployEvent.APOGEE = Apogée\r
+RecoveryDevice.DeployEvent.ALTITUDE = Altitude spécifiée durant la descente\r
+RecoveryDevice.DeployEvent.NEVER = Jamais\r
+\r
+! FlightEvent\r
+FlightEvent.Type.LAUNCH = Lancement\r
+FlightEvent.Type.IGNITION = Allumage du moteur\r
+FlightEvent.Type.LIFTOFF = Décollage\r
+FlightEvent.Type.LAUNCHROD = Dégagement de rampe de lancement\r
+FlightEvent.Type.BURNOUT = Fin de combustion du moteur\r
+FlightEvent.Type.EJECTION_CHARGE = Charge d'éjection\r
+FlightEvent.Type.STAGE_SEPARATION = Séparation d'étage\r
+FlightEvent.Type.APOGEE = Apogée\r
+FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Déploiement du dispositif de récupération\r
+FlightEvent.Type.GROUND_HIT = Atterrissage\r
+FlightEvent.Type.SIMULATION_END = Fin de la simulation\r
+FlightEvent.Type.ALTITUDE = Changement d'altitude\r
+\r
+! ThrustCurveMotorColumns\r
+TCurveMotorCol.MANUFACTURER = Fabricant\r
+TCurveMotorCol.DESIGNATION = Désignation\r
+TCurveMotorCol.TYPE = Type\r
+TCurveMotorCol.DIAMETER = Diamètre\r
+TCurveMotorCol.LENGTH = Longueur\r
+\r
+! RocketInfo\r
+RocketInfo.lengthLine.Length = Longueur\r
+RocketInfo.lengthLine.maxdiameter = , diamètre max.\r
+RocketInfo.massText1 = Masse avec moteurs \r
+RocketInfo.massText2 = Masse sans moteurs\r
+RocketInfo.at = à M=\r
+RocketInfo.cgText = CG:\r
+RocketInfo.cpText = CP:\r
+RocketInfo.stabText = Stabilité:\r
+RocketInfo.Warning = Avertissement:\r
+RocketInfo.Calculating = Calcul en cours...\r
+RocketInfo.Apogee = Apogée:\r
+RocketInfo.Maxvelocity = Vitesse Max.:\r
+RocketInfo.Maxacceleration = Accélération Max.:\r
+RocketInfo.apogeeValue = N/A\r
+RocketInfo.Mach = (Mach\r
+RocketInfo.velocityValue = N/A\r
+RocketInfo.accelerationValue = N/A\r
+\r
+! FinSet\r
+FinSet.CrossSection.SQUARE = Carré\r
+FinSet.CrossSection.ROUNDED = Arondie\r
+FinSet.CrossSection.AIRFOIL = Airfoil\r
+FinSet.TabRelativePosition.FRONT = Emplanture avant\r
+FinSet.TabRelativePosition.CENTER = Emplanture centrale\r
+FinSet.TabRelativePosition.END = Emplanture arrière\r
+\r
+! FlightDataType\r
+FlightDataType.TYPE_TIME = Temps\r
+FlightDataType.TYPE_ALTITUDE = Altitude\r
+FlightDataType.TYPE_VELOCITY_Z = Vitesse verticale\r
+FlightDataType.TYPE_ACCELERATION_Z = Accélération verticale\r
+FlightDataType.TYPE_VELOCITY_TOTAL = Vitesse totale\r
+FlightDataType.TYPE_ACCELERATION_TOTAL = Accélération totale\r
+FlightDataType.TYPE_POSITION_X = Position contre le vent\r
+FlightDataType.TYPE_POSITION_Y = Position parallèle au vent\r
+FlightDataType.TYPE_POSITION_XY = Distance latérale\r
+FlightDataType.TYPE_POSITION_DIRECTION = Direction latérale\r
+FlightDataType.TYPE_VELOCITY_XY = Vitesse latérale\r
+FlightDataType.TYPE_ACCELERATION_XY = Accélération latérale\r
+FlightDataType.TYPE_AOA = Angle d'attaque\r
+FlightDataType.TYPE_ROLL_RATE = Taux de roulis\r
+FlightDataType.TYPE_PITCH_RATE = Taux de tangage\r
+FlightDataType.TYPE_YAW_RATE = Taux d'embardée\r
+FlightDataType.TYPE_MASS = Masse\r
+FlightDataType.TYPE_LONGITUDINAL_INERTIA = Moment d'inertie longitudinale\r
+FlightDataType.TYPE_ROTATIONAL_INERTIA = Moment d'inertie rotatif\r
+FlightDataType.TYPE_CP_LOCATION = Emplacement du CP\r
+FlightDataType.TYPE_CG_LOCATION = Emplacement du CG\r
+FlightDataType.TYPE_STABILITY = Calibres marge de stabilité\r
+FlightDataType.TYPE_MACH_NUMBER = Mach number\r
+FlightDataType.TYPE_REYNOLDS_NUMBER = Nombre de Reynolds\r
+FlightDataType.TYPE_THRUST_FORCE = Poussée\r
+FlightDataType.TYPE_DRAG_FORCE = Force de traînée\r
+FlightDataType.TYPE_DRAG_COEFF = Coefficient de traînée\r
+FlightDataType.TYPE_AXIAL_DRAG_COEFF = Coefficient de trainée axiale\r
+FlightDataType.TYPE_FRICTION_DRAG_COEFF = Coefficient de traînée de friction\r
+FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Coefficient de traînée de pression\r
+FlightDataType.TYPE_BASE_DRAG_COEFF = Coefficient de traînée de base\r
+FlightDataType.TYPE_NORMAL_FORCE_COEFF = Coefficient de force normale\r
+FlightDataType.TYPE_PITCH_MOMENT_COEFF = Coefficient de moment de tangage\r
+FlightDataType.TYPE_YAW_MOMENT_COEFF = Coefficient de moment d'embardée \r
+FlightDataType.TYPE_SIDE_FORCE_COEFF = Coefficient de force latérale \r
+FlightDataType.TYPE_ROLL_MOMENT_COEFF = Coefficient de moment de roulis \r
+FlightDataType.TYPE_ROLL_FORCING_COEFF = Coefficient de forçage de roulis\r
+FlightDataType.TYPE_ROLL_DAMPING_COEFF = Coefficient d'amortissement de roulis\r
+FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Coefficient d'amortissement de tangage\r
+FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Coefficient d'amortissement d'embardée\r
+FlightDataType.TYPE_REFERENCE_LENGTH = Longueur de référence\r
+FlightDataType.TYPE_REFERENCE_AREA = Surface de référence\r
+FlightDataType.TYPE_ORIENTATION_THETA = Orientation verticale (zénith)\r
+FlightDataType.TYPE_ORIENTATION_PHI = Orientation latérale (azimut)\r
+FlightDataType.TYPE_WIND_VELOCITY = Vitesse de vent\r
+FlightDataType.TYPE_AIR_TEMPERATURE = Température de l'air\r
+FlightDataType.TYPE_AIR_PRESSURE = Pression atmosphérique\r
+FlightDataType.TYPE_SPEED_OF_SOUND = Vitesse du son\r
+FlightDataType.TYPE_TIME_STEP = Pas de simulation du temps\r
+FlightDataType.TYPE_COMPUTATION_TIME = Temps de calcul\r
+FlightDataType.TYPE_LATITUDE = Latitude\r
+FlightDataType.TYPE_LONGITUDE = Longitude\r
+FlightDataType.TYPE_CORIOLIS_ACCELERATION = Accélération de Coriolis\r
+\r
+! PlotConfiguration\r
+PlotConfiguration.Verticalmotion = Mouvement vertical par rapport au temps\r
+PlotConfiguration.Totalmotion = Mouvement total par rapport au temps\r
+PlotConfiguration.Flightside = Profil latéral du vol\r
+PlotConfiguration.Stability = Stabilité par rapport au temps\r
+PlotConfiguration.Dragcoef = Coefficients de traînée par rapport au Mach number\r
+PlotConfiguration.Rollcharacteristics = Caractéristiques de roulis\r
+PlotConfiguration.Angleofattack = Angle d'attaque et orientation par rapport au temps\r
+PlotConfiguration.Simulationtime = Pas du temps et temps de calcul\r
+\r
+! Warning\r
+Warning.LargeAOA.str1 = Grand angle d'attaque rencontré.\r
+Warning.LargeAOA.str2 = Grand angle d'attaque rencontré (\r
+Warning.DISCONTINUITY = Discontinuité dans le diamètre du corps de la fusée.\r
+Warning.THICK_FIN = Les ailerons fin ne seront peut être pas modélisés correctement.\r
+Warning.JAGGED_EDGED_FIN = Des ailerons aux bords irréguliers ne seront pas modélisés correctement.\r
+Warning.LISTENERS_AFFECTED = Listeners modified the flight simulation\r
+Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Le dispositif de récupération s'est ouvert alors que la combustion du moteur n'était pas finie.\r
+Warning.FILE_INVALID_PARAMETER = Paramètre invalide rencontré, ignorer.\r
+\r
+\r
+! Scale dialog\r
+ScaleDialog.lbl.scaleRocket = Fusée entière\r
+ScaleDialog.lbl.scaleSubselection = La sélection et tous ses composants \r
+ScaleDialog.lbl.scaleSelection = Seulement les composants sélectionnés\r
+ScaleDialog.title = Redimensionner le projet\r
+ScaleDialog.lbl.scale = Mise à l'échelle:\r
+ScaleDialog.lbl.scale.ttip = Choisir de redimensionner tout le projet ou seulement la pièce choisie\r
+ScaleDialog.lbl.scaling = Echelle à appliquer:\r
+ScaleDialog.lbl.scaling.ttip = Taille résultante,les valeurs au-dessus de 100% agrandissent et les valeurs en-dessous de 100% réduisent le design.\r
+! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"\r
+ScaleDialog.lbl.scaleFrom = Mise à l'échelle de \r
+ScaleDialog.lbl.scaleTo = à\r
+ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and resulting length.\r
+ScaleDialog.checkbox.scaleMass = Update explicit mass values\r
+ScaleDialog.checkbox.scaleMass.ttip = Scale mass component and override mass values by the cube of the scaling factor\r
+ScaleDialog.button.scale = Redimensionner\r
+ScaleDialog.undo.scaleRocket = Redimensionner la fusée\r
+ScaleDialog.undo.scaleComponent = Redimensionner une pièce\r
+ScaleDialog.undo.scaleComponents = Redimensionner les pièces\r
+\r
+!icons\r
+Icons.Undo = Undo\r
+Icons.Redo = Redo\r
+\r
+OpenRocketPrintable.Partsdetail = Détail des pièces\r
+OpenRocketPrintable.Fintemplates = Gabaries des ailerons\r
+OpenRocketPrintable.DesignReport = Rapport de conception\r
+\r
+OpenRocketDocument.Redo = Refaire\r
+OpenRocketDocument.Undo = Défaire\r
+\r
+!EllipticalFinSet\r
+EllipticalFinSet.Ellipticalfinset = Ailerons elliptique\r
+\r
+! Optimization\r
+\r
+! Modifiers\r
+\r
+optimization.modifier.nosecone.length = Longueur du cône\r
+optimization.modifier.nosecone.length.desc = Optimise la longueur du cône.\r
+optimization.modifier.nosecone.diameter = Diamètre du cône\r
+optimization.modifier.nosecone.diameter.desc = Optimise le diamètre du cône.\r
+optimization.modifier.nosecone.thickness = Epaisseur du cône\r
+optimization.modifier.nosecone.thickness.desc = Optimise l'épaisseur des parois du cône.\r
+optimization.modifier.nosecone.shapeparameter = Paramètre de la forme\r
+optimization.modifier.nosecone.shapeparameter.desc = Optimise les paramètres de forme du cône.\r
+ \r
+optimization.modifier.transition.length = Longueur de la Transition\r
+optimization.modifier.transition.length.desc = Optimise la longueur de la transition.\r
+optimization.modifier.transition.forediameter = Diamètre avant de la Transition\r
+optimization.modifier.transition.forediameter.desc = Optimise le diamètre avant de la transition.\r
+optimization.modifier.transition.aftdiameter = Diamètre arrière de la transition\r
+optimization.modifier.transition.aftdiameter.desc = Optimise le diamètre arrière de la transition.\r
+optimization.modifier.transition.thickness = Epaisseur de la transition\r
+optimization.modifier.transition.thickness.desc = Optimise l'épaisseur des parois de la transition.\r
+optimization.modifier.transition.shapeparameter = Paramètre de la forme\r
+optimization.modifier.transition.shapeparameter.desc = Optimise le paramètre de la forme.\r
+\r
+optimization.modifier.bodytube.length = Longueur du tube du corps\r
+optimization.modifier.bodytube.length.desc = Optimise la longueur du tube du corps.\r
+optimization.modifier.bodytube.outerDiameter = Diamètre externe du tube du corps\r
+optimization.modifier.bodytube.outerDiameter.desc = Optimise le diamètre externe du tube du corps tout en maintenant l'épaisseur des parois.\r
+optimization.modifier.bodytube.innerDiameter = Diamètre interne du tube du corps\r
+optimization.modifier.bodytube.thickness = Epaisseur du tube du corps\r
+optimization.modifier.bodytube.thickness.desc = Optimise l'épaisseur des parois du tube du corps.\r
+\r
+optimization.modifier.trapezoidfinset.rootChord = Root chord\r
+optimization.modifier.trapezoidfinset.rootChord.desc = Optimize the root chord length of the fin set (length of fin at the rocket body).\r
+optimization.modifier.trapezoidfinset.tipChord = Tip chord\r
+optimization.modifier.trapezoidfinset.tipChord.desc = Optimize the tip chord length of the fin set (length of fin at outer edge).\r
+optimization.modifier.trapezoidfinset.sweep = Sweep\r
+optimization.modifier.trapezoidfinset.sweep.desc = Optimize the sweep of the fin set (distance that the leading edge sweeps backwards).\r
+optimization.modifier.trapezoidfinset.height = Hauteur\r
+optimization.modifier.trapezoidfinset.height.desc = Optimize the height (semi-span) of the fin set.\r
+\r
+optimization.modifier.ellipticalfinset.length = Root chord\r
+optimization.modifier.ellipticalfinset.length.desc = Optimize the root chord length of the fin set.\r
+optimization.modifier.ellipticalfinset.height = Hauteur\r
+optimization.modifier.ellipticalfinset.height.desc = Optimize the height (semi-span) of the fin set.\r
+\r
+optimization.modifier.finset.cant = Cant angle\r
+optimization.modifier.finset.cant.desc = Optimize the cant angle of the fin set.\r
+optimization.modifier.finset.position = Position\r
+optimization.modifier.finset.position.desc = Optimisation de la position du jeux d'ailerons sur le corps de la fusée.\r
+\r
+optimization.modifier.launchlug.length = Longueur\r
+optimization.modifier.launchlug.length.desc = Optimisation de la longueur du tube de guidage.\r
+optimization.modifier.launchlug.outerDiameter = Diamètre externe\r
+optimization.modifier.launchlug.outerDiameter.desc = Optimisation du diamètre externe du tube de guidage.\r
+optimization.modifier.launchlug.thickness = Epaisseur\r
+optimization.modifier.launchlug.thickness.desc = Optimise l'épaisseur de la bague de guide tout en gardant le diamètre extérieur constant.\r
+optimization.modifier.launchlug.position = Position\r
+optimization.modifier.launchlug.position.desc = Optimise la position de la bague de guidage le long du corps de la fusée.\r
+\r
+\r
+optimization.modifier.internalcomponent.position = Position\r
+optimization.modifier.internalcomponent.position.desc = Optimise la position de la pièce par rapport à la pièce parent.\r
+\r
+optimization.modifier.masscomponent.mass = Masse\r
+optimization.modifier.masscomponent.mass.desc = Optimise la masse du composant.\r
+\r
+optimization.modifier.parachute.diameter = Diamètre\r
+optimization.modifier.parachute.diameter.desc = Optimise le diamètre de la coupole du parachute.\r
+optimization.modifier.parachute.coefficient = Coefficient de trainée\r
+optimization.modifier.parachute.coefficient.desc = Optimisation du coefficient de trainée du parachute. Un parachute type à un coefficient de trainée d'environ 0.8.\r
+\r
+optimization.modifier.streamer.length = Longueur\r
+optimization.modifier.streamer.length.desc = Optimisation de la longueur de la banderole (streamer).\r
+optimization.modifier.streamer.width = Largeur\r
+optimization.modifier.streamer.width.desc = Optimisation de la largeur de la banderole (streamer).\r
+optimization.modifier.streamer.aspectRatio = Aspect ratio\r
+optimization.modifier.streamer.aspectRatio.desc = Optimize the aspect ratio of the streamer (length/width). You should NOT select streamer length or width at the same time with the aspect ratio.\r
+optimization.modifier.streamer.coefficient = Coefficient de trainée\r
+optimization.modifier.streamer.coefficient.desc = Optimisation du coéfficient de trainée de la banderole (streamer).\r
+\r
+optimization.modifier.recoverydevice.deployDelay = Retard du déploiement\r
+optimization.modifier.recoverydevice.deployDelay.desc = Optimise le délai du déploiement du système du récupération.\r
+optimization.modifier.recoverydevice.deployAltitude = Altitude du déploiement\r
+optimization.modifier.recoverydevice.deployAltitude.desc = Optimise l'altitude de déploiement du dispositif de récupération.\r
+\r
+optimization.modifier.rocketcomponent.overrideMass = Forcer la masse\r
+optimization.modifier.rocketcomponent.overrideMass.desc = Optimise le forçage de la masse du composant.\r
+optimization.modifier.rocketcomponent.overrideCG = forcer le CG\r
+optimization.modifier.rocketcomponent.overrideCG.desc = Optimise le forçage du centre de gravité du composant.\r
+\r
+optimization.modifier.motormount.overhang = Surplomb du moteur\r
+optimization.modifier.motormount.overhang.desc = Optimise le surplomb du moteur.\r
+optimization.modifier.motormount.delay = Retard de l'allumage moteur\r
+optimization.modifier.motormount.delay.desc = Optimisation du retard d'allumage du moteur.\r
+\r
+\r
+\r
+\r
+! General rocket design optimization dialog\r
+\r
+GeneralOptimizationDialog.title = Optimisation de la fusée\r
+GeneralOptimizationDialog.goal.maximize = Maximiser la valeur\r
+GeneralOptimizationDialog.goal.minimize = Minimiser la valeur\r
+GeneralOptimizationDialog.goal.seek = Cherchez la valeur de\r
+GeneralOptimizationDialog.btn.start = Démarrer l'optimisation\r
+GeneralOptimizationDialog.btn.stop = Terminer l'optimisation\r
+GeneralOptimizationDialog.lbl.paramsToOptimize = Paramètres à optimiser:\r
+GeneralOptimizationDialog.btn.add = Ajouter\r
+GeneralOptimizationDialog.btn.add.ttip = Ajouter le paramètre sélectionné aux paramètres à optimiser\r
+GeneralOptimizationDialog.btn.remove = Enlever\r
+GeneralOptimizationDialog.btn.remove.ttip = Enlever le paramètre sélectionné des paramètres à optimiser\r
+GeneralOptimizationDialog.btn.removeAll = Tout enlever\r
+GeneralOptimizationDialog.btn.removeAll.ttip = Enlever tous les paramètres de l'optimisation\r
+GeneralOptimizationDialog.lbl.availableParams = Paramètres disponible:\r
+GeneralOptimizationDialog.lbl.optimizationOpts = Options pour l'optimisation\r
+GeneralOptimizationDialog.lbl.optimizeSim = Optimiser la simulation:\r
+GeneralOptimizationDialog.lbl.optimizeSim.ttip = Choisir la simulation à optimiser\r
+GeneralOptimizationDialog.lbl.optimizeValue = Valeur optimum\r
+GeneralOptimizationDialog.lbl.optimizeValue.ttip = Choisir quelle valeur à optimiser\r
+GeneralOptimizationDialog.lbl.optimizeGoal = But de l'optimisation:\r
+GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Choisir le but de l'optimisation\r
+GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Valeur personnalisée à rechercher\r
+GeneralOptimizationDialog.lbl.requireStability = Stabilité désirée\r
+GeneralOptimizationDialog.lbl.requireMinStability = Stabilité minimum:\r
+GeneralOptimizationDialog.lbl.requireMinStability.ttip = Exiger une marge de stabilité statique minimale pour le design\r
+GeneralOptimizationDialog.lbl.requireMaxStability = Stabilité maximum:\r
+GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Exiger une marge de stabilité statique maximale pour le design\r
+GeneralOptimizationDialog.status.bestValue = Meilleure valeur:\r
+GeneralOptimizationDialog.status.bestValue.ttip = Meilleure valeur optimum trouvé jusqu'à présent.\r
+GeneralOptimizationDialog.status.stepCount = Step count:\r
+GeneralOptimizationDialog.status.stepCount.ttip = Number of optimization steps that have been performed.\r
+GeneralOptimizationDialog.status.evalCount = Evaluations:\r
+GeneralOptimizationDialog.status.evalCount.ttip = Total number of function evaluations (simulations) that have been performed.\r
+GeneralOptimizationDialog.status.stepSize = Step size:\r
+GeneralOptimizationDialog.status.stepSize.ttip = Current optimization step size (relative to the optimization parameter ranges)\r
+GeneralOptimizationDialog.btn.plotPath = Plot path\r
+GeneralOptimizationDialog.btn.plotPath.ttip = Plot the optimization path (one and two dimensional optimization only)\r
+GeneralOptimizationDialog.btn.save = Save path\r
+GeneralOptimizationDialog.btn.save.ttip = Save the results of the function evaluations (simulations) as a CSV file.\r
+GeneralOptimizationDialog.btn.apply = Appliquer l'optimisation\r
+GeneralOptimizationDialog.btn.apply.ttip = Appliquer les résultats de l'optimisation au design de la fusée\r
+GeneralOptimizationDialog.btn.reset = Re-Réinitialiser\r
+GeneralOptimizationDialog.btn.reset.ttip = Réinitialiser le design de la fusée au design actuel de la fusée\r
+GeneralOptimizationDialog.btn.close = Fermer\r
+GeneralOptimizationDialog.btn.close.ttip = Fermer la fenêtre de dialogue sans modifier la fusée\r
+GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters.\r
+GeneralOptimizationDialog.error.selectParams.title = Choisir les paramètres de l'optimisation\r
+GeneralOptimizationDialog.error.optimizationFailure.text = L'optimisation n'a pas fonctionnée:\r
+GeneralOptimizationDialog.error.optimizationFailure.title = L'optimisation n'a pas réussie\r
+GeneralOptimizationDialog.undoText = Appliquer l'optimisation\r
+GeneralOptimizationDialog.basicSimulationName = Simulation simple\r
+GeneralOptimizationDialog.noSimulationName = Pas de simulation\r
+GeneralOptimizationDialog.table.col.parameter = Paramètre\r
+GeneralOptimizationDialog.table.col.current = Courant\r
+GeneralOptimizationDialog.table.col.min = Minimum\r
+GeneralOptimizationDialog.table.col.max = Maximum\r
+GeneralOptimizationDialog.export.header = Inclure la ligne d'en tête\r
+GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions.\r
+GeneralOptimizationDialog.export.stability = Stabilité\r
+\r
+\r
+! Dialog for plotting optimization results\r
+OptimizationPlotDialog.title = Résultats de l'optimisation\r
+OptimizationPlotDialog.lbl.zoomInstructions = Click et glisser en bas et à droite pour zoomer plus, en haut et à gauche pour zoomer moins\r
+OptimizationPlotDialog.plot1d.title = Résultat de l'optimisation\r
+OptimizationPlotDialog.plot1d.series = Résultat de l'optimisation\r
+OptimizationPlotDialog.plot2d.title = Optimization path\r
+OptimizationPlotDialog.plot2d.path = Chemin pour l'optimisation\r
+OptimizationPlotDialog.plot2d.evals = Evaluations\r
+OptimizationPlotDialog.plot.ttip.stability = Stabilité:\r
+OptimizationPlotDialog.plot.label.optimum = Optimum\r
+\r
+! Optimization parameters\r
+MaximumAltitudeParameter.name = Altitude de l'apogée\r
+MaximumVelocityParameter.name = Vitesse maximum\r
+MaximumAccelerationParameter.name = Accélération maximum\r
+StabilityParameter.name = Stabilité\r
+GroundHitVelocityParameter.name = Vitesse à l'atterrissage\r
+LandingDistanceParameter.name = Distance à l'atterrissage\r
+TotalFlightTimeParameter.name = Durée totale du vol\r
+DeploymentVelocityParameter.name = Vitesse lors de l'ouverture du parachute\r
+\r
+\r
+! Compass directions drawn on a compass rose.\r
+CompassRose.lbl.north = N\r
+CompassRose.lbl.east = E\r
+CompassRose.lbl.south = S\r
+CompassRose.lbl.west = O\r
+\r
+! Compass directions with subdirections. These might not be localized even if the directions on the compass rose are.\r
+CompassSelectionButton.lbl.N = N\r
+CompassSelectionButton.lbl.NE = NE\r
+CompassSelectionButton.lbl.E = E\r
+CompassSelectionButton.lbl.SE = SE\r
+CompassSelectionButton.lbl.S = S\r
+CompassSelectionButton.lbl.SW = SO\r
+CompassSelectionButton.lbl.W = O\r
+CompassSelectionButton.lbl.NW = NO\r
+\r
+\r
+SlideShowDialog.btn.next = Suivant\r
+SlideShowDialog.btn.prev = Précédent\r
+\r
+GuidedTourSelectionDialog.title = Tours d'horizon\r
+GuidedTourSelectionDialog.lbl.selectTour = Choisir un tour d'horizon:\r
+GuidedTourSelectionDialog.lbl.description = Description du tour d'horizon:\r
+GuidedTourSelectionDialog.lbl.length = Nombre de diapositives:\r
+GuidedTourSelectionDialog.btn.start = Commencer le tour d'horizon!\r
+++ /dev/null
-
-#
-# English base translation file
-#
-# Should you need to add new logical keys here is the proposed method
-#
-# className.ComponentType.componentName
-#
-#
-# Text tokens within braces should not be translated, e.g.
-# "The file '{filename}' exists."
-# They are pieces that are inserted dynamically.
-#
-
-
-! Set to the name of the current translation file (used for debugging purposes)
-debug.currentFile = messages.properties
-
-! RocketActions
-RocketActions.checkbox.Donotaskmeagain = Do not ask me again
-RocketActions.lbl.Youcanchangedefop = You can change the default operation in the preferences.
-RocketActions.showConfirmDialog.lbl1 = Delete the selected simulations?
-RocketActions.showConfirmDialog.lbl2 = <html><i>This operation cannot be undone.</i>
-RocketActions.showConfirmDialog.title = Delete simulations
-RocketActions.DelCompAct.Delete = Delete
-RocketActions.DelCompAct.ttip.Delete = Delete the selected component.
-RocketActions.DelSimuAct.Delete = Delete
-RocketActions.DelSimuAct.ttip.Delete = Delete the selected simulation.
-RocketActions.DelAct.Delete = Delete
-RocketActions.DelAct.ttip.Delete = Delete the selected component or simulation.
-RocketActions.CutAction.Cut = Cut
-RocketActions.CutAction.ttip.Cut = Cut this component or simulation to the clipboard and remove from this design
-RocketActions.CopyAct.Copy = Copy
-RocketActions.CopyAct.ttip.Copy = Copy this component (and subcomponents) to the clipboard.
-RocketActions.PasteAct.Paste = Paste
-RocketActions.PasteAct.ttip.Paste = Paste the component or simulation on the clipboard to the design.
-RocketActions.EditAct.Edit = Edit
-RocketActions.EditAct.ttip.Edit = Edit the selected component.
-RocketActions.NewStageAct.Newstage = New stage
-RocketActions.NewStageAct.ttip.Newstage = Add a new stage to the rocket design.
-RocketActions.ActBoosterstage = Booster stage
-RocketActions.MoveUpAct.Moveup = Move up
-RocketActions.MoveUpAct.ttip.Moveup = Move this component upwards.
-RocketActions.MoveDownAct.Movedown = Move down
-RocketActions.MoveDownAct.ttip.Movedown = Move this component downwards.
-
-! RocketPanel
-RocketPanel.FigTypeAct.Sideview = Side view
-RocketPanel.FigTypeAct.ttip.Sideview = Side view
-RocketPanel.FigTypeAct.Backview = Back view
-RocketPanel.FigTypeAct.ttip.Backview = Rear view
-RocketPanel.lbl.Motorcfg = Motor configuration:
-RocketPanel.lbl.infoMessage = <html>Click to select Shift+click to select other Double-click to edit Click+drag to move
-
-
-! BasicFrame
-BasicFrame.SimpleFileFilter1 = All rocket designs (*.ork; *.rkt)
-BasicFrame.SimpleFileFilter2 = OpenRocket designs (*.ork)
-BasicFrame.SimpleFileFilter3 = RockSim designs (*.rkt)
-BasicFrame.tab.Rocketdesign = Rocket design
-BasicFrame.tab.Flightsim = Flight simulations
-BasicFrame.title.Addnewcomp = Add new component
-BasicFrame.dlg.lbl1 = Design '
-BasicFrame.dlg.lbl2 = ' has not been saved.
-BasicFrame.dlg.lbl3 = Do you want to save it?
-BasicFrame.dlg.title = Design not saved
-BasicFrame.StageName.Sustainer = Sustainer
-BasicFrame.WarningDialog.txt1 = The following problems were encountered while opening
-BasicFrame.WarningDialog.txt2 = Some design features may not have been loaded correctly.
-BasicFrame.WarningDialog.title = Warnings while opening file
-
-
-! General error messages used in multiple contexts
-error.fileExists.title = File exists
-error.fileExists.desc = File '{filename}' exists. Do you want to overwrite it?
-
-error.writing.title = Error writing file
-error.writing.desc = An error occurred while writing to the file:
-
-
-! Labels used in buttons of dialog windows
-# TODO: Rename these to "btn.xxx"
-button.ok = OK
-button.cancel = Cancel
-button.close = Close
-
-! Common labels used in buttons of dialog windows
-dlg.but.ok = OK
-dlg.but.cancel = Cancel
-dlg.but.close = Close
-
-
-! General file type names
-filetypes.pdf = PDF files
-
-
-! About Dialog
-AboutDialog.lbl.version = Version
-! The texts below provide additional credits for the translation maintainer
-! - In AboutDialog.lbl.translation replace "English" with the current language.
-! - AboutDialog.lbl.translator is the translator / group name (may be empty)
-! - AboutDialog.lbl.translatorWebsite is a URL to the translator / group (may be empty)
-! - AboutDialog.lbl.translatorIcon is the file name of an icon under pix/translators/ (may be empty)
-AboutDialog.lbl.translation = English translation by:
-AboutDialog.lbl.translator =
-AboutDialog.lbl.translatorWebsite =
-AboutDialog.lbl.translatorIcon =
-
-
-! Print dialog
-PrintDialog.title = Print or export
-PrintDialog.but.previewAndPrint = Preview & Print
-PrintDialog.checkbox.showByStage = Show by stage
-PrintDialog.lbl.selectElements = Select elements to include:
-printdlg.but.saveaspdf = Save as PDF
-printdlg.but.preview = Preview
-printdlg.but.settings = Settings
-PrintDialog.error.preview.title = Unable to open preview
-PrintDialog.error.preview.desc1 = Unable to open PDF preview.
-PrintDialog.error.preview.desc2 = Please use the "Save as PDF" option instead.
-
-
-!PrintSettingsDialog
-PrintSettingsDialog.title = Print settings
-PrintSettingsDialog.lbl.Templatefillcolor = Template fill color:
-PrintSettingsDialog.lbl.Templatebordercolor = Template border color:
-PrintSettingsDialog.lbl.Papersize = Paper size:
-PrintSettingsDialog.lbl.Paperorientation = Paper orientation:
-PrintSettingsDialog.but.Reset = Reset
-PrintSettingsDialog.but.Close = Close
-
-
-! Bug Report dialog
-bugreport.dlg.title = Bug report
-bugreport.dlg.but.Sendbugreport = Send bug report
-bugreport.dlg.but.Sendbugreport.Ttip = Automatically send the bug report to the OpenRocket developers.
-bugreport.dlg.successmsg1 = Bug report successfully sent.
-bugreport.dlg.successmsg2 = Thank you for helping make OpenRocket better!
-bugreport.dlg.successmsg3 = Bug report sent
-bugreport.dlg.connectedInternet = <html>If connected to the Internet, you can simply click <em>Send bug report</em>.
-bugreport.dlg.otherwise = Otherwise, send the text below to the address:
-bugreport.lbl.Theinformation = The information above may be included in a public bug report. Make sure it does not contain any sensitive information you do not want to be made public.
-bugreport.dlg.failedmsg1 = OpenRocket was unable to send the bug report:
-bugreport.dlg.failedmsg2 = Please send the report manually to
-bugreport.dlg.failedmsg3 = Error sending report
-bugreport.reportDialog.txt = <html><b>You can report a bug in OpenRocket by filling in and submitting the form below.</b><br>You can also report bugs and include attachments on the project web site.
-bugreport.reportDialog.txt2 = <html><b>Please include a short description about what you were doing when the exception occurred.</b>
-bugreport.dlg.provideDescription = Please provide a description of the bug first.
-bugreport.dlg.provideDescription.title = Bug description missing
-
-
-! Debug log dialog
-debuglogdlg.but.clear = Clear
-debuglogdlg.OpenRocketdebuglog = OpenRocket debug log
-debuglogdlg.Displayloglines = Display log lines:
-debuglogdlg.Follow = Follow
-debuglogdlg.col.Time = Time
-debuglogdlg.col.Level = Level
-debuglogdlg.col.Location = Location
-debuglogdlg.col.Message = Message
-debuglogdlg.lbl.Loglinenbr = Log line number:
-debuglogdlg.lbl.Time = Time:
-debuglogdlg.lbl.Level = Level:
-debuglogdlg.lbl.Location = Location:
-debuglogdlg.lbl.Logmessage = Log message:
-debuglogdlg.lbl.Stacktrace = Stack trace:
-
-
-! Edit Motor configuration dialog
-edtmotorconfdlg.but.removemotor = Remove motor
-edtmotorconfdlg.but.Selectmotor = Select motor
-edtmotorconfdlg.but.Removeconfiguration = Remove configuration
-edtmotorconfdlg.but.Newconfiguration = New configuration
-edtmotorconfdlg.lbl.Motormounts = <html><b>Motor mounts:</b>
-edtmotorconfdlg.title.Editmotorconf = Edit motor configurations
-edtmotorconfdlg.selectcomp = <html>Select which components function as motor mounts:
-edtmotorconfdlg.lbl.Motorconfig = <html><b>Motor configurations:</b>
-edtmotorconfdlg.lbl.Configname = Configuration name:
-edtmotorconfdlg.lbl.Leavenamedefault = Leave name empty for default.
-
-! Example design dialog
-exdesigndlg.but.open = Open
-exdesigndlg.lbl.Selectexample = Select example designs to open:
-exdesigndlg.lbl.Openexampledesign = Open example design
-exdesigndlg.lbl.Exampledesignsnotfound = Example designs could not be found.
-exdesigndlg.lbl.Examplesnotfound = Examples not found
-
-
-! Material edit panel
-matedtpan.but.new = New
-matedtpan.but.edit = Edit
-matedtpan.but.delete = Delete
-matedtpan.but.revertall = Revert all
-matedtpan.col.Material = Material
-matedtpan.col.Type = Type
-matedtpan.col.Density = Density
-matedtpan.col.but.ttip.New = Add a new material
-matedtpan.title.Addcustmaterial = Add a custom material
-matedtpan.but.ttip.edit = Edit an existing material
-matedtpan.title.Editmaterial = Edit material
-matedtpan.title2.Editmaterial = The built-in materials cannot be modified.
-matedtpan.but.ttip.delete = Delete a user-defined material
-matedtpan.but.ttip.revertall = Delete all user-defined materials
-matedtpan.title.Deletealluser-defined = Delete all user-defined materials?
-matedtpan.title.Revertall = Revert all?
-matedtpan.lbl.edtmaterials = Editing materials will not affect existing rocket designs.
-
-!MaterialModel
-MaterialModel.title.Material = Material
-MaterialModel.title.Defcustmat = Define custom material
-
-
-! Preference dialog
-pref.dlg.but.add = Add
-pref.dlg.but.reset = Reset
-pref.dlg.but.checknow = Check now
-pref.dlg.but.defaultmetric = Default metric
-pref.dlg.but.defaultimperial = Default imperial
-pref.dlg.title.Preferences = Preferences
-pref.dlg.tab.Units = Units
-pref.dlg.tab.Defaultunits = Default units
-pref.dlg.tab.Materials = Materials
-pref.dlg.tab.Custommaterials = Custom materials
-pref.dlg.tab.Options = Options
-pref.dlg.tab.Miscellaneousoptions = Miscellaneous options
-pref.dlg.lbl.Positiontoinsert = Position to insert new body components:
-pref.dlg.lbl.Confirmdeletion = Confirm deletion of simulations:
-pref.dlg.lbl.User-definedthrust = User-defined thrust curves:
-pref.dlg.Allthrustcurvefiles = All thrust curve files (*.eng; *.rse; *.zip; directories)
-pref.dlg.RASPfiles = RASP motor files (*.eng)
-pref.dlg.RockSimfiles = RockSim engine files (*.rse)
-pref.dlg.ZIParchives = ZIP archives (*.zip)
-pref.dlg.checkbox.Checkupdates = Check for software updates at startup
-pref.dlg.ttip.Checkupdatesnow = Check for software updates now
-pref.dlg.lbl.Selectprefunits = Select your preferred units:
-pref.dlg.lbl.Rocketdimensions = Rocket dimensions:
-pref.dlg.lbl.Linedensity = Line density:
-pref.dlg.lbl.Motordimensions = Motor dimensions:
-pref.dlg.lbl.Surfacedensity = Surface density:
-pref.dlg.lbl.Distance = Distance:
-pref.dlg.lbl.Bulkdensity = Bulk density:
-pref.dlg.lbl.Velocity = Velocity:
-pref.dlg.lbl.Surfaceroughness = Surface roughness:
-pref.dlg.lbl.Acceleration = Acceleration:
-pref.dlg.lbl.Area = Area:
-pref.dlg.lbl.Mass = Mass:
-pref.dlg.lbl.Angle = Angle:
-pref.dlg.lbl.Force = Force:
-pref.dlg.lbl.Rollrate = Roll rate:
-pref.dlg.lbl.Totalimpulse = Total impulse:
-pref.dlg.lbl.Temperature = Temperature:
-pref.dlg.lbl.Momentofinertia = Moment of inertia:
-pref.dlg.lbl.Pressure = Pressure:
-pref.dlg.lbl.Stability = Stability:
-pref.dlg.lbl.FlightTime = Flight time:
-pref.dlg.lbl.effect1 = The effects will take place the next time you open a window.
-pref.dlg.lbl.Checkingupdates = Checking for updates...
-pref.dlg.lbl.msg1 = An error occurred while communicating with the server.
-pref.dlg.lbl.msg2 = Unable to retrieve update information
-pref.dlg.lbl.msg3 = You are running the latest version of OpenRocket.
-pref.dlg.lbl.msg4 = No updates available
-pref.dlg.PrefChoiseSelector1 = Always ask
-pref.dlg.PrefChoiseSelector2 = Insert in middle
-pref.dlg.PrefChoiseSelector3 = Add to end
-pref.dlg.PrefBooleanSelector1 = Delete
-pref.dlg.PrefBooleanSelector2 = Confirm
-pref.dlg.Add = Add
-pref.dlg.DescriptionArea.Adddirectories = Add directories, RASP motor files (*.eng), RockSim engine files (*.rse) or ZIP archives separated by a semicolon (;) to load external thrust curves. Changes will take effect the next time you start OpenRocket.
-
-PreferencesDialog.lbl.language = Interface language:
-PreferencesDialog.languages.default = System default
-PreferencesDialog.lbl.languageEffect = The language will change the next time you start OpenRocket.
-
-! Simulation edit dialog
-simedtdlg.but.runsimulation = Run simulation
-simedtdlg.but.resettodefault = Reset to default
-simedtdlg.but.add = Add
-simedtdlg.but.remove = Remove
-simedtdlg.title.Editsim = Edit simulation
-simedtdlg.lbl.Simname = Simulation name:
-simedtdlg.tab.Launchcond = Launch conditions
-simedtdlg.tab.Simopt = Simulation options
-simedtdlg.tab.Plotdata = Plot data
-simedtdlg.tab.Exportdata = Export data
-simedtdlg.lbl.Motorcfg = Motor configuration:
-simedtdlg.lbl.ttip.Motorcfg = Select the motor configuration to use.
-simedtdlg.combo.ttip.motorconf = Select the motor configuration to use.
-simedtdlg.lbl.Wind = Wind
-simedtdlg.lbl.Averwindspeed = Average windspeed:
-simedtdlg.lbl.ttip.Averwindspeed = The average windspeed relative to the ground.
-simedtdlg.lbl.Stddeviation = Standard deviation:
-simedtdlg.lbl.ttip.Stddeviation = <html>The standard deviation of the windspeed.<br>The windspeed is within twice the standard deviation from the average for 95% of the time.
-simedtdlg.lbl.Turbulenceintensity = Turbulence intensity:
-simedtdlg.lbl.ttip.Turbulenceintensity1 = <html>The turbulence intensity is the standard deviation divided by the average windspeed.<br>
-simedtdlg.lbl.ttip.Turbulenceintensity2 = Typical values range from
-simedtdlg.lbl.ttip.Turbulenceintensity3 = to
-simedtdlg.border.Atmoscond = Atmospheric conditions
-simedtdlg.checkbox.InterStdAtmosphere = Use International Standard Atmosphere
-simedtdlg.checkbox.ttip.InterStdAtmosphere1 = <html>Select to use the International Standard Atmosphere model.<br>This model has a temperature of
-simedtdlg.checkbox.ttip.InterStdAtmosphere2 = and a pressure of
-simedtdlg.checkbox.ttip.InterStdAtmosphere3 = at sea level.
-simedtdlg.lbl.Temperature = Temperature:
-simedtdlg.lbl.ttip.Temperature = The temperature at the launch site.
-simedtdlg.lbl.Pressure = Pressure:
-simedtdlg.lbl.ttip.Pressure = The atmospheric pressure at the launch site.
-simedtdlg.lbl.Launchsite = Launch site
-simedtdlg.lbl.Latitude = Latitude:
-simedtdlg.lbl.ttip.Latitude = <html>The launch site latitude affects the gravitational pull of Earth.<br>Positive values are on the Northern hemisphere, negative values on the Southern hemisphere.
-
-simedtdlg.lbl.Longitude = Longitude:
-simedtdlg.lbl.ttip.Longitude = <html>Required for weather prediction and elevation models.
-
-simedtdlg.lbl.Altitude = Altitude:
-simedtdlg.lbl.ttip.Altitude = <html>The launch altitude above mean sea level.<br>This affects the position of the rocket in the atmospheric model.
-simedtdlg.border.Launchrod = Launch rod
-simedtdlg.lbl.Length = Length:
-simedtdlg.lbl.ttip.Length = The length of the launch rod.
-simedtdlg.lbl.Angle = Angle:
-simedtdlg.lbl.ttip.Angle = The angle of the launch rod from vertical.
-simedtdlg.lbl.Direction = Direction:
-simedtdlg.lbl.ttip.Direction1 = <html>Direction of the launch rod relative to the wind.<br>
-simedtdlg.lbl.ttip.Direction2 = = towards the wind,
-simedtdlg.lbl.ttip.Direction3 = = downwind.
-simedtdlg.border.Simopt = Simulator options
-simedtdlg.lbl.Calcmethod = Calculation method:
-simedtdlg.lbl.ttip.Calcmethod = <html>The Extended Barrowman method calculates aerodynamic forces according <br>to the Barrowman equations extended to accommodate more components.
-simedtdlg.lbl.ExtBarrowman = Extended Barrowman
-simedtdlg.lbl.Simmethod = Simulation method:
-simedtdlg.lbl.ttip.Simmethod1 = <html>The six degree-of-freedom simulator allows the rocket total freedom during flight.<br>
-simedtdlg.lbl.ttip.Simmethod2 = Integration is performed using a 4<sup>th</sup> order Runge-Kutta 4 numerical integration.
-simedtdlg.lbl.GeodeticMethod = Geodetic calculations:
-simedtdlg.lbl.ttip.GeodeticMethodTip = Relate to the calculation of coordinates on the earth. This also enables coriolis effect computations.
-simedtdlg.lbl.Timestep = Time step:
-simedtdlg.lbl.ttip.Timestep1 = <html>The time between simulation steps.<br>A smaller time step results in a more accurate but slower simulation.<br>
-simedtdlg.lbl.ttip.Timestep2 = The 4<sup>th</sup> order simulation method is quite accurate with a time step of
-simedtdlg.but.ttip.resettodefault = Reset the time step to its default value (
-simedtdlg.border.Simlist = Simulator listeners
-simedtdlg.txt.longA1 = <html><i>Simulation listeners</i> is an advanced feature that allows user-written code to listen to and interact with the simulation.
-simedtdlg.txt.longA2 = For details on writing simulation listeners, see the OpenRocket technical documentation.
-simedtdlg.lbl.Curlist = Current listeners:
-simedtdlg.lbl.Addsimlist = Add simulation listener
-simedtdlg.lbl.Noflightdata = No flight data available.
-simedtdlg.lbl.runsimfirst = Please run the simulation first.
-simedtdlg.chart.Simflight = Simulated flight
-simedtdlg.dlg.Simres = Simulation results
-simedtdlg.IntensityDesc.None = None
-simedtdlg.IntensityDesc.Verylow = Very low
-simedtdlg.IntensityDesc.Low = Low
-simedtdlg.IntensityDesc.Medium = Medium
-simedtdlg.IntensityDesc.High = High
-simedtdlg.IntensityDesc.Veryhigh = Very high
-simedtdlg.IntensityDesc.Extreme = Extreme
-
-GeodeticComputationStrategy.flat.name = Flat Earth
-GeodeticComputationStrategy.flat.desc = Perform computations with a flat Earth approximation. Sufficient for low-altitude flights.
-GeodeticComputationStrategy.spherical.name = Spherical approximation
-GeodeticComputationStrategy.spherical.desc = <html>Perform geodetic computations assuming a spherical Earth.<br>This is sufficiently accurate for almost all purposes.
-GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid
-GeodeticComputationStrategy.wgs84.desc = <html>Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.<br>Slower and unnecessary in most cases.
-
-
-
-
-! Simulation Panel
-simpanel.but.newsimulation = New simulation
-simpanel.but.editsimulation = Edit simulation
-simpanel.but.runsimulations = Run simulations
-simpanel.but.deletesimulations = Delete simulations
-simpanel.but.plotexport = Plot / export
-simpanel.but.ttip.newsimulation = Add a new simulation
-simpanel.but.ttip.editsim = Edit the selected simulation
-simpanel.but.ttip.runsimu = Re-run the selected simulations
-simpanel.but.ttip.deletesim = Delete the selected simulations
-simpanel.checkbox.donotask = Do not ask me again
-simpanel.lbl.defpref = You can change the default operation in the preferences.
-simpanel.dlg.lbl.DeleteSim1 = Delete the selected simulations?
-simpanel.dlg.lbl.DeleteSim2 = <html><i>This operation cannot be undone.</i>
-simpanel.dlg.lbl.DeleteSim3 = Delete simulations
-simpanel.col.Name = Name
-simpanel.col.Motors = Motors
-simpanel.col.Apogee = Apogee
-simpanel.col.Maxvelocity = Max. velocity
-simpanel.col.Maxacceleration = Max. acceleration
-simpanel.col.Timetoapogee = Time to apogee
-simpanel.col.Flighttime = Flight time
-simpanel.col.Groundhitvelocity = Ground hit velocity
-
-! SimulationRunDialog
-SimuRunDlg.title.RunSim = Running simulations...
-SimuRunDlg.lbl.Running = Running ...
-SimuRunDlg.lbl.Simutime = Simulation time:
-SimuRunDlg.lbl.Altitude = Altitude:
-SimuRunDlg.lbl.Velocity = Velocity:
-SimuRunDlg.msg.Unabletosim = Unable to simulate:
-SimuRunDlg.msg.errorOccurred = An error occurred during the simulation:
-SimuRunDlg.msg.AnException1 = An exception occurred during the simulation:
-SimuRunDlg.msg.AnException2 = Please report this as a bug along with the details below.
-SimuRunDlg.msg.AssertionError1 = A computation error occurred during the simulation.
-SimuRunDlg.msg.AssertionError2 = Please report this as a bug along with the details below.
-SimuRunDlg.msg.unknownerror1 = An unknown error was encountered during the simulation.
-SimuRunDlg.msg.unknownerror2 = The program may be unstable, you should save all your designs and restart OpenRocket now!
-
-
-RK4SimulationStepper.error.valuesTooLarge = Simulation values exceeded limits. Try selecting a shorter time step.
-
-
-! SimulationExportPanel
-SimExpPan.desc = Comma Separated Files (*.csv)
-SimExpPan.border.Vartoexport = Variables to export
-SimExpPan.but.Selectall = Select all
-SimExpPan.but.Selectnone = Select none
-SimExpPan.border.Fieldsep = Field separator
-SimExpPan.lbl.Fieldsepstr = Field separator string:
-SimExpPan.lbl.longA1 = <html>The string used to separate the fields in the exported file.<br>
-SimExpPan.lbl.longA2 = Use ',' for a Comma Separated Values (CSV) file.
-SimExpPan.checkbox.Includesimudesc = Include simulation description
-SimExpPan.checkbox.ttip.Includesimudesc = Include a comment at the beginning of the file describing the simulation.
-SimExpPan.border.Comments = Comments
-SimExpPan.checkbox.Includefielddesc = Include field descriptions
-SimExpPan.checkbox.ttip.Includefielddesc = Include a comment line with the descriptions of the exported variables.
-SimExpPan.checkbox.Incflightevents = Include flight events
-SimExpPan.checkbox.ttip.Incflightevents = Include a comment line for every flight event.
-SimExpPan.lbl.Commentchar = Comment character:
-SimExpPan.lbl.ttip.Commentchar = The character(s) that mark a comment line.
-SimExpPan.but.Exporttofile = Export to file...
-SimExpPan.Fileexists.desc1 = File \"
-SimExpPan.Fileexists.desc2 = \" exists. Overwrite?
-SimExpPan.Fileexists.title = File exists
-SimExpPan.ExportingVar.desc1 = Exporting 1 variable out of
-SimExpPan.ExportingVar.desc2 = Exporting
-SimExpPan.ExportingVar.desc3 = variables out of
-SimExpPan.Col.Variable = Variable
-SimExpPan.Col.Unit = Unit
-
-
-CsvOptionPanel.separator.space = SPACE
-CsvOptionPanel.separator.tab = TAB
-
-
-
-! MotorPlot
-MotorPlot.title.Motorplot = Motor plot
-MotorPlot.but.Select = Select
-MotorPlot.Chart.Motorthrustcurve = Motor thrust curve
-MotorPlot.Chart.Time = Time / s
-MotorPlot.Chart.Thrust = Thrust / N
-MotorPlot.txt.Designation = Designation:
-MotorPlot.txt.Manufacturer = Manufacturer:
-MotorPlot.txt.Type = Type:
-MotorPlot.txt.Delays = Delays:
-MotorPlot.txt.Comment = Comment:\n
-
-
-
-! Simulation plot panel
-simplotpanel.lbl.Presetplotconf = Preset plot configurations:
-simplotpanel.lbl.Xaxistype = X axis type:
-simplotpanel.lbl.Unit = Unit:
-simplotpanel.lbl.Yaxistypes = Y axis types:
-simplotpanel.lbl.Flightevents = Flight events:
-simplotpanel.but.All = All
-simplotpanel.but.None = None
-simplotpanel.but.NewYaxisplottype = New Y axis plot type
-simplotpanel.but.Plotflight = Plot flight
-simplotpanel.lbl.Axis = Axis:
-simplotpanel.but.ttip.Removethisplot = Remove this plot
-simplotpanel.Desc = The data will be plotted in time order even if the X axis type is not time.
-simplotpanel.OptionPane.lbl1 = A maximum of 15 plots is allowed.
-simplotpanel.OptionPane.lbl2 = Cannot add plot
-simplotpanel.AUTO_NAME = Auto
-simplotpanel.LEFT_NAME = Left
-simplotpanel.RIGHT_NAME = Right
-simplotpanel.CUSTOM = Custom
-SimulationPlotPanel.error.noPlotSelected = Please add one or more variables to plot on the Y-axis.
-SimulationPlotPanel.error.noPlotSelected.title = Nothing to plot
-
-
-! Component add buttons
-compaddbuttons.Bodycompandfinsets = Body components and fin sets
-compaddbuttons.Nosecone = Nose cone
-compaddbuttons.Bodytube = Body tube
-compaddbuttons.Transition = Transition
-compaddbuttons.Trapezoidal = Trapezoidal
-compaddbuttons.Elliptical = Elliptical
-compaddbuttons.Freeform = Freeform
-compaddbuttons.Launchlug = Launch lug
-compaddbuttons.Innercomponent = Inner component
-compaddbuttons.Innertube = Inner tube
-compaddbuttons.Coupler = Coupler
-compaddbuttons.Centeringring = Centering\nring
-compaddbuttons.Bulkhead = Bulkhead
-compaddbuttons.Engineblock = Engine\nblock
-compaddbuttons.Massobjects = Mass objects
-compaddbuttons.Parachute = Parachute
-compaddbuttons.Streamer = Streamer
-compaddbuttons.Shockcord = Shock cord
-compaddbuttons.Masscomponent = Mass\ncomponent
-compaddbuttons.Donotaskmeagain = Do not ask me again
-compaddbuttons.Selectcomppos = Select component position
-compaddbuttons.lbl.Youcanchange = You can change the default operation in the preferences.
-compaddbuttons.lbl.insertcomp = Insert the component after the current component or as the last component?
-compaddbuttons.askPosition.Inserthere = Insert here
-compaddbuttons.askPosition.Addtotheend = Add to the end
-compaddbuttons.askPosition.Cancel = Cancel
-
-! Component Analysis Dialog
-componentanalysisdlg.componentanalysis = Component analysis
-componentanalysisdlg.lbl.winddir = Wind direction:
-componentanalysisdlg.TitledBorder.warnings = Warnings:
-componentanalysisdlg.ToggleBut.worst = Worst
-componentanalysisdlg.lbl.angleofattack = Angle of attack:
-componentanalysisdlg.lbl.machnumber = Mach number:
-componentanalysisdlg.lbl.rollrate = Roll rate:
-componentanalysisdlg.lbl.activestages = Active stages:
-componentanalysisdlg.lbl.motorconf = Motor configuration:
-componentanalysisdlg.TabStability.Col = Component
-componentanalysisdlg.TabStability = Stability
-componentanalysisdlg.TabStability.ttip = Stability information
-componentanalysisdlg.dragTableModel.Col.Component = Component
-componentanalysisdlg.dragTableModel.Col.Pressure = <html>Pressure C<sub>D</sub>
-componentanalysisdlg.dragTableModel.Col.Base = <html>Base C<sub>D</sub>
-componentanalysisdlg.dragTableModel.Col.friction = <html>Friction C<sub>D</sub>
-componentanalysisdlg.dragTableModel.Col.total = <html>Total C<sub>D</sub>
-componentanalysisdlg.dragTabchar = Drag characteristics
-componentanalysisdlg.dragTabchar.ttip = Drag characteristics
-componentanalysisdlg.rollTableModel.Col.component = Component
-componentanalysisdlg.rollTableModel.Col.rollforc = Roll forcing coefficient
-componentanalysisdlg.rollTableModel.Col.rolldamp = Roll damping coefficient
-componentanalysisdlg.rollTableModel.Col.total = <html>Total C<sub>l</sub>
-componentanalysisdlg.rollTableModel = Roll dynamics
-componentanalysisdlg.rollTableModel.ttip = Roll dynamics
-componentanalysisdlg.println.closingmethod = Closing method called:
-componentanalysisdlg.println.settingnam = SETTING NAN VALUES
-componentanalysisdlg.lbl.reflenght = Reference length:
-componentanalysisdlg.lbl.refarea = Reference area:
-!componentanalysisdlg.But.close =Close
-componentanalysisdlg.TabStability.Col.Component = Component
-
-! Custom Material dialog
-custmatdlg.title.Custommaterial = Custom material
-custmatdlg.lbl.Materialname = Material name:
-custmatdlg.lbl.Materialtype = Material type:
-custmatdlg.lbl.Materialdensity = Material density:
-custmatdlg.checkbox.Addmaterial = Add material to database
-
-
-! Ring Component Config
-ringcompcfg.OuterRadius = OuterRadius
-ringcompcfg.Automatic = Automatic
-ringcompcfg.InnerRadius = InnerRadius
-ringcompcfg.Thickness = Thickness
-ringcompcfg.Length = Length
-ringcompcfg.Positionrelativeto = Position relative to:
-ringcompcfg.plus = plus
-ringcompcfg.PositionValue = PositionValue
-ringcompcfg.Radialdistance = Radial distance:
-ringcompcfg.Distancefrom = Distance from the rocket centerline
-ringcompcfg.Radialdirection = Radial direction:
-ringcompcfg.radialdirectionfrom = The radial direction from the rocket centerline
-ringcompcfg.but.Reset = Reset
-ringcompcfg.but.Resetcomponant = Reset the component to the rocket centerline
-ringcompcfg.EngineBlock.desc = <html>An <b>engine block</b> stops the motor from moving forwards in the motor mount tube.<br><br>In order to add a motor, create a <b>body tube</b> or <b>inner tube</b> and mark it as a motor mount in the <em>Motor</em> tab.
-ringcompcfg.note.desc = Note: An inner tube will not affect the aerodynamics of the rocket even if it is located outside of the body tube.
-
-
-! Body Tube Config
-BodyTubecfg.lbl.Bodytubelength = Body tube length:
-BodyTubecfg.lbl.Outerdiameter = Outer diameter:
-BodyTubecfg.lbl.Innerdiameter = Inner diameter:
-BodyTubecfg.lbl.Wallthickness = Wall thickness:
-BodyTubecfg.tab.General = General
-BodyTubecfg.tab.Generalproperties = General properties
-BodyTubecfg.tab.Motor = Motor
-BodyTubecfg.tab.Motormountconf = Motor mount configuration
-BodyTubecfg.checkbox.Automatic = Automatic
-BodyTubecfg.checkbox.Filled = Filled
-
-! FinSetConfig
-FinSetConfig.tab.Fintabs = Fin tabs
-FinSetConfig.tab.Through-the-wall = Through-the-wall fin tabs
-FinSetConfig.but.Converttofreeform = Convert to freeform
-FinSetConfig.but.Converttofreeform.ttip = Convert this fin set into a freeform fin set
-FinSetConfig.Convertfinset = Convert fin set
-FinSetConfig.but.Splitfins = Split fins
-FinSetConfig.but.Splitfins.ttip = Split the fin set into separate fins
-FinSetConfig.but.AutoCalc = Calculate automatically
-FinSetConfig.lbl.Through-the-wall = Through-the-wall fin tabs:
-FinSetConfig.lbl.Tablength = Tab length:
-FinSetConfig.ttip.Tablength = The length of the fin tab.
-FinSetConfig.lbl.Tabheight = Tab height:
-FinSetConfig.ttip.Tabheight = The spanwise height of the fin tab.
-FinSetConfig.lbl.Tabposition = Tab position:
-FinSetConfig.ttip.Tabposition = The position of the fin tab.
-FinSetConfig.lbl.relativeto = relative to
-
-!FinMarkingGuide
-FinMarkingGuide.lbl.Front = Front
-
-! MotorDatabaseLoadingDialog
-MotorDbLoadDlg.title = Loading motors
-MotorDbLoadDlg.Loadingmotors = Loading motors...
-
-! RocketConfig
-RocketCfg.lbl.Designname = Design name:
-RocketCfg.lbl.Designer = Designer:
-RocketCfg.lbl.Comments = Comments:
-RocketCfg.lbl.Revisionhistory = Revision history:
-RocketCfg.lbl.Material = Material:
-
-! ShockCordConfig
-ShockCordCfg.lbl.Shockcordlength = Shock cord length:
-
-! RocketComponentConfig
-RocketCompCfg.lbl.Componentname = Component name:
-RocketCompCfg.ttip.Thecomponentname = The component name.
-RocketCompCfg.tab.Override = Override
-RocketCompCfg.tab.MassandCGoverride = Mass and CG override options
-RocketCompCfg.tab.Figure = Figure
-RocketCompCfg.tab.Figstyleopt = Figure style options
-RocketCompCfg.tab.Comment = Comment
-RocketCompCfg.tab.Specifyacomment = Specify a comment for the component
-RocketCompCfg.lbl.Mass = Mass:
-RocketCompCfg.lbl.Componentmass = Component mass:
-RocketCompCfg.lbl.overriddento = (overridden to
-RocketCompCfg.lbl.overriddenby = (overridden by
-RocketCompCfg.lbl.Componentmaterial = Component material:
-RocketCompCfg.lbl.Componentfinish = Component finish:
-RocketCompCfg.lbl.ttip.componentmaterialaffects = The component material affects the weight of the component.
-RocketCompCfg.combo.ttip.componentmaterialaffects = The component material affects the weight of the component.
-RocketCompCfg.lbl.longA1 = <html>The component finish affects the aerodynamic drag of the component.<br>
-RocketCompCfg.lbl.longA2 = The value indicated is the average roughness height of the surface.
-RocketCompCfg.but.Setforall = Set for all
-RocketCompCfg.but.ttip.Setforall = Set this finish for all components of the rocket.
-RocketCompCfg.lbl.Overridemassorcenter = Override the mass or center of gravity of the
-RocketCompCfg.checkbox.Overridemass = Override mass:
-RocketCompCfg.checkbox.Overridecenterofgrav = Override center of gravity:
-RocketCompCfg.checkbox.OverridemassandCG = Override mass and CG of all subcomponents
-RocketCompCfg.lbl.longB1 = <html>The overridden mass does not include motors.<br>
-RocketCompCfg.lbl.longB2 = The center of gravity is measured from the front end of the
-RocketCompCfg.lbl.Commentsonthe = Comments on the
-RocketCompCfg.lbl.Figurestyle = Figure style:
-RocketCompCfg.lbl.Componentcolor = Component color:
-RocketCompCfg.lbl.Choosecolor = Choose color
-RocketCompCfg.checkbox.Usedefaultcolor = Use default color
-RocketCompCfg.lbl.Complinestyle = Component line style:
-RocketCompCfg.but.Saveasdefstyle = Save as default style
-RocketCompCfg.lbl.Diameter = Diameter:
-RocketCompCfg.lbl.Length = Length:
-RocketCompCfg.lbl.Thickness = Thickness:
-RocketCompCfg.checkbox.Endcapped = End capped
-RocketCompCfg.ttip.Endcapped = Whether the end of the shoulder is capped.
-RocketCompCfg.title.Noseconeshoulder = Nose cone shoulder
-RocketCompCfg.title.Aftshoulder = Aft shoulder
-RocketCompCfg.border.Foreshoulder = Fore shoulder
-!RocketCompCfg.lbl.Length = Length:
-
-! BulkheadConfig
-BulkheadCfg.tab.Diameter = Diameter:
-BulkheadCfg.tab.Thickness = Thickness:
-BulkheadCfg.tab.General = General
-BulkheadCfg.tab.Generalproperties = General properties
-
-!CenteringRingConfig
-CenteringRingCfg.tab.Outerdiam = Outer diameter:
-CenteringRingCfg.tab.Innerdiam = Inner diameter:
-CenteringRingCfg.tab.Thickness = Thickness:
-CenteringRingCfg.tab.General = General
-CenteringRingCfg.tab.Generalproperties = General properties
-
-!ComponentConfigDialog
-ComponentCfgDlg.configuration = configuration
-ComponentCfgDlg.configuration1 =
-ComponentCfgDlg.Modify = Modify
-
-!EllipticalFinSetConfig
-EllipticalFinSetCfg.Nbroffins = Number of fins:
-EllipticalFinSetCfg.Rotation = Rotation:
-EllipticalFinSetCfg.Fincant = Fin cant:
-EllipticalFinSetCfg.Rootchord = Root chord:
-EllipticalFinSetCfg.Height = Height:
-EllipticalFinSetCfg.Positionrelativeto = Position relative to:
-EllipticalFinSetCfg.plus = plus
-EllipticalFinSetCfg.FincrossSection = Fin cross section:
-EllipticalFinSetCfg.Thickness = Thickness:
-EllipticalFinSetCfg.General = General
-EllipticalFinSetCfg.Generalproperties = General properties
-EllipticalFinSetCfg.ttip.Fincant = The angle that the fins are canted with respect to the rocket body.
-
-!FreeformFinSetConfig
-FreeformFinSetCfg.tab.General = General
-FreeformFinSetCfg.tab.ttip.General = General properties
-FreeformFinSetCfg.tab.Shape = Shape
-FreeformFinSetCfg.tab.ttip.Finshape = Fin shape
-FreeformFinSetCfg.lbl.Numberoffins = Number of fins:
-FreeformFinSetCfg.lbl.Finrotation = Fin rotation:
-FreeformFinSetCfg.lbl.Fincant = Fin cant:
-FreeformFinSetCfg.lbl.ttip.Fincant = The angle that the fins are canted with respect to the rocket body.
-FreeformFinSetCfg.lbl.Posrelativeto = Position relative to:
-FreeformFinSetCfg.lbl.plus = plus
-FreeformFinSetCfg.lbl.FincrossSection = Fin cross section:
-FreeformFinSetCfg.lbl.Thickness = Thickness:
-! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle
-FreeformFinSetConfig.lbl.doubleClick1 = Double-click
-FreeformFinSetConfig.lbl.doubleClick2 = to edit
-FreeformFinSetConfig.lbl.clickDrag = Click+drag: Add and move points
-FreeformFinSetConfig.lbl.ctrlClick = Ctrl+click: Remove point
-
-
-!InnerTubeConfig
-InnerTubeCfg.tab.Motor = Motor
-InnerTubeCfg.tab.ttip.Motor = Motor mount configuration
-InnerTubeCfg.tab.Cluster = Cluster
-InnerTubeCfg.tab.ttip.Cluster = Cluster configuration
-InnerTubeCfg.tab.Radialpos = Radial position
-InnerTubeCfg.tab.ttip.Radialpos = Radial position
-InnerTubeCfg.lbl.Selectclustercfg = Select cluster configuration:
-InnerTubeCfg.lbl.TubeSep = Tube separation:
-InnerTubeCfg.lbl.ttip.TubeSep = The separation of the tubes, 1.0 = touching each other
-InnerTubeCfg.lbl.Rotation = Rotation:
-InnerTubeCfg.lbl.ttip.Rotation = Rotation angle of the cluster configuration
-InnerTubeCfg.lbl.Rotangle = Rotation angle of the cluster configuration
-InnerTubeCfg.but.Splitcluster = Split cluster
-InnerTubeCfg.lbl.longA1 = <html>Split the cluster into separate components.<br>
-InnerTubeCfg.lbl.longA2 = This also duplicates all components attached to this inner tube.
-InnerTubeCfg.but.Resetsettings = Reset settings
-InnerTubeCfg.but.ttip.Resetsettings = Reset the separation and rotation to the default values
-
-! LaunchLugConfig
-LaunchLugCfg.lbl.Length = Length:
-LaunchLugCfg.lbl.Outerdiam = Outer diameter:
-LaunchLugCfg.lbl.Innerdiam = Inner diameter:
-LaunchLugCfg.lbl.Thickness = Thickness:
-LaunchLugCfg.lbl.Radialpos = Radial position:
-LaunchLugCfg.lbl.Posrelativeto = Position relative to:
-LaunchLugCfg.lbl.plus = plus
-LaunchLugCfg.tab.General = General
-LaunchLugCfg.tab.Generalprop = General properties
-
-! MassComponentConfig
-MassComponentCfg.lbl.Mass = Mass:
-MassComponentCfg.lbl.Length = Length:
-MassComponentCfg.lbl.Diameter = Diameter:
-MassComponentCfg.lbl.PosRelativeto = Position relative to:
-MassComponentCfg.lbl.plus = plus
-MassComponentCfg.tab.General = General
-MassComponentCfg.tab.ttip.General = General properties
-MassComponentCfg.tab.Radialpos = Radial position
-MassComponentCfg.tab.ttip.Radialpos = Radial position configuration
-MassComponentCfg.lbl.Radialdistance = Radial distance:
-MassComponentCfg.lbl.Radialdirection = Radial direction:
-MassComponentCfg.but.Reset = Reset
-
-! MotorConfig
-MotorCfg.checkbox.compmotormount = This component is a motor mount
-MotorCfg.lbl.Motorcfg = Motor configuration:
-MotorCfg.but.New = New
-MotorCfg.lbl.Currentmotor = Current motor:
-MotorCfg.lbl.Motoroverhang = Motor overhang:
-MotorCfg.lbl.Ignitionat = Ignition at:
-MotorCfg.lbl.plus = plus
-MotorCfg.lbl.seconds = seconds
-MotorCfg.lbl.longA1 = The current design has only one stage.
-MotorCfg.lbl.longA2 = Stages can be added by clicking \"New stage\".
-MotorCfg.lbl.longB1 = The current design has
-MotorCfg.lbl.longB2 = stages.
-MotorCfg.but.Selectmotor = Select motor
-MotorCfg.but.Removemotor = Remove motor
-MotorCfg.lbl.motorLabel = None
-
-! NoseConeConfig
-NoseConeCfg.lbl.Noseconeshape = Nose cone shape:
-NoseConeCfg.lbl.Shapeparam = Shape parameter:
-NoseConeCfg.lbl.Noseconelength = Nose cone length:
-NoseConeCfg.lbl.Basediam = Base diameter:
-NoseConeCfg.checkbox.Automatic = Automatic
-NoseConeCfg.lbl.Wallthickness = Wall thickness:
-NoseConeCfg.checkbox.Filled = Filled
-NoseConeCfg.tab.General = General
-NoseConeCfg.tab.ttip.General = General properties
-NoseConeCfg.tab.Shoulder = Shoulder
-NoseConeCfg.tab.ttip.Shoulder = Shoulder properties
-
-! ParachuteConfig
-ParachuteCfg.lbl.Canopy = Canopy:
-ParachuteCfg.lbl.Diameter = Diameter:
-ParachuteCfg.lbl.Material = Material:
-ParachuteCfg.combo.MaterialModel = The component material affects the weight of the component.
-ParachuteCfg.lbl.longA1 = <html>Drag coefficient C<sub>D</sub>:
-ParachuteCfg.lbl.longB1 = <html>The drag coefficient relative to the total area of the parachute.<br>
-ParachuteCfg.lbl.longB2 = A larger drag coefficient yields a slowed descent rate.
-ParachuteCfg.lbl.longB3 = A typical value for parachutes is 0.8.
-ParachuteCfg.but.Reset = Reset
-ParachuteCfg.lbl.Shroudlines = Shroud lines:
-ParachuteCfg.lbl.Numberoflines = Number of lines:
-ParachuteCfg.lbl.Linelength = Line length:
-ParachuteCfg.lbl.Material = Material:
-ParachuteCfg.lbl.Posrelativeto = Position relative to:
-ParachuteCfg.lbl.plus = plus
-ParachuteCfg.lbl.Packedlength = Packed length:
-ParachuteCfg.lbl.Packeddiam = Packed diameter:
-ParachuteCfg.lbl.Deploysat = Deploys at:
-ParachuteCfg.lbl.seconds = seconds
-ParachuteCfg.lbl.Altitude = Altitude:
-ParachuteCfg.tab.General = General
-ParachuteCfg.tab.ttip.General = General properties
-ParachuteCfg.tab.Radialpos = Radial position
-ParachuteCfg.tab.ttip.Radialpos = Radial position configuration
-ParachuteCfg.lbl.Radialdistance = Radial distance:
-ParachuteCfg.lbl.Radialdirection = Radial direction:
-ParachuteCfg.but.Reset = Reset
-ParachuteCfg.lbl.plusdelay = plus
-
-! ShockCordConfig
-ShockCordCfg.lbl.Shockcordlength = Shock cord length:
-ShockCordCfg.lbl.Shockcordmaterial = Shock cord material:
-ShockCordCfg.lbl.Posrelativeto = Position relative to:
-ShockCordCfg.lbl.plus = plus
-ShockCordCfg.lbl.Packedlength = Packed length:
-ShockCordCfg.lbl.Packeddiam = Packed diameter:
-ShockCordCfg.tab.General = General
-ShockCordCfg.tab.ttip.General = General properties
-
-!SleeveConfig
-SleeveCfg.tab.Outerdiam = Outer diameter:
-SleeveCfg.tab.Innerdiam = Inner diameter:
-SleeveCfg.tab.Wallthickness = Wall thickness:
-SleeveCfg.tab.Length = Length:
-SleeveCfg.tab.General = General
-SleeveCfg.tab.Generalproperties = General properties
-
-! StreamerConfig
-StreamerCfg.lbl.Striplength = Strip length:
-StreamerCfg.lbl.Stripwidth = Strip width:
-StreamerCfg.lbl.Striparea = Strip area:
-StreamerCfg.lbl.Aspectratio = Aspect ratio:
-StreamerCfg.lbl.Material = Material:
-StreamerCfg.combo.ttip.MaterialModel = The component material affects the weight of the component.
-StreamerCfg.lbl.longA1 = <html>Drag coefficient C<sub>D</sub>:
-StreamerCfg.lbl.longB1 = <html>The drag coefficient relative to the total area of the streamer.<br>
-StreamerCfg.lbl.longB2 = A larger drag coefficient yields a slowed descent rate.
-StreamerCfg.lbl.Automatic = Automatic
-StreamerCfg.lbl.longC1 = The drag coefficient is relative to the area of the streamer.
-StreamerCfg.lbl.Posrelativeto = Position relative to:
-StreamerCfg.lbl.plus = plus
-StreamerCfg.lbl.Packedlength = Packed length:
-StreamerCfg.lbl.Packeddiam = Packed diameter:
-StreamerCfg.lbl.Deploysat = Deploys at:
-StreamerCfg.lbl.seconds = seconds
-StreamerCfg.lbl.Altitude = Altitude:
-StreamerCfg.tab.General = General
-StreamerCfg.tab.ttip.General = General properties
-StreamerCfg.tab.Radialpos = Radial position
-StreamerCfg.tab.ttip.Radialpos = Radial position configuration
-StreamerCfg.lbl.Radialdistance = Radial distance:
-StreamerCfg.lbl.Radialdirection = Radial direction:
-StreamerCfg.but.Reset = Reset
-StreamerCfg.lbl.plusdelay = plus
-
-! ThicknessRingComponentConfig
-ThicknessRingCompCfg.tab.Outerdiam = Outer diameter:
-ThicknessRingCompCfg.tab.Innerdiam = Inner diameter:
-ThicknessRingCompCfg.tab.Wallthickness = Wall thickness:
-ThicknessRingCompCfg.tab.Length = Length:
-ThicknessRingCompCfg.tab.General = General
-ThicknessRingCompCfg.tab.Generalprop = General properties
-
-! TransitionConfig
-TransitionCfg.lbl.Transitionshape = Transition shape:
-TransitionCfg.checkbox.Clipped = Clipped
-TransitionCfg.lbl.Shapeparam = Shape parameter:
-TransitionCfg.lbl.Transitionlength = Transition length:
-TransitionCfg.lbl.Forediam = Fore diameter:
-TransitionCfg.checkbox.Automatic = Automatic
-TransitionCfg.lbl.Aftdiam = Aft diameter:
-TransitionCfg.lbl.Wallthickness = Wall thickness:
-TransitionCfg.checkbox.Filled = Filled
-TransitionCfg.tab.General = General
-TransitionCfg.tab.Generalproperties = General properties
-TransitionCfg.tab.Shoulder = Shoulder
-TransitionCfg.tab.Shoulderproperties = Shoulder properties
-
-! TrapezoidFinSetConfig
-TrapezoidFinSetCfg.lbl.Nbroffins = Number of fins:
-TrapezoidFinSetCfg.lbl.ttip.Nbroffins = The number of fins in the fin set.
-TrapezoidFinSetCfg.lbl.Finrotation = Fin rotation:
-TrapezoidFinSetCfg.lbl.ttip.Finrotation = The angle of the first fin in the fin set.
-TrapezoidFinSetCfg.lbl.Fincant = Fin cant:
-TrapezoidFinSetCfg.lbl.ttip.Fincant =The angle that the fins are canted with respect to the rocket body.
-TrapezoidFinSetCfg.lbl.Rootchord = Root chord:
-TrapezoidFinSetCfg.lbl.Tipchord = Tip chord:
-TrapezoidFinSetCfg.lbl.Height = Height:
-TrapezoidFinSetCfg.lbl.Sweeplength = Sweep length:
-TrapezoidFinSetCfg.lbl.Sweepangle = Sweep angle:
-TrapezoidFinSetCfg.lbl.FincrossSection = Fin cross section:
-TrapezoidFinSetCfg.lbl.Thickness = Thickness:
-TrapezoidFinSetCfg.lbl.Posrelativeto = Position relative to:
-TrapezoidFinSetCfg.lbl.plus = plus
-TrapezoidFinSetCfg.tab.General = General
-TrapezoidFinSetCfg.tab.Generalproperties = General properties
-
-!MotorConfigurationModel
-MotorCfgModel.Editcfg = Edit configurations
-
-! StorageOptionChooser
-StorageOptChooser.lbl.Simdatatostore = Simulated data to store:
-StorageOptChooser.rdbut.Allsimdata = All simulated data
-StorageOptChooser.lbl.longA1 = <html>Store all simulated data.<br>
-StorageOptChooser.lbl.longA2 = This can result in very large files!
-StorageOptChooser.rdbut.Every = Every
-StorageOptChooser.lbl.longB1 = <html>Store plottable values approximately this far apart.<br>
-StorageOptChooser.lbl.longB2 = Larger values result in smaller files.
-StorageOptChooser.lbl.seconds = seconds
-StorageOptChooser.rdbut.Onlyprimfig = Only primary figures
-StorageOptChooser.lbl.longC1 = <html>Store only the values shown in the summary table.<br>
-StorageOptChooser.lbl.longC2 = This results in the smallest files.
-StorageOptChooser.checkbox.Compfile = Compress file
-StorageOptChooser.lbl.UsingComp = Using compression reduces the file size significantly.
-StorageOptChooser.lbl.longD1 = An estimate on how large the resulting file would be with the present options.
-StorageOptChooser.ttip.Saveopt = Save options
-StorageOptChooser.lbl.Estfilesize = Estimated file size:
-StorageOptChooser.lbl.Saveopt = Save options
-
-! ThrustCurveMotorSelectionPanel
-TCMotorSelPan.lbl.Selrocketmotor = Select rocket motor:
-TCMotorSelPan.checkbox.hideSimilar = Hide very similar thrust curves
-TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Show all motors
-TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Show motors with diameter less than that of the motor mount
-TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Show motors with diameter equal to that of the motor mount
-TCMotorSelPan.lbl.Motormountdia = Motor mount diameter:
-TCMotorSelPan.lbl.Search = Search:
-TCMotorSelPan.lbl.Selectthrustcurve = Select thrust curve:
-TCMotorSelPan.lbl.Ejectionchargedelay = Ejection charge delay:
-TCMotorSelPan.equalsIgnoreCase.None = None
-TCMotorSelPan.lbl.NumberofsecondsorNone = (Number of seconds or \"None\")
-TCMotorSelPan.lbl.Totalimpulse = Total impulse:
-TCMotorSelPan.lbl.Avgthrust = Avg. thrust:
-TCMotorSelPan.lbl.Maxthrust = Max. thrust:
-TCMotorSelPan.lbl.Burntime = Burn time:
-TCMotorSelPan.lbl.Launchmass = Launch mass:
-TCMotorSelPan.lbl.Emptymass = Empty mass:
-TCMotorSelPan.lbl.Datapoints = Data points:
-TCMotorSelPan.lbl.Digest = Digest:
-TCMotorSelPan.title.Thrustcurve = Thrust curve:
-TCMotorSelPan.title.Thrust = Thrust
-TCMotorSelPan.delayBox.None = None
-
-
-! PlotDialog
-PlotDialog.title.Flightdataplot = Flight data plot
-PlotDialog.Chart.Simulatedflight = Simulated flight
-PlotDialog.CheckBox.Showdatapoints = Show data points
-PlotDialog.lbl.Chart = Click and drag down+right to zoom in, up+left to zoom out
-
-
-! "main" prefix is used for the main application dialog
-
-# FIXME: Rename the description keys
-
-main.menu.file = File
-main.menu.file.desc = File-handling related tasks
-main.menu.file.new = New
-main.menu.file.new.desc = Create a new rocket design
-main.menu.file.open = Open...
-BasicFrame.item.Openrocketdesign = Open a rocket design
-main.menu.file.openExample = Open example...
-BasicFrame.item.Openexamplerocketdesign = Open an example rocket design
-main.menu.file.save = Save
-BasicFrame.item.SavecurRocketdesign = Save the current rocket design
-main.menu.file.saveAs = Save as...
-BasicFrame.item.SavecurRocketdesnewfile = Save the current rocket design to a new file
-main.menu.file.print = Print / Export PDF...
-main.menu.file.print.desc = Print or save as PDF the parts list and fin templates
-main.menu.file.close = Close
-BasicFrame.item.Closedesign = Close the current rocket design
-main.menu.file.quit = Quit
-BasicFrame.item.Quitprogram = Quit the program
-
-main.menu.edit = Edit
-BasicFrame.menu.Rocketedt = Rocket editing
-main.menu.edit.undo = Undo
-main.menu.edit.undo.desc = Undo the previous operation
-main.menu.edit.redo = Redo
-main.menu.edit.redo.desc = Redo the previously undone operation
-main.menu.edit.cut = Cut
-main.menu.edit.copy = Copy
-main.menu.edit.paste = Paste
-main.menu.edit.delete = Delete
-main.menu.edit.resize = Scale...
-main.menu.edit.resize.desc = Scale parts of the rocket design
-main.menu.edit.preferences = Preferences
-main.menu.edit.preferences.desc = Setup the application preferences
-
-main.menu.analyze = Analyze
-main.menu.analyze.desc = Rocket analysis
-main.menu.analyze.componentAnalysis = Component analysis
-main.menu.analyze.componentAnalysis.desc = Analyze the rocket components separately
-main.menu.analyze.optimization = Rocket optimization
-main.menu.analyze.optimization.desc = General rocket design optimization
-
-main.menu.help = Help
-main.menu.help.desc = Information about OpenRocket
-main.menu.help.tours = Guided tours
-main.menu.help.tours.desc = Take guided tours on OpenRocket
-main.menu.help.license = License
-main.menu.help.license.desc = OpenRocket license information
-main.menu.help.bugReport = Bug report
-main.menu.help.bugReport.desc = Information about reporting bugs in OpenRocket
-main.menu.help.debugLog = Debug log
-main.menu.help.debugLog.desc = View the OpenRocket debug log
-main.menu.help.about = About
-main.menu.help.about.desc = Copyright details about OpenRocket
-
-main.menu.debug = Debug
-main.menu.debug.whatisthismenu = What is this menu?
-main.menu.debug.createtestrocket = Create test rocket
-
-! database
-! Translate here all material database
-!
-
-! Material database
-! BULK_MATERIAL
-Databases.materials.Acrylic = Acrylic
-Databases.materials.Balsa = Balsa
-Databases.materials.Basswood = Basswood
-Databases.materials.Birch = Birch
-Databases.materials.Cardboard = Cardboard
-Databases.materials.Carbonfiber = Carbon fiber
-Databases.materials.Cork = Cork
-Databases.materials.DepronXPS = Depron (XPS)
-Databases.materials.Fiberglass = Fiberglass
-Databases.materials.Kraftphenolic = Kraft phenolic
-Databases.materials.Maple = Maple
-Databases.materials.Paperoffice = Paper (office)
-Databases.materials.Pine = Pine
-Databases.materials.Plywoodbirch = Plywood (birch)
-Databases.materials.PolycarbonateLexan = Polycarbonate (Lexan)
-Databases.materials.Polystyrene = Polystyrene
-Databases.materials.PVC = PVC
-Databases.materials.Spruce = Spruce
-Databases.materials.StyrofoamgenericEPS = Styrofoam (generic EPS)
-Databases.materials.StyrofoamBluefoamXPS = Styrofoam \"Blue foam\" (XPS)
-Databases.materials.Quantumtubing = Quantum tubing
-Databases.materials.BlueTube = Blue tube
-!SURFACE_MATERIAL
-Databases.materials.Ripstopnylon = Ripstop nylon
-Databases.materials.Mylar = Mylar
-Databases.materials.Polyethylenethin = Polyethylene (thin)
-Databases.materials.Polyethyleneheavy = Polyethylene (heavy)
-Databases.materials.Silk = Silk
-Databases.materials.Paperoffice = Paper (office)
-Databases.materials.Cellophane = Cellophane
-Databases.materials.Crepepaper = Cr\u00eape paper
-! LINE_MATERIAL
-Databases.materials.Threadheavy-duty = Thread (heavy-duty)
-Databases.materials.Elasticcordround2mm = Elastic cord (round 2mm, 1/16 in)
-Databases.materials.Elasticcordflat6mm = Elastic cord (flat 6mm, 1/4 in)
-Databases.materials.Elasticcordflat12mm = Elastic cord (flat 12mm, 1/2 in)
-Databases.materials.Elasticcordflat19mm = Elastic cord (flat 19mm, 3/4 in)
-Databases.materials.Elasticcordflat25mm = Elastic cord (flat 25mm, 1 in)
-Databases.materials.Braidednylon2mm = Braided nylon (2 mm, 1/16 in)
-Databases.materials.Braidednylon3mm = Braided nylon (3 mm, 1/8 in)
-Databases.materials.Tubularnylon11mm = Tubular nylon (11 mm, 7/16 in)
-Databases.materials.Tubularnylon14mm = Tubular nylon (14 mm, 9/16 in)
-Databases.materials.Tubularnylon25mm = Tubular nylon (25 mm, 1 in)
-
-! ExternalComponent
-ExternalComponent.Rough = Rough
-ExternalComponent.Unfinished = Unfinished
-ExternalComponent.Regularpaint = Regular paint
-ExternalComponent.Smoothpaint = Smooth paint
-ExternalComponent.Polished = Polished
-
-! LineStyle
-LineStyle.Solid = Solid
-LineStyle.Dashed = Dashed
-LineStyle.Dotted = Dotted
-LineStyle.Dash-dotted = Dash-dotted
-LineStyle.Defaultstyle = Default style
-
-! Shape
-Shape.Conical = Conical
-Shape.Conical.desc1 = A conical nose cone has a profile of a triangle.
-Shape.Conical.desc2 = A conical transition has straight sides.
-Shape.Ogive = Ogive
-Shape.Ogive.desc1 = An ogive nose cone has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube, values less than 1 produce <b>secant ogives</b>.
-Shape.Ogive.desc2 = An ogive transition has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube at the aft end, values less than 1 produce <b>secant ogives</b>.
-Shape.Ellipsoid = Ellipsoid
-Shape.Ellipsoid.desc1 = An ellipsoidal nose cone has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>.
-Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>. If the transition is not clipped, then the profile is extended at the center by the corresponding radius.
-Shape.Powerseries = Power series
-Shape.Powerseries.desc1 = A power series nose cone has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 this is a <b>\u00BD-power</b> or <b>parabolic</b> nose cone, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 a <b>conical</b> nose cone.
-Shape.Powerseries.desc2 = A power series transition has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 the transition is <b>\u00BD-power</b> or <b>parabolic</b>, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 <b>conical</b>.
-Shape.Parabolicseries = Parabolic series
-Shape.Parabolicseries.desc1 = A parabolic series nose cone has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> nose cone.
-Shape.Parabolicseries.desc2 = A parabolic series transition has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube at the aft end, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> transition.
-Shape.Haackseries = Haack series
-Shape.Haackseries.desc1 = The Haack series nose cones are designed to minimize drag. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> nose cone, which minimizes drag for fixed length and diameter, while a value of 0.333 produces an <b>LV-Haack</b> nose cone, which minimizes drag for fixed length and volume.
-Shape.Haackseries.desc2 = The Haack series <i>nose cones</i> are designed to minimize drag. These transition shapes are their equivalents, but do not necessarily produce optimal drag for transitions. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> shape, while a value of 0.333 produces an <b>LV-Haack</b> shape.
-
-
-! RocketComponent
-RocketComponent.Position.TOP = Top of the parent component
-RocketComponent.Position.MIDDLE = Middle of the parent component
-RocketComponent.Position.BOTTOM = Bottom of the parent component
-RocketComponent.Position.AFTER = After the parent component
-RocketComponent.Position.ABSOLUTE = Tip of the nose cone
-
-! LaunchLug
-LaunchLug.Launchlug = Launch lug
-! NoseCone
-NoseCone.NoseCone = Nose cone
-! Transition
-Transition.Transition = Transition
-!Stage
-Stage.Stage = Stage
-! BodyTube
-BodyTube.BodyTube = Body tube
-! TubeCoupler
-TubeCoupler.TubeCoupler = Tube coupler
-!InnerTube
-InnerTube.InnerTube = Inner Tube
-! TrapezoidFinSet
-TrapezoidFinSet.TrapezoidFinSet = Trapezoidal fin set
-! FreeformFinSet
-FreeformFinSet.FreeformFinSet = Freeform fin set
-!MassComponent
-MassComponent.MassComponent = Mass component
-! Parachute
-Parachute.Parachute = Parachute
-! ShockCord
-ShockCord.ShockCord = Shock cord
-! Bulkhead
-Bulkhead.Bulkhead = Bulkhead
-
-!Rocket
-Rocket.motorCount.Nomotor = [No motors]
-Rocket.compname.Rocket = Rocket
-
-!MotorMount
-MotorMount.IgnitionEvent.AUTOMATIC = Automatic (launch or ejection charge)
-MotorMount.IgnitionEvent.LAUNCH = Launch
-MotorMount.IgnitionEvent.EJECTION_CHARGE = First ejection charge of previous stage
-MotorMount.IgnitionEvent.BURNOUT = First burnout of previous stage
-MotorMount.IgnitionEvent.NEVER = Never
-
-!ComponentIcons
-ComponentIcons.Nosecone = Nose cone
-ComponentIcons.Bodytube = Body tube
-ComponentIcons.Transition = Transition
-ComponentIcons.Trapezoidalfinset = Trapezoidal fin set
-ComponentIcons.Ellipticalfinset = Elliptical fin set
-ComponentIcons.Freeformfinset = Freeform fin set
-ComponentIcons.Launchlug = Launch lug
-ComponentIcons.Innertube = Inner tube
-ComponentIcons.Tubecoupler = Tube coupler
-ComponentIcons.Centeringring = Centering ring
-ComponentIcons.Bulkhead = Bulk head
-ComponentIcons.Engineblock = Engine block
-ComponentIcons.Parachute = Parachute
-ComponentIcons.Streamer = Streamer
-ComponentIcons.Shockcord = Shock cord
-ComponentIcons.Masscomponent = Mass component
-ComponentIcons.disabled = (disabled)
-
-! StageAction
-StageAction.Stage = Stage
-
-! RecoveryDevice
-RecoveryDevice.DeployEvent.LAUNCH = Launch (plus NN seconds)
-RecoveryDevice.DeployEvent.EJECTION = First ejection charge of this stage
-RecoveryDevice.DeployEvent.APOGEE = Apogee
-RecoveryDevice.DeployEvent.ALTITUDE = Specific altitude during descent
-RecoveryDevice.DeployEvent.NEVER = Never
-
-! FlightEvent
-FlightEvent.Type.LAUNCH = Launch
-FlightEvent.Type.IGNITION = Motor ignition
-FlightEvent.Type.LIFTOFF = Lift-off
-FlightEvent.Type.LAUNCHROD = Launch rod clearance
-FlightEvent.Type.BURNOUT = Motor burnout
-FlightEvent.Type.EJECTION_CHARGE = Ejection charge
-FlightEvent.Type.STAGE_SEPARATION = Stage separation
-FlightEvent.Type.APOGEE = Apogee
-FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Recovery device deployment
-FlightEvent.Type.GROUND_HIT = Ground hit
-FlightEvent.Type.SIMULATION_END = Simulation end
-FlightEvent.Type.ALTITUDE = Altitude change
-
-! ThrustCurveMotorColumns
-TCurveMotorCol.MANUFACTURER = Manufacturer
-TCurveMotorCol.DESIGNATION = Designation
-TCurveMotorCol.TYPE = Type
-TCurveMotorCol.DIAMETER = Diameter
-TCurveMotorCol.LENGTH = Length
-
-! RocketInfo
-RocketInfo.lengthLine.Length = Length
-RocketInfo.lengthLine.maxdiameter = , max. diameter
-RocketInfo.massText1 = Mass with motors
-RocketInfo.massText2 = Mass with no motors
-RocketInfo.at = at M=
-RocketInfo.cgText = CG:
-RocketInfo.cpText = CP:
-RocketInfo.stabText = Stability:
-RocketInfo.Warning = Warning:
-RocketInfo.Calculating = Calculating...
-RocketInfo.Apogee = Apogee:
-RocketInfo.Maxvelocity = Max. velocity:
-RocketInfo.Maxacceleration = Max. acceleration:
-RocketInfo.apogeeValue = N/A
-RocketInfo.Mach = (Mach
-RocketInfo.velocityValue = N/A
-RocketInfo.accelerationValue = N/A
-
-! FinSet
-FinSet.CrossSection.SQUARE = Square
-FinSet.CrossSection.ROUNDED = Rounded
-FinSet.CrossSection.AIRFOIL = Airfoil
-FinSet.TabRelativePosition.FRONT = Root chord leading edge
-FinSet.TabRelativePosition.CENTER = Root chord midpoint
-FinSet.TabRelativePosition.END = Root chord trailing edge
-
-! FlightDataType
-FlightDataType.TYPE_TIME = Time
-FlightDataType.TYPE_ALTITUDE = Altitude
-FlightDataType.TYPE_VELOCITY_Z = Vertical velocity
-FlightDataType.TYPE_ACCELERATION_Z = Vertical acceleration
-FlightDataType.TYPE_VELOCITY_TOTAL = Total velocity
-FlightDataType.TYPE_ACCELERATION_TOTAL = Total acceleration
-FlightDataType.TYPE_POSITION_X = Position upwind
-FlightDataType.TYPE_POSITION_Y = Position parallel to wind
-FlightDataType.TYPE_POSITION_XY = Lateral distance
-FlightDataType.TYPE_POSITION_DIRECTION = Lateral direction
-FlightDataType.TYPE_VELOCITY_XY = Lateral velocity
-FlightDataType.TYPE_ACCELERATION_XY = Lateral acceleration
-FlightDataType.TYPE_AOA = Angle of attack
-FlightDataType.TYPE_ROLL_RATE = Roll rate
-FlightDataType.TYPE_PITCH_RATE = Pitch rate
-FlightDataType.TYPE_YAW_RATE = Yaw rate
-FlightDataType.TYPE_MASS = Mass
-FlightDataType.TYPE_LONGITUDINAL_INERTIA = Longitudinal moment of inertia
-FlightDataType.TYPE_ROTATIONAL_INERTIA = Rotational moment of inertia
-FlightDataType.TYPE_CP_LOCATION = CP location
-FlightDataType.TYPE_CG_LOCATION = CG location
-FlightDataType.TYPE_STABILITY = Stability margin calibers
-FlightDataType.TYPE_MACH_NUMBER = Mach number
-FlightDataType.TYPE_REYNOLDS_NUMBER = Reynolds number
-FlightDataType.TYPE_THRUST_FORCE = Thrust
-FlightDataType.TYPE_DRAG_FORCE = Drag force
-FlightDataType.TYPE_DRAG_COEFF = Drag coefficient
-FlightDataType.TYPE_AXIAL_DRAG_COEFF = Axial drag coefficient
-FlightDataType.TYPE_FRICTION_DRAG_COEFF = Friction drag coefficient
-FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Pressure drag coefficient
-FlightDataType.TYPE_BASE_DRAG_COEFF = Base drag coefficient
-FlightDataType.TYPE_NORMAL_FORCE_COEFF = Normal force coefficient
-FlightDataType.TYPE_PITCH_MOMENT_COEFF = Pitch moment coefficient
-FlightDataType.TYPE_YAW_MOMENT_COEFF = Yaw moment coefficient
-FlightDataType.TYPE_SIDE_FORCE_COEFF = Side force coefficient
-FlightDataType.TYPE_ROLL_MOMENT_COEFF = Roll moment coefficient
-FlightDataType.TYPE_ROLL_FORCING_COEFF = Roll forcing coefficient
-FlightDataType.TYPE_ROLL_DAMPING_COEFF = Roll damping coefficient
-FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Pitch damping coefficient
-FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Yaw damping coefficient
-FlightDataType.TYPE_REFERENCE_LENGTH = Reference lenght
-FlightDataType.TYPE_REFERENCE_AREA = Reference area
-FlightDataType.TYPE_ORIENTATION_THETA = Vertical orientation (zenith)
-FlightDataType.TYPE_ORIENTATION_PHI = Lateral orientation (azimuth)
-FlightDataType.TYPE_WIND_VELOCITY = Wind velocity
-FlightDataType.TYPE_AIR_TEMPERATURE = Air temperature
-FlightDataType.TYPE_AIR_PRESSURE = Air pressure
-FlightDataType.TYPE_SPEED_OF_SOUND = Speed of sound
-FlightDataType.TYPE_TIME_STEP = Simulation time step
-FlightDataType.TYPE_COMPUTATION_TIME = Computation time
-FlightDataType.TYPE_LATITUDE = Latitude
-FlightDataType.TYPE_LONGITUDE = Longitude
-FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration
-
-! PlotConfiguration
-PlotConfiguration.Verticalmotion = Vertical motion vs. time
-PlotConfiguration.Totalmotion = Total motion vs. time
-PlotConfiguration.Flightside = Flight side profile
-PlotConfiguration.Stability = Stability vs. time
-PlotConfiguration.Dragcoef = Drag coefficients vs. Mach number
-PlotConfiguration.Rollcharacteristics = Roll characteristics
-PlotConfiguration.Angleofattack = Angle of attack and orientation vs. time
-PlotConfiguration.Simulationtime = Simulation time step and computation time
-
-! Warning
-Warning.LargeAOA.str1 = Large angle of attack encountered.
-Warning.LargeAOA.str2 = Large angle of attack encountered (
-Warning.DISCONTINUITY = Discontinuity in rocket body diameter.
-Warning.THICK_FIN = Thick fins may not be modeled accurately.
-Warning.JAGGED_EDGED_FIN = Jagged-edged fin predictions may be inaccurate.
-Warning.LISTENERS_AFFECTED = Listeners modified the flight simulation
-Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Recovery device opened while motor still burning.
-Warning.FILE_INVALID_PARAMETER = Invalid parameter encountered, ignoring.
-
-
-! Scale dialog
-ScaleDialog.lbl.scaleRocket = Entire rocket
-ScaleDialog.lbl.scaleSubselection = Selection and all subcomponents
-ScaleDialog.lbl.scaleSelection = Only selected component
-ScaleDialog.title = Scale design
-ScaleDialog.lbl.scale = Scale:
-ScaleDialog.lbl.scale.ttip = Select whether to scale the entire design or only the selected component
-ScaleDialog.lbl.scaling = Scaling to apply:
-ScaleDialog.lbl.scaling.ttip = Resulting size, values above 100% grow and values below 100% shrink the design.
-! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"
-ScaleDialog.lbl.scaleFrom = Scale from
-ScaleDialog.lbl.scaleTo = to
-ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and resulting length.
-ScaleDialog.checkbox.scaleMass = Update explicit mass values
-ScaleDialog.checkbox.scaleMass.ttip = Scale mass component and override mass values by the cube of the scaling factor
-ScaleDialog.button.scale = Scale
-ScaleDialog.undo.scaleRocket = Scale rocket
-ScaleDialog.undo.scaleComponent = Scale component
-ScaleDialog.undo.scaleComponents = Scale components
-
-!icons
-Icons.Undo = Undo
-Icons.Redo = Redo
-
-OpenRocketPrintable.Partsdetail = Parts detail
-OpenRocketPrintable.Fintemplates = Fin templates
-OpenRocketPrintable.Transitiontemplates = Transition templates
-OpenRocketPrintable.Noseconetemplates = Nose Cone templates
-OpenRocketPrintable.Finmarkingguide = Fin marking guide
-OpenRocketPrintable.DesignReport = Design Report
-
-OpenRocketDocument.Redo = Redo
-OpenRocketDocument.Undo = Undo
-
-!EllipticalFinSet
-EllipticalFinSet.Ellipticalfinset = Elliptical fin set
-
-! Optimization
-
-! Modifiers
-
-optimization.modifier.nosecone.length = Length
-optimization.modifier.nosecone.length.desc = Optimize the nose cone length.
-optimization.modifier.nosecone.diameter = Diameter
-optimization.modifier.nosecone.diameter.desc = Optimize the nose cone base diameter.
-optimization.modifier.nosecone.thickness = Thickness
-optimization.modifier.nosecone.thickness.desc = Optimize the nose cone wall thickness.
-optimization.modifier.nosecone.shapeparameter = Shape parameter
-optimization.modifier.nosecone.shapeparameter.desc = Optimize the nose cone shape parameter.
-
-optimization.modifier.transition.length = Length
-optimization.modifier.transition.length.desc = Optimize the transition length.
-optimization.modifier.transition.forediameter = Fore diameter
-optimization.modifier.transition.forediameter.desc = Optimize the transition fore diameter.
-optimization.modifier.transition.aftdiameter = Aft diameter
-optimization.modifier.transition.aftdiameter.desc = Optimize the transition aft diameter.
-optimization.modifier.transition.thickness = Thickness
-optimization.modifier.transition.thickness.desc = Optimize the transition wall thickness.
-optimization.modifier.transition.shapeparameter = Shape parameter
-optimization.modifier.transition.shapeparameter.desc = Optimize the transition shape parameter.
-
-optimization.modifier.bodytube.length = Length
-optimization.modifier.bodytube.length.desc = Optimize the body tube length.
-optimization.modifier.bodytube.outerDiameter = Outer diameter
-optimization.modifier.bodytube.outerDiameter.desc = Optimize the body tube outer diameter while maintaining the wall thickness.
-optimization.modifier.bodytube.thickness = Thickness
-optimization.modifier.bodytube.thickness.desc = Optimize the body tube wall thickness.
-
-optimization.modifier.trapezoidfinset.rootChord = Root chord
-optimization.modifier.trapezoidfinset.rootChord.desc = Optimize the root chord length of the fin set (length of fin at the rocket body).
-optimization.modifier.trapezoidfinset.tipChord = Tip chord
-optimization.modifier.trapezoidfinset.tipChord.desc = Optimize the tip chord length of the fin set (length of fin at outer edge).
-optimization.modifier.trapezoidfinset.sweep = Sweep
-optimization.modifier.trapezoidfinset.sweep.desc = Optimize the sweep of the fin set (distance that the leading edge sweeps backwards).
-optimization.modifier.trapezoidfinset.height = Height
-optimization.modifier.trapezoidfinset.height.desc = Optimize the height (semi-span) of the fin set.
-
-optimization.modifier.ellipticalfinset.length = Root chord
-optimization.modifier.ellipticalfinset.length.desc = Optimize the root chord length of the fin set.
-optimization.modifier.ellipticalfinset.height = Height
-optimization.modifier.ellipticalfinset.height.desc = Optimize the height (semi-span) of the fin set.
-
-optimization.modifier.finset.cant = Cant angle
-optimization.modifier.finset.cant.desc = Optimize the cant angle of the fin set.
-optimization.modifier.finset.position = Position
-optimization.modifier.finset.position.desc = Optimize the fin set position along the rocket body.
-
-optimization.modifier.launchlug.length = Length
-optimization.modifier.launchlug.length.desc = Optimize the launch lug length.
-optimization.modifier.launchlug.outerDiameter = Outer diameter
-optimization.modifier.launchlug.outerDiameter.desc = Optimize the outer diameter of the launch lug.
-optimization.modifier.launchlug.thickness = Thickness
-optimization.modifier.launchlug.thickness.desc = Optimize the launch lug thickness while keeping the outer diameter constant.
-optimization.modifier.launchlug.position = Position
-optimization.modifier.launchlug.position.desc = Optimize the launch lug position along the rocket body.
-
-
-optimization.modifier.internalcomponent.position = Position
-optimization.modifier.internalcomponent.position.desc = Optimize the position of the component relative to the parent component.
-
-optimization.modifier.masscomponent.mass = Mass
-optimization.modifier.masscomponent.mass.desc = Optimize the mass of the mass component.
-
-optimization.modifier.parachute.diameter = Diameter
-optimization.modifier.parachute.diameter.desc = Optimize the parachute canopy diameter.
-optimization.modifier.parachute.coefficient = Drag coefficient
-optimization.modifier.parachute.coefficient.desc = Optimize the drag coefficient of the parachute. Typical parachutes have a drag coefficient of about 0.8.
-
-optimization.modifier.streamer.length = Length
-optimization.modifier.streamer.length.desc = Optimize the length of the streamer.
-optimization.modifier.streamer.width = Width
-optimization.modifier.streamer.width.desc = Optimize the width of the streamer.
-optimization.modifier.streamer.aspectRatio = Aspect ratio
-optimization.modifier.streamer.aspectRatio.desc = Optimize the aspect ratio of the streamer (length/width). You should NOT select streamer length or width at the same time with the aspect ratio.
-optimization.modifier.streamer.coefficient = Drag coefficient
-optimization.modifier.streamer.coefficient.desc = Optimize the drag coefficient of the streamer.
-
-optimization.modifier.recoverydevice.deployDelay = Deployment delay
-optimization.modifier.recoverydevice.deployDelay.desc = Optimize the deployment delay of the recovery device.
-optimization.modifier.recoverydevice.deployAltitude = Deployment altitude
-optimization.modifier.recoverydevice.deployAltitude.desc = Optimize the deployment altitude of the recovery device.
-
-optimization.modifier.rocketcomponent.overrideMass = Override mass
-optimization.modifier.rocketcomponent.overrideMass.desc = Optimize the overridden mass of the component.
-optimization.modifier.rocketcomponent.overrideCG = Override CG
-optimization.modifier.rocketcomponent.overrideCG.desc = Optimize the overridden center of gravity of the component.
-
-optimization.modifier.motormount.overhang = Motor overhang
-optimization.modifier.motormount.overhang.desc = Optimize the motor overhang.
-optimization.modifier.motormount.delay = Motor ignition delay
-optimization.modifier.motormount.delay.desc = Optimize the motor ignition delay.
-
-
-
-
-! General rocket design optimization dialog
-
-GeneralOptimizationDialog.title = Rocket optimization
-GeneralOptimizationDialog.goal.maximize = Maximize value
-GeneralOptimizationDialog.goal.minimize = Minimize value
-GeneralOptimizationDialog.goal.seek = Seek value of
-GeneralOptimizationDialog.btn.start = Start optimization
-GeneralOptimizationDialog.btn.stop = Stop optimization
-GeneralOptimizationDialog.lbl.paramsToOptimize = Parameters to optimize:
-GeneralOptimizationDialog.btn.add = Add
-GeneralOptimizationDialog.btn.add.ttip = Add the selected parameter to the optimization
-GeneralOptimizationDialog.btn.remove = Remove
-GeneralOptimizationDialog.btn.remove.ttip = Remove the selected parameter from the optimization
-GeneralOptimizationDialog.btn.removeAll = Remove all
-GeneralOptimizationDialog.btn.removeAll.ttip = Remove all parameters from the optimization
-GeneralOptimizationDialog.lbl.availableParams = Available parameters:
-GeneralOptimizationDialog.lbl.optimizationOpts = Optimization options
-GeneralOptimizationDialog.lbl.optimizeSim = Optimize simulation:
-GeneralOptimizationDialog.lbl.optimizeSim.ttip = Select which simulation to optimize
-GeneralOptimizationDialog.lbl.optimizeValue = Optimized value:
-GeneralOptimizationDialog.lbl.optimizeValue.ttip = Select what value is to be optimized
-GeneralOptimizationDialog.lbl.optimizeGoal = Optimization goal:
-GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Select the goal of the optimization
-GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Custom value to seek
-GeneralOptimizationDialog.lbl.requireStability = Required stability
-GeneralOptimizationDialog.lbl.requireMinStability = Minimum stability:
-GeneralOptimizationDialog.lbl.requireMinStability.ttip = Require a minimum static stability margin for the design
-GeneralOptimizationDialog.lbl.requireMaxStability = Maximum stability:
-GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Require a maximum static stability margin for the design
-GeneralOptimizationDialog.status.bestValue = Best value:
-GeneralOptimizationDialog.status.bestValue.ttip = Best optimization value found so far.
-GeneralOptimizationDialog.status.stepCount = Step count:
-GeneralOptimizationDialog.status.stepCount.ttip = Number of optimization steps that have been performed.
-GeneralOptimizationDialog.status.evalCount = Evaluations:
-GeneralOptimizationDialog.status.evalCount.ttip = Total number of function evaluations (simulations) that have been performed.
-GeneralOptimizationDialog.status.stepSize = Step size:
-GeneralOptimizationDialog.status.stepSize.ttip = Current optimization step size (relative to the optimization parameter ranges)
-GeneralOptimizationDialog.btn.plotPath = Plot path
-GeneralOptimizationDialog.btn.plotPath.ttip = Plot the optimization path (one and two dimensional optimization only)
-GeneralOptimizationDialog.btn.save = Save path
-GeneralOptimizationDialog.btn.save.ttip = Save the results of the function evaluations (simulations) as a CSV file.
-GeneralOptimizationDialog.btn.apply = Apply optimization
-GeneralOptimizationDialog.btn.apply.ttip = Apply the optimization results to the rocket design
-GeneralOptimizationDialog.btn.reset = Reset
-GeneralOptimizationDialog.btn.reset.ttip = Reset the rocket design to the current rocket design
-GeneralOptimizationDialog.btn.close = Close
-GeneralOptimizationDialog.btn.close.ttip = Close the dialog without modifying the rocket design
-GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters.
-GeneralOptimizationDialog.error.selectParams.title = Select optimization parameters
-GeneralOptimizationDialog.error.optimizationFailure.text = The optimization failed to run:
-GeneralOptimizationDialog.error.optimizationFailure.title = Optimization failed
-GeneralOptimizationDialog.undoText = Apply optimization
-GeneralOptimizationDialog.basicSimulationName = Basic simulation
-GeneralOptimizationDialog.noSimulationName = No simulation
-GeneralOptimizationDialog.table.col.parameter = Parameter
-GeneralOptimizationDialog.table.col.current = Current
-GeneralOptimizationDialog.table.col.min = Minimum
-GeneralOptimizationDialog.table.col.max = Maximum
-GeneralOptimizationDialog.export.header = Include header line
-GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions.
-GeneralOptimizationDialog.export.stability = Stability
-
-
-! Dialog for plotting optimization results
-OptimizationPlotDialog.title = Optimization results
-OptimizationPlotDialog.lbl.zoomInstructions = Click and drag down+right to zoom in, up+left to zoom out
-OptimizationPlotDialog.plot1d.title = Optimization result
-OptimizationPlotDialog.plot1d.series = Optimization result
-OptimizationPlotDialog.plot2d.title = Optimization path
-OptimizationPlotDialog.plot2d.path = Optimization path
-OptimizationPlotDialog.plot2d.evals = Evaluations
-OptimizationPlotDialog.plot.ttip.stability = Stability:
-OptimizationPlotDialog.plot.label.optimum = Optimum
-
-! Optimization parameters
-MaximumAltitudeParameter.name = Apogee altitude
-MaximumVelocityParameter.name = Maximum velocity
-MaximumAccelerationParameter.name = Maximum acceleration
-StabilityParameter.name = Stability
-GroundHitVelocityParameter.name = Ground hit speed
-LandingDistanceParameter.name = Landing distance
-TotalFlightTimeParameter.name = Total flight time
-DeploymentVelocityParameter.name = Velocity at parachute deployment
-
-
-! Compass directions drawn on a compass rose.
-CompassRose.lbl.north = N
-CompassRose.lbl.east = E
-CompassRose.lbl.south = S
-CompassRose.lbl.west = W
-
-! Compass directions with subdirections. These might not be localized even if the directions on the compass rose are.
-CompassSelectionButton.lbl.N = N
-CompassSelectionButton.lbl.NE = NE
-CompassSelectionButton.lbl.E = E
-CompassSelectionButton.lbl.SE = SE
-CompassSelectionButton.lbl.S = S
-CompassSelectionButton.lbl.SW = SW
-CompassSelectionButton.lbl.W = W
-CompassSelectionButton.lbl.NW = NW
-
-
-SlideShowDialog.btn.next = Next
-SlideShowDialog.btn.prev = Previous
-
-GuidedTourSelectionDialog.title = Guided tours
-GuidedTourSelectionDialog.lbl.selectTour = Select guided tour:
-GuidedTourSelectionDialog.lbl.description = Tour description:
-GuidedTourSelectionDialog.lbl.length = Number of slides:
-GuidedTourSelectionDialog.btn.start = Start tour!
-
-
+++ /dev/null
-\r
-#\r
-# German base translation file\r
-#\r
-# Should you need to add new logical keys here is the proposed method\r
-#\r
-# className.ComponantType.componantName\r
-#\r
-#\r
-# Text tokens within braces should not be translated, e.g.\r
-# "The file '{filename}' exists."\r
-# They are pieces that are inserted dynamically.\r
-#\r
-\r
-\r
-! Set to the name of the current translation file (used for debugging purposes)\r
-debug.currentFile = messages_de.properties\r
-\r
-! RocketActions\r
-RocketActions.checkbox.Donotaskmeagain = Nicht wieder fragen\r
-RocketActions.lbl.Youcanchangedefop = Die Standardaktion kann in den Einstellungen geändert werden.\r
-RocketActions.showConfirmDialog.lbl1 = Simulationen löschen?\r
-RocketActions.showConfirmDialog.lbl2 = <html><i>Diese Aktion kann nicht rückgängig gemacht werden.</i>\r
-RocketActions.showConfirmDialog.title = Simulationen löschen\r
-RocketActions.DelCompAct.Delete = Löschen\r
-RocketActions.DelCompAct.ttip.Delete = Die ausgewählte Komponente löschen.\r
-RocketActions.DelSimuAct.Delete = Löschen\r
-RocketActions.DelSimuAct.ttip.Delete = Die ausgewählte Simulation löschen.\r
-RocketActions.DelAct.Delete = Löschen\r
-RocketActions.DelAct.ttip.Delete = Die ausgewählte Komponente oder Simulation löschen.\r
-RocketActions.CutAction.Cut = Ausschneiden\r
-RocketActions.CutAction.ttip.Cut = Diese Komponente oder Simulation ausschneiden und aus dem Design entfernen\r
-RocketActions.CopyAct.Copy = Kopieren\r
-RocketActions.CopyAct.ttip.Copy = Komponente (und Subkomponenten) in die Zwischenablage kopieren.\r
-RocketActions.PasteAct.Paste = Einfügen\r
-RocketActions.PasteAct.ttip.Paste = Fügt die Komponente oder Simulation aus der Zwischenablage in das Design ein.\r
-RocketActions.EditAct.Edit = Bearbeiten\r
-RocketActions.EditAct.ttip.Edit = Die ausgewählte Komponente bearbeiten.\r
-RocketActions.NewStageAct.Newstage = Neue Stufe\r
-RocketActions.NewStageAct.ttip.Newstage = Fügt eine neue Stufe in das Raketendesign ein.\r
-RocketActions.ActBoosterstage = Booster-Stufe\r
-RocketActions.MoveUpAct.Moveup = Nach oben verschieben\r
-RocketActions.MoveUpAct.ttip.Moveup = Verschiebt diese Komponente nach oben.\r
-RocketActions.MoveDownAct.Movedown = Nach unten verschieben\r
-RocketActions.MoveDownAct.ttip.Movedown = Verschiebt diese Komponente nach unten.\r
-\r
-! RocketPanel\r
-RocketPanel.FigTypeAct.Sideview = Seitenansicht\r
-RocketPanel.FigTypeAct.ttip.Sideview = Seitenansicht\r
-RocketPanel.FigTypeAct.Backview = Rückansicht\r
-RocketPanel.FigTypeAct.ttip.Backview = Vorderansicht\r
-RocketPanel.lbl.Motorcfg = Motorkonfiguration\r
-RocketPanel.lbl.infoMessage = <html>Zum Auswählen klicken Shift+Klick andere auswählen Doppelklick zum Bearbeiten Klicken+Ziehen zum Verschieben\r
-\r
-\r
-! BasicFrame\r
-BasicFrame.SimpleFileFilter1 = Alle Raketendesigns (*.ork; *.rkt)\r
-BasicFrame.SimpleFileFilter2 = OpenRocket Designs (*.ork)\r
-BasicFrame.SimpleFileFilter3 = RockSim Designs (*.rkt)\r
-BasicFrame.tab.Rocketdesign = Raketendesign\r
-BasicFrame.tab.Flightsim = Flugsimulation\r
-BasicFrame.title.Addnewcomp = Neue Komponente hinzufügen\r
-BasicFrame.dlg.lbl1 = Design '\r
-BasicFrame.dlg.lbl2 = ' ist nicht gespeichert.\r
-BasicFrame.dlg.lbl3 = Möchten Sie es speichern?\r
-BasicFrame.dlg.title = Design nicht gespeichert\r
-BasicFrame.StageName.Sustainer = Hauptstufe\r
-BasicFrame.WarningDialog.txt1 = Die folgenden Probleme würden beim Öffnen festgestellt\r
-BasicFrame.WarningDialog.txt2 = Einige Designeigenschaften wurde eventuell nicht korrekt geladen.\r
-BasicFrame.WarningDialog.title = Warnungen während des Öffnens der Datei\r
-\r
-\r
-! General error messages used in multiple contexts\r
-error.fileExists.title = File exists\r
-error.fileExists.desc = File '{filename}' exists. Do you want to overwrite it?\r
-\r
-error.writing.title = Error writing file\r
-error.writing.desc = An error occurred while writing to the file:\r
-\r
-\r
-! Labels used in buttons of dialog windows\r
-button.ok = OK\r
-button.cancel = Abbrechen\r
-button.close = Schließen\r
-\r
-! Common labels used in buttons of dialog windows\r
-dlg.but.ok = OK\r
-dlg.but.cancel = Abbrechen\r
-dlg.but.close = Schließen\r
-\r
-\r
-! General file type names\r
-filetypes.pdf = PDF files\r
-\r
-\r
-! About Dialog\r
-AboutDialog.lbl.version = Version\r
-! The texts below provide additional credits for the translation maintainer\r
-! - In AboutDialog.lbl.translation replace "English" with the current language.\r
-! - AboutDialog.lbl.translator is the translator / group name (may be empty)\r
-! - AboutDialog.lbl.translatorWebsite is a URL to the translator / group (may be empty)\r
-! - AboutDialog.lbl.translatorIcon is the file name of an icon under pix/translators/ (may be empty)\r
-AboutDialog.lbl.translation = Ins Deutsche übersetzt von:\r
-AboutDialog.lbl.translator = Stefan Lobas (ERIG e.V.)\r
-AboutDialog.lbl.translatorWebsite = http://www.er-ig.de/\r
-AboutDialog.lbl.translatorIcon = ERIG_Logo-small.png\r
-\r
-\r
-! Print dialog\r
-PrintDialog.title = Drucken oder exportieren\r
-PrintDialog.but.previewAndPrint = Vorschau & Drucken\r
-PrintDialog.checkbox.showByStage = In Stufen anzeigen\r
-PrintDialog.lbl.selectElements = Elemente auswählen, die berücksichtigt werden sollen:\r
-printdlg.but.saveaspdf = Als PDF speichern\r
-printdlg.but.preview = Vorschau\r
-printdlg.but.settings = Einstellungen\r
-PrintDialog.error.preview.title = Vorschau kann nicht geöffnet werden\r
-PrintDialog.error.preview.desc1 = PDF-Vorschau kann nicht geöffnet werden\r
-PrintDialog.error.preview.desc2 = Bitte "Als PDF speichern" benutzen.\r
-\r
-\r
-!PrintSettingsDialog\r
-PrintSettingsDialog.title = Print settings\r
-PrintSettingsDialog.lbl.Templatefillcolor = Template fill color:\r
-PrintSettingsDialog.lbl.Templatebordercolor = Template border color:\r
-PrintSettingsDialog.lbl.Papersize = Paper size:\r
-PrintSettingsDialog.lbl.Paperorientation = Paper orientation:\r
-PrintSettingsDialog.but.Reset = Reset\r
-PrintSettingsDialog.but.Close = Close\r
-\r
-\r
-! Bug Report dialog\r
-bugreport.dlg.title = Fehlerbericht\r
-bugreport.dlg.but.Sendbugreport = Fehlerbericht senden\r
-bugreport.dlg.but.Sendbugreport.Ttip = Automatische einen Fehlerbericht an die OpenRocket-Entwickler senden.\r
-bugreport.dlg.successmsg1 = Fehlerbericht erfolgreich gesendet.\r
-bugreport.dlg.successmsg2 = Danke für die Hilfe, OpenRocket noch besser zu machen!\r
-bugreport.dlg.successmsg3 = Fehlerbericht gesendet\r
-bugreport.dlg.connectedInternet = <html>Wenn Sie mit dem Internet verbunden sind, können Sie einfach auf <em>Fehlerbericht senden</em> klicken.\r
-bugreport.dlg.otherwise = Sonst senden Sie den den folgenden Text an diese Adresse:\r
-bugreport.lbl.Theinformation = Die oben stehenden Informationen können in einem öffentlichen Fehlerbericht erscheinen. Bitte stellen Sie sicher, dass der Bericht keine sensiblen Informationen enthält, die nicht veröffentlicht werden sollen!\r
-bugreport.dlg.failedmsg1 = OpenRocket konnte den Fehlerbericht nicht versenden:\r
-bugreport.dlg.failedmsg2 = Bitte senden Sie den Bericht manuell an\r
-bugreport.dlg.failedmsg3 = Fehler beim Versenden des Berichts\r
-bugreport.reportDialog.txt = <html><b>Sie können eine Fehler in OpenRocket mitteilen, indem Sie das unten stehende Formular ausfüllen und abschicken.</b><br>Sie können Fehler mit angehängten Dateien auch auf der Projekt-Website mitteilen.\r
-bugreport.reportDialog.txt2 = Bitte beschreiben Sie kurz, was Sie getan haben, als der Fehler auftrat.</b>\r
-bugreport.dlg.provideDescription = Please provide a description of the bug first.\r
-bugreport.dlg.provideDescription.title = Bug description missing\r
-\r
-\r
-! Debug log dialog\r
-debuglogdlg.but.clear = Löschen\r
-debuglogdlg.OpenRocketdebuglog = OpenRocket Fehler-Log\r
-debuglogdlg.Displayloglines = Zeige Log-Zeilen:\r
-debuglogdlg.Follow = Folgen\r
-debuglogdlg.col.Time = Zeit\r
-debuglogdlg.col.Level = Level\r
-debuglogdlg.col.Location = Ort\r
-debuglogdlg.col.Message = Nachricht\r
-debuglogdlg.lbl.Loglinenbr = Log-Zeilennummer\r
-debuglogdlg.lbl.Time = Zeit:\r
-debuglogdlg.lbl.Level = Level:\r
-debuglogdlg.lbl.Location = Location:\r
-debuglogdlg.lbl.Logmessage = Log message:\r
-debuglogdlg.lbl.Stacktrace = Stack trace:\r
-\r
-\r
-! Edit Motor configuration dialog\r
-edtmotorconfdlg.but.removemotor = Motor entfernen\r
-edtmotorconfdlg.but.Selectmotor = Motor auswählen\r
-edtmotorconfdlg.but.Removeconfiguration = Konfiguration entfernen\r
-edtmotorconfdlg.but.Newconfiguration = Neue Konfiguration\r
-edtmotorconfdlg.lbl.Motormounts = <html><b>Motorhalterungen:</b>\r
-edtmotorconfdlg.title.Editmotorconf = Motorkonfiguration bearbeiten\r
-edtmotorconfdlg.selectcomp = <html>Auswählen, welche Komponenten Motorhalterungen sind:\r
-edtmotorconfdlg.lbl.Motorconfig = <html><b>Motorkonfigurationen:</b>\r
-edtmotorconfdlg.lbl.Configname = Name der Konfiguration:\r
-edtmotorconfdlg.lbl.Leavenamedefault = Leer lassen für Standardwert.\r
-\r
-! Example design dialog\r
-exdesigndlg.but.open = Öffnen\r
-exdesigndlg.lbl.Selectexample = Beispieldesigns zum Öffnen auswählen:\r
-exdesigndlg.lbl.Openexampledesign = Beispieldesign öffnen\r
-exdesigndlg.lbl.Exampledesignsnotfound = Beispieldesigns konnten nicht gefunden werden.\r
-exdesigndlg.lbl.Examplesnotfound = Beispieldesign konnten nicht gefunden werden\r
-\r
-\r
-! Material edit panel\r
-matedtpan.but.new = Neu\r
-matedtpan.but.edit = Bearbeiten\r
-matedtpan.but.delete = Löschen\r
-matedtpan.but.revertall = Alle löschen\r
-matedtpan.col.Material = Material\r
-matedtpan.col.Type = Typ\r
-matedtpan.col.Density = Dichte\r
-matedtpan.col.but.ttip.New = Neues Material hinzufügen\r
-matedtpan.title.Addcustmaterial = Benutzerdefiniertes Material hinzufügen\r
-matedtpan.but.ttip.edit = Bestehendes Material bearbeiten\r
-matedtpan.title.Editmaterial = Material bearbeiten\r
-matedtpan.title2.Editmaterial = Die mitgelieferten Materialien können nicht verändert werden.\r
-matedtpan.but.ttip.delete = Benutzerdefiniertes Material löschen\r
-matedtpan.but.ttip.revertall = Alle benutzerdefinierten Materialien löschen\r
-matedtpan.title.Deletealluser-defined = Alle benutzerdefinierten Materialien löschen?\r
-matedtpan.title.Revertall = Alle löschen?\r
-matedtpan.lbl.edtmaterials = Das Bearbeiten der Materialien beeinflusst keine bereits existierenden Raketendesigns.\r
-\r
-!MaterialModel\r
-MaterialModel.title.Material = Material\r
-MaterialModel.title.Defcustmat = Benutzerdefiniertes Material definieren\r
-\r
-\r
-! Preference dialog\r
-pref.dlg.but.add = Hinzufügen\r
-pref.dlg.but.reset = Zurücksetzen\r
-pref.dlg.but.checknow = Jetzt überprüfen\r
-pref.dlg.but.defaultmetric = Metrisches System\r
-pref.dlg.but.defaultimperial = Imperialistisches System\r
-pref.dlg.title.Preferences = Einstellungen\r
-pref.dlg.tab.Units = Einheiten\r
-pref.dlg.tab.Defaultunits = Standardeinheiten\r
-pref.dlg.tab.Materials = Materialien\r
-pref.dlg.tab.Custommaterials = Benutzerdefinierte Materialien\r
-pref.dlg.tab.Options = Optionen\r
-pref.dlg.tab.Miscellaneousoptions = Weiter Optionen\r
-pref.dlg.lbl.Positiontoinsert = Position, um neue Komponenten einzufügen:\r
-pref.dlg.lbl.Confirmdeletion = Löschen von Simulationen bestätigen\r
-pref.dlg.lbl.User-definedthrust = Benutzerdefinierte Schubkurven:\r
-pref.dlg.Allthrustcurvefiles = Alle Schubkurvendateien (*.eng; *.rrse; *.zzip; Verzeichnisse)\r
-pref.dlg.RASPfiles = RASP Schubkurven (*.eng)\r
-pref.dlg.RockSimfiles = RockSim Schubkurven(*.rse)\r
-pref.dlg.ZIParchives = ZIP-Archiv (*.zip)\r
-pref.dlg.checkbox.Checkupdates = Beim Starten auf neue Version prüfen\r
-pref.dlg.ttip.Checkupdatesnow = Jetzt auf neue Version prüfen\r
-pref.dlg.lbl.Selectprefunits = Wählen Sie Ihre bevorzugten Einheiten aus:\r
-pref.dlg.lbl.Rocketdimensions = Raketendimensionen:\r
-pref.dlg.lbl.Linedensity = Liniendichte:\r
-pref.dlg.lbl.Motordimensions = Motordimensionen:\r
-pref.dlg.lbl.Surfacedensity = Oberflächendichte:\r
-pref.dlg.lbl.Distance = Entfernung:\r
-pref.dlg.lbl.Bulkdensity = Bulk density::\r
-pref.dlg.lbl.Velocity = Geschwindigkeit\r
-pref.dlg.lbl.Surfaceroughness = Oberflächenrauhheit:\r
-pref.dlg.lbl.Acceleration = Beschleunigung:\r
-pref.dlg.lbl.Area = Fläche\r
-pref.dlg.lbl.Mass = Masse:\r
-pref.dlg.lbl.Angle = Winkel:\r
-pref.dlg.lbl.Force = Kraft:\r
-pref.dlg.lbl.Rollrate = Roll-Rate:\r
-pref.dlg.lbl.Totalimpulse = Gesamtimpuls:\r
-pref.dlg.lbl.Temperature = Temperatur:\r
-pref.dlg.lbl.Momentofinertia = Trägheitsmoment:\r
-pref.dlg.lbl.Pressure = Druck:\r
-pref.dlg.lbl.Stability = Stabilität:\r
-pref.dlg.lbl.FlightTime = Flight time:\r
-pref.dlg.lbl.effect1 = Die Änderungen werden wirksam, wenn Sie das nächste Mal ein Fenster öffnen.\r
-pref.dlg.lbl.Checkingupdates = Prüfe, ob Aktualisierungen verfügbar sind...\r
-pref.dlg.lbl.msg1 = Ein Fehler trat bei der Kommunikation mit dem Server auf.\r
-pref.dlg.lbl.msg2 = Es konnten keine Informationen über Programmaktualisierungen empfangen werden.\r
-pref.dlg.lbl.msg3 = Sie benutzen die neueste Version von OpenRocket.\r
-pref.dlg.lbl.msg4 = Keine Aktualisierungen verfügbar.\r
-pref.dlg.PrefChoiseSelector1 = Immer fragen\r
-pref.dlg.PrefChoiseSelector2 = in der Mitte einfügen\r
-pref.dlg.PrefChoiseSelector3 = an das Ende anhängen\r
-pref.dlg.PrefBooleanSelector1 = Löschen\r
-pref.dlg.PrefBooleanSelector2 = Bestätigen\r
-pref.dlg.Add = Hinzufügen\r
-pref.dlg.DescriptionArea.Adddirectories = Um eigene Schubkurven zu laden, Verzeichnisse, RASP-Motordateien (*.eng), RockSim-Motordateien (*.rse) oder ZIP-Archive mit Semikolon getrennt eingeben. Änderungen werden beim nächsten Neustart von OpenRocket übernommen.\r
-\r
-PreferencesDialog.lbl.language = Interface language:\r
-PreferencesDialog.languages.default = System default\r
-PreferencesDialog.lbl.languageEffect = The language will change the next time you start OpenRocket.\r
-\r
-! Simulation edit dialog\r
-simedtdlg.but.runsimulation = Simulation starten\r
-simedtdlg.but.resettodefault = Auf Standardeinstellungen zurücksetzen\r
-simedtdlg.but.add = Hinzufügen\r
-simedtdlg.but.remove = Entfernen\r
-simedtdlg.title.Editsim = Simulation bearbeiten\r
-simedtdlg.lbl.Simname = Name der Simulation:\r
-simedtdlg.tab.Launchcond = Startbedingungen\r
-simedtdlg.tab.Simopt = Simulationsoptionen\r
-simedtdlg.tab.Plotdata = Daten plotten\r
-simedtdlg.tab.Exportdata = Daten exportieren\r
-simedtdlg.lbl.Motorcfg = Motorkonfiguration:\r
-simedtdlg.lbl.ttip.Motorcfg = Motorkonfiguration auswählen\r
-simedtdlg.combo.ttip.motorconf = Die Motorkonfiguration auswählen.\r
-simedtdlg.lbl.Wind = Wind\r
-simedtdlg.lbl.Averwindspeed = Durchschnittliche Windgeschwindigkeit:\r
-simedtdlg.lbl.ttip.Averwindspeed = Die durchschnittliche Windgeschwindigkeit relativ zum Boden.\r
-simedtdlg.lbl.Stddeviation = Standardabweichung\r
-simedtdlg.lbl.ttip.Stddeviation = <html>Die Standardabweichung der Windgeschwindigkeit. <br>Die Windgeschwindigkeit liegt im Durchschnitt zu 95% der Zeit in der doppelten Standardabweichung.\r
-simedtdlg.lbl.Turbulenceintensity = Intensität der Turbulenz:\r
-simedtdlg.lbl.ttip.Turbulenceintensity1 = <html>Die Intensität der Turbulenz ist die Standardabweichung geteilt durch durch die durchschnittliche Windgeschwindigkeit.<br>\r
-simedtdlg.lbl.ttip.Turbulenceintensity2 = Typischer Wertebereich von\r
-simedtdlg.lbl.ttip.Turbulenceintensity3 = bis\r
-simedtdlg.border.Atmoscond = Atmosphärische Bedingungen\r
-simedtdlg.checkbox.InterStdAtmosphere = Internationale Standardatmosphäre benutzen\r
-simedtdlg.checkbox.ttip.InterStdAtmosphere1 = <html>Auswählen, um das Modell der Internationalen Standardatmosphäre zu verwenden.<br>In diesem Modell gilt eine Temperatur von\r
-simedtdlg.checkbox.ttip.InterStdAtmosphere2 = und ein Luftdruck von\r
-simedtdlg.checkbox.ttip.InterStdAtmosphere3 = auf Meeresniveau.\r
-simedtdlg.lbl.Temperature = Temperatur:\r
-simedtdlg.lbl.ttip.Temperature = Die Temperatur am Startplatz.\r
-simedtdlg.lbl.Pressure = Luftdruck:\r
-simedtdlg.lbl.ttip.Pressure = Der Luftdruck am Startplatz.\r
-simedtdlg.lbl.Launchsite = Startplatz\r
-simedtdlg.lbl.Latitude = Breitengrad:\r
-simedtdlg.lbl.ttip.Latitude = <html>Der Breitengrad des Startplatzes beeinflusst die wirksame Gravitationskraft.<br>Positive Werte liegen auf der Nordhalbkugel, negative Werte auf der Südhalbkugel.\r
-\r
-simedtdlg.lbl.Longitude = Longitude:\r
-simedtdlg.lbl.ttip.Longitude = <html>Required for weather prediction and elevation models.\r
-\r
-simedtdlg.lbl.Altitude = Höhe:\r
-simedtdlg.lbl.ttip.Altitude = <html>Die Höhe des Startplatzes über Meeresniveau.<br>Die Höhe des Startplatzes beeinflusst die Position der Rakete im atmosphärischen Modell.\r
-simedtdlg.border.Launchrod = Startrampe\r
-simedtdlg.lbl.Length = Länge:\r
-simedtdlg.lbl.ttip.Length = Die Länge der Startrampe\r
-simedtdlg.lbl.Angle = Winkel:\r
-simedtdlg.lbl.ttip.Angle = Der Winkel der Startrampe aus der Vertikalen.\r
-simedtdlg.lbl.Direction = Richtung:\r
-simedtdlg.lbl.ttip.Direction1 = <html>Richtung der Startrampe relativ zur Windrichtung<br>\r
-simedtdlg.lbl.ttip.Direction2 = = gegen den Wind.\r
-simedtdlg.lbl.ttip.Direction3 = = mit dem Wind\r
-simedtdlg.border.Simopt = Simulationsoptionen\r
-simedtdlg.lbl.Calcmethod = Berechnungsmethode\r
-simedtdlg.lbl.ttip.Calcmethod = <html>Die erweiterte Methode nach Barrowman berechnet die aerodynamischen Kräfte<br>nach den Gleichungen von Barrowman, die um weitere Faktoren erweitert wurden.\r
-simedtdlg.lbl.ExtBarrowman = Barrowman (erweitert)\r
-simedtdlg.lbl.Simmethod = Simulationsmethode:\r
-simedtdlg.lbl.ttip.Simmethod1 = <html>Der Sechs-Freiheitsgradsimulator erlaubt der Rakete völlige Bewegungsfreiheit während des Fluges.<br>\r
-simedtdlg.lbl.ttip.Simmethod2 = Das Integrieren wird nach dem numerischen Runge-Kutta-Verfahren 4. Ordnung durchgeführt.\r
-simedtdlg.lbl.GeodeticMethod = Geodetic calculations:\r
-simedtdlg.lbl.ttip.GeodeticMethodTip = Relate to the calculation of coordinates on the earth. This also enables coriolis effect computations.\r
-simedtdlg.lbl.Timestep = Zeitschritt:\r
-simedtdlg.lbl.ttip.Timestep1 = <html>Die Zeit zwischen den Simulationsschritten.<br>Kleinere Schritte ergeben genauere Ergebnisse, die Simulationen dauern aber länger.<br>\r
-simedtdlg.lbl.ttip.Timestep2 = Die Berechnung der Simulation mit dem Verfahren 4. Ordnung liefert gute Ergebnisse mit Zeitschritten von\r
-simedtdlg.but.ttip.resettodefault = Zeitschritte zurücksetzen auf den Standardwert (\r
-simedtdlg.border.Simlist = Simulationsempfänger\r
-simedtdlg.txt.longA1 = <html><i>Simulationsempfänger</i> sind ein fortgeschrittenes Feature, dass es benutzerdefinierten Programmen erlaubt, die Simulationsdaten zu empfangen und mit der Simulation zu interagieren. \r
-simedtdlg.txt.longA2 = Mehr Information zum Schreiben von Simualtionsempfängern sind in der OpenRocket technical documentation zu finden.\r
-simedtdlg.lbl.Curlist = Aktuelle Simulationsempfänger:\r
-simedtdlg.lbl.Addsimlist = Simulationsempfänger hinzufügen\r
-simedtdlg.lbl.Noflightdata = Keine Flugdaten verfügbar.\r
-simedtdlg.lbl.runsimfirst = Bitte erst die Simulation ausführen.\r
-simedtdlg.chart.Simflight = Simulierter Flug\r
-simedtdlg.dlg.Simres = Ergebnisse der Simulation\r
-simedtdlg.IntensityDesc.None = Keine\r
-simedtdlg.IntensityDesc.Verylow = Sehr niedrig\r
-simedtdlg.IntensityDesc.Low = Niedrig\r
-simedtdlg.IntensityDesc.Medium = Mittel\r
-simedtdlg.IntensityDesc.High = Hoch\r
-simedtdlg.IntensityDesc.Veryhigh = Sehr hoch\r
-simedtdlg.IntensityDesc.Extreme = Extrem\r
-\r
-GeodeticComputationStrategy.none.name = None\r
-GeodeticComputationStrategy.none.desc = Perform no geodetic computations.\r
-GeodeticComputationStrategy.spherical.name = Spherical approximation\r
-GeodeticComputationStrategy.spherical.desc = <html>Perform geodetic computations assuming a spherical Earth.<br>This is sufficiently accurate for almost all purposes.\r
-GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid\r
-GeodeticComputationStrategy.wgs84.desc = <html>Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.<br>Slower and unnecessary in most cases.\r
-\r
-\r
-\r
-\r
-! Simulation Panel\r
-simpanel.but.newsimulation = Neue Simulation\r
-simpanel.but.editsimulation = Simulation bearbeiten\r
-simpanel.but.runsimulations = Simulation ausführen\r
-simpanel.but.deletesimulations = Simulation löschen\r
-simpanel.but.plotexport = Plotten / exportieren\r
-simpanel.but.ttip.newsimulation = Neue Simulation hinzufügen\r
-simpanel.but.ttip.editsim = Ausgewählte Simulation bearbeiten\r
-simpanel.but.ttip.runsimu = Neuberechnen der ausgewählten Simulationen\r
-simpanel.but.ttip.deletesim = Ausgewählte Simulationen löschen\r
-simpanel.checkbox.donotask = Nicht wieder fragen\r
-simpanel.lbl.defpref = Die Standardaktion kann in den Einstellungen geändert werden.\r
-simpanel.dlg.lbl.DeleteSim1 = Die ausgewählten Simulationen löschen?\r
-simpanel.dlg.lbl.DeleteSim2 = <html><i>Diese Aktion kann nicht rückgängig gemacht werden.</i>\r
-simpanel.dlg.lbl.DeleteSim3 = Simulationen löschen\r
-simpanel.col.Name = Name der Simulation:\r
-simpanel.col.Motors = Motoren\r
-simpanel.col.Apogee = Apogäum\r
-simpanel.col.Maxvelocity = max. Geschwindigkeit\r
-simpanel.col.Maxacceleration = max. Beschleunigung\r
-simpanel.col.Timetoapogee = Zeit bis zum Apogäum\r
-simpanel.col.Flighttime = Flugzeit\r
-simpanel.col.Groundhitvelocity = Landegeschwindigkeit\r
-\r
-! SimulationRunDialog\r
-SimuRunDlg.title.RunSim = Simuliere...\r
-SimuRunDlg.lbl.Running = Arbeite...\r
-SimuRunDlg.lbl.Simutime = Simulationsdauer:\r
-SimuRunDlg.lbl.Altitude = Höhe:\r
-SimuRunDlg.lbl.Velocity = Geschwindigkeit:\r
-SimuRunDlg.msg.Unabletosim = Simulieren nicht möglich:\r
-SimuRunDlg.msg.errorOccurred = Während der Simulation trat ein Fehler auf:\r
-SimuRunDlg.msg.AnException1 = Während der Simulation trat eine Ausnahme auf:\r
-SimuRunDlg.msg.AnException2 = Bitte berichten Sie diesen Fehler mit den unten stehenden Details.\r
-SimuRunDlg.msg.AssertionError1 = Während der Simulation trat ein Berechnungsfehler auf:\r
-SimuRunDlg.msg.AssertionError2 = Bitte berichten Sie diesen Fehler mit den unten stehenden Details.\r
-SimuRunDlg.msg.unknownerror1 = Während der Simulation trat ein unbekannter Fehler auf:\r
-SimuRunDlg.msg.unknownerror2 = Das Programm könnte instabil sein, speichern Sie Ihr Design und starten Sie OpenRocket neu!\r
-\r
-\r
-\r
-! SimulationExportPanel\r
-SimExpPan.desc = Komma getrennte Werte (*.csv)\r
-SimExpPan.border.Vartoexport = zu exportierende Variablen\r
-SimExpPan.but.Selectall = Alle auswählen\r
-SimExpPan.but.Selectnone = Keine auswählen\r
-SimExpPan.border.Fieldsep = Feldtrennung\r
-SimExpPan.lbl.Fieldsepstr = Trennzeichen\r
-SimExpPan.lbl.longA1 = <html>Das Trennzeichen wird benutzt, um die Felder in der exportierten Datei voneinander zu trennen.<br>\r
-SimExpPan.lbl.longA2 = Für eine CSV-Datei (Comma Separated Values) ein ',' benutzen.\r
-SimExpPan.checkbox.Includesimudesc = Simulationsbeschreibung einfügen\r
-SimExpPan.checkbox.ttip.Includesimudesc = Fügt einen Kommentar mit einer Simulationsbeschreibung am Anfang der Datei ein.\r
-SimExpPan.border.Comments = Kommentare\r
-SimExpPan.checkbox.Includefielddesc = Feldbeschreibungen einfügen\r
-SimExpPan.checkbox.ttip.Includefielddesc = Fügt eine Kommentarzeile mit der Beschreibung der exportierten Variablen ein.\r
-SimExpPan.checkbox.Incflightevents = Flugereignisse einfügen\r
-SimExpPan.checkbox.ttip.Incflightevents = Fügt eine Kommentarzeile für jedes Flugereignis ein.\r
-SimExpPan.lbl.Commentchar = Kommentarzeichen:\r
-SimExpPan.lbl.ttip.Commentchar = Zeichen, das einen Kommentar in der exportierten Datei kennzeichnet.\r
-SimExpPan.but.Exporttofile = In Datei exportieren...\r
-SimExpPan.Fileexists.desc1 = File \"",Datei \«"\r
-SimExpPan.Fileexists.desc2 = \" existiert bereits. Überschreiben?"\r
-SimExpPan.Fileexists.title = Datei existiert bereits\r
-SimExpPan.ExportingVar.desc1 = Exportiere Variable 1 aus\r
-SimExpPan.ExportingVar.desc2 = Exportiere\r
-SimExpPan.ExportingVar.desc3 = Variablen aus\r
-SimExpPan.Col.Variable = Variable\r
-SimExpPan.Col.Unit = Einheit\r
-\r
-\r
-CsvOptionPanel.separator.space = SPACE\r
-CsvOptionPanel.separator.tab = TAB\r
-\r
-\r
-\r
-! MotorPlot\r
-MotorPlot.title.Motorplot = Motorkurve\r
-MotorPlot.but.Select = Auswahl\r
-MotorPlot.Chart.Motorthrustcurve = Motorschubkurve\r
-MotorPlot.Chart.Time = Zeit / s\r
-MotorPlot.Chart.Thrust = Schub / N\r
-MotorPlot.txt.Designation = Bezeichnung:\r
-MotorPlot.txt.Manufacturer = Hersteller\r
-MotorPlot.txt.Type = Typ:\r
-MotorPlot.txt.Delays = Verzögerungen:\r
-MotorPlot.txt.Comment = Kommentare:\n\r
-\r
-\r
-\r
-! Simulation plot panel\r
-simplotpanel.lbl.Presetplotconf = Plotparameter setzen\r
-simplotpanel.lbl.Xaxistype = X-Achse:\r
-simplotpanel.lbl.Unit = Einheit:\r
-simplotpanel.lbl.Yaxistypes = Y-Achse:\r
-simplotpanel.lbl.Flightevents = Flugereignisse:\r
-simplotpanel.but.All = Alle auswählen\r
-simplotpanel.but.None = Keine\r
-simplotpanel.but.NewYaxisplottype = Neuer Y-Achsenplot-Typ\r
-simplotpanel.but.Plotflight = Flug plotten\r
-simplotpanel.lbl.Axis = Achsen:\r
-simplotpanel.but.ttip.Removethisplot = Diesen Plot löschen\r
-simplotpanel.Desc = Die Daten werden in zeitlicher Reihenfolge geplottet, auch wenn der X-Achsen-Typ nicht Zeit ist.\r
-simplotpanel.OptionPane.lbl1 = Es sind maximal 15 Plots erlaubt.\r
-simplotpanel.OptionPane.lbl2 = Plot konnte nicht hinzugefügt werden\r
-simplotpanel.AUTO_NAME = Auto\r
-simplotpanel.LEFT_NAME = Links\r
-simplotpanel.RIGHT_NAME = Rechts\r
-simplotpanel.CUSTOM = Benutzerdefiniert\r
-\r
-! Component add buttons\r
-compaddbuttons.Bodycompandfinsets = Körperteile und Leitwerke\r
-compaddbuttons.Nosecone = Spitze\r
-compaddbuttons.Bodytube = Körperrohr\r
-compaddbuttons.Transition = Übergang\r
-compaddbuttons.Trapezoidal = Trapeziod\r
-compaddbuttons.Elliptical = Elliptisch\r
-compaddbuttons.Freeform = Freiform\r
-compaddbuttons.Launchlug = Leit-\nröhrchen\r
-compaddbuttons.Innercomponent = Innenteile\r
-compaddbuttons.Innertube = Innenrohr\r
-compaddbuttons.Coupler = Koppler\r
-compaddbuttons.Centeringring = Zentrier-\nring\r
-compaddbuttons.Bulkhead = Schott\r
-compaddbuttons.Engineblock = Motor-\nblock\r
-compaddbuttons.Massobjects = Massenobjekte\r
-compaddbuttons.Parachute = Fallschirm\r
-compaddbuttons.Streamer = Strömer\r
-compaddbuttons.Shockcord = Gummiband\r
-compaddbuttons.Masscomponent = Massen-\nobjekt\r
-compaddbuttons.Donotaskmeagain = Nicht wieder fragen\r
-compaddbuttons.Selectcomppos = Komponentenposition auswählen\r
-compaddbuttons.lbl.Youcanchange = Die Standardaktion kann in den Einstellungen geändert werden.\r
-compaddbuttons.lbl.insertcomp = Die Komponente nach der aktuellen Komponente oder als letzte Komponente einfügen?\r
-compaddbuttons.askPosition.Inserthere = Hier einfügen\r
-compaddbuttons.askPosition.Addtotheend = Zum Ende hinzufügen\r
-compaddbuttons.askPosition.Cancel = Abbrechen\r
-\r
-! Component Analysis Dialog\r
-componentanalysisdlg.componentanalysis = Component analysis\r
-componentanalysisdlg.lbl.winddir = Windrichtung\r
-componentanalysisdlg.TitledBorder.warnings = Warnungen:\r
-componentanalysisdlg.ToggleBut.worst = Worst\r
-componentanalysisdlg.lbl.angleofattack = Angriffswinkel:\r
-componentanalysisdlg.lbl.machnumber = Machzahl:\r
-componentanalysisdlg.lbl.rollrate = Rollrate:\r
-componentanalysisdlg.lbl.activestages = Aktive Stufen:\r
-componentanalysisdlg.lbl.motorconf = Motorkonfiguration:\r
-componentanalysisdlg.TabStability.Col = Komponente\r
-componentanalysisdlg.TabStability = Stabilität\r
-componentanalysisdlg.TabStability.ttip = Stabilitätsinformationen\r
-componentanalysisdlg.dragTableModel.Col.Component = Komponente\r
-componentanalysisdlg.dragTableModel.Col.Pressure = <html>Druck C<sub>D</sub>\r
-componentanalysisdlg.dragTableModel.Col.Base = <html>Base C<sub>D</sub>\r
-componentanalysisdlg.dragTableModel.Col.friction = <html>Reibung C<sub>D</sub>\r
-componentanalysisdlg.dragTableModel.Col.total = <html>Gesamt C<sub>D</sub>\r
-componentanalysisdlg.dragTabchar = Luftwiderstand\r
-componentanalysisdlg.dragTabchar.ttip = Luftwiderstands-Eigenschaften\r
-componentanalysisdlg.rollTableModel.Col.component = Komponente\r
-componentanalysisdlg.rollTableModel.Col.rollforc = Roll forcing coefficient\r
-componentanalysisdlg.rollTableModel.Col.rolldamp = Roll damping coefficient\r
-componentanalysisdlg.rollTableModel.Col.total = <html>Gesamt C<sub>l</sub>\r
-componentanalysisdlg.rollTableModel = Rolldynamik\r
-componentanalysisdlg.rollTableModel.ttip = Rolldynamik\r
-componentanalysisdlg.println.closingmethod = Closing method called:\r
-componentanalysisdlg.println.settingnam = SETTING NAN VALUES\r
-componentanalysisdlg.lbl.reflenght = Referenzlänge:\r
-componentanalysisdlg.lbl.refarea = Referenzfläche:\r
-!componentanalysisdlg.But.close =Close\r
-componentanalysisdlg.TabStability.Col.Component = Component\r
-\r
-! Custom Material dialog\r
-custmatdlg.title.Custommaterial = Benutzerdefiniertes Material\r
-custmatdlg.lbl.Materialname = Name des Materials:\r
-custmatdlg.lbl.Materialtype = Materialtyp\r
-custmatdlg.lbl.Materialdensity = Materialdichte:\r
-custmatdlg.checkbox.Addmaterial = Material zur Datenbank hinzufügen\r
-\r
-\r
-! Ring Component Config\r
-ringcompcfg.OuterRadius = Äußerer Radius\r
-ringcompcfg.Automatic = Automatisch\r
-ringcompcfg.InnerRadius = Innerer Radius\r
-ringcompcfg.Thickness = Wandstärke\r
-ringcompcfg.Length = Länge\r
-ringcompcfg.Positionrelativeto = Relative Position zu:\r
-ringcompcfg.plus = plus\r
-ringcompcfg.PositionValue = Positionswert\r
-ringcompcfg.Radialdistance = Radialer Abstand:\r
-ringcompcfg.Distancefrom = Abstand von der Raketenmittellinie\r
-ringcompcfg.Radialdirection = Radiale Richtung\r
-ringcompcfg.radialdirectionfrom = Die radiale Richtung von der Raketenmittellinie\r
-ringcompcfg.but.Reset = Zurücksetzen\r
-ringcompcfg.but.Resetcomponant = Komponente auf die Raketenmittellinie zurücksetzen\r
-ringcompcfg.EngineBlock.desc = <html>Eine <b>Motorhalterung</b> verhindert, dass der Motor sich im Rohr nach vorne bewegt.<br><br>Um einen Motor hinzuzufügen, ein <b>Körperrohr</b> oder ein <b>Innenrohr</b> hinzufügen und im Reiter <em>Motor</em> als Motorhalterung markieren.\r
-ringcompcfg.note.desc = Hinweis: Innenrohre beeinflussen die Aerodynamik der Rakete nicht, auch wenn sie außerhalb des Körperohres liegen.\r
-\r
-\r
-! Body Tube Config\r
-BodyTubecfg.lbl.Bodytubelength = Länge des Körperrohres:\r
-BodyTubecfg.lbl.Outerdiameter = Außendurchmesser:\r
-BodyTubecfg.lbl.Innerdiameter = Innendurchmesser:\r
-BodyTubecfg.lbl.Wallthickness = Wandstärke:\r
-BodyTubecfg.tab.General = Allgemein\r
-BodyTubecfg.tab.Generalproperties = Allgemeine Eigenschaften\r
-BodyTubecfg.tab.Motor = Motor\r
-BodyTubecfg.tab.Motormountconf = Motorkonfiguration\r
-BodyTubecfg.checkbox.Automatic = Automatisch\r
-BodyTubecfg.checkbox.Filled = Gefüllt\r
-\r
-! FinSetConfig\r
-FinSetConfig.tab.Fintabs = Leitwerke\r
-FinSetConfig.tab.Through-the-wall = Durchsteckbare Leitwerke\r
-FinSetConfig.but.Converttofreeform = In Freiform konvertieren\r
-FinSetConfig.but.Converttofreeform.ttip = Konvertiert diese Leitwerke in eine Freiform\r
-FinSetConfig.Convertfinset = Leitwerke konvertieren\r
-FinSetConfig.but.Splitfins = Geteilte Leitwerke\r
-FinSetConfig.but.Splitfins.ttip = Teilt den Leitwerkssatz in getrennte Leitwerke\r
-FinSetConfig.lbl.Through-the-wall = Durchsteckbare Leitwerke:\r
-FinSetConfig.lbl.Tablength = Länge:\r
-FinSetConfig.ttip.Tablength = Länge des Leitwerks.\r
-FinSetConfig.lbl.Tabheight = Höhe:\r
-FinSetConfig.ttip.Tabheight = Spannweite des Leitwerks.\r
-FinSetConfig.lbl.Tabposition = Position:\r
-FinSetConfig.ttip.Tabposition = Position des Leitwerks.\r
-FinSetConfig.lbl.relativeto = relativ zu\r
-\r
-! MotorDatabaseLoadingDialog\r
-MotorDbLoadDlg.title = Lade Motoren\r
-MotorDbLoadDlg.Loadingmotors = Lade Motoren...\r
-\r
-! RocketConfig\r
-RocketCfg.lbl.Designname = Name der Rakete:\r
-RocketCfg.lbl.Designer = Ersteller:\r
-RocketCfg.lbl.Comments = Kommentare:\r
-RocketCfg.lbl.Revisionhistory = Versionsgeschichte:\r
-RocketCfg.lbl.Material = Material:\r
-\r
-! ShockCordConfig\r
-ShockCordCfg.lbl.Shockcordlength = Gummibandlänge\r
-\r
-! RocketComponentConfig\r
-RocketCompCfg.lbl.Componentname = Komponentenname:\r
-RocketCompCfg.ttip.Thecomponentname = Name der Komponente.\r
-RocketCompCfg.tab.Override = Werte überschreiben\r
-RocketCompCfg.tab.MassandCGoverride = Massen- und Schwerpunktsoptionen\r
-RocketCompCfg.tab.Figure = Form\r
-RocketCompCfg.tab.Figstyleopt = Formoptionen\r
-RocketCompCfg.tab.Comment = Kommentar\r
-RocketCompCfg.tab.Specifyacomment = Kommentar zu dieser Komponente\r
-RocketCompCfg.lbl.Mass = Masse:\r
-RocketCompCfg.lbl.Componentmass = Masse der Komponente:\r
-RocketCompCfg.lbl.overriddento = (überschrieben auf\r
-RocketCompCfg.lbl.overriddenby = (überschrieben durch\r
-RocketCompCfg.lbl.Componentmaterial = Material:\r
-RocketCompCfg.lbl.Componentfinish = Oberfläche:\r
-RocketCompCfg.lbl.ttip.componentmaterialaffects = Das Material beeinflusst die Masse der Komponente.\r
-RocketCompCfg.combo.ttip.componentmaterialaffects = Das Material beeinflusst die Masse der Komponente.\r
-RocketCompCfg.lbl.longA1 = <html>Die Oberfläche beeinflusst den aerodynamischen Widerstand der Komponente.<br>\r
-RocketCompCfg.lbl.longA2 = Der angegebene Wert ist die durchschnittliche Rautiefe der Oberfläche.\r
-RocketCompCfg.but.Setforall = Für alle setzen\r
-RocketCompCfg.but.ttip.Setforall = Diese Oberflächen für alle Komponenten der Rakete setzen.\r
-RocketCompCfg.lbl.Overridemassorcenter = Überschreiben von Masse oder Schwerpunkts von \r
-RocketCompCfg.checkbox.Overridemass = Masse überschreiben:\r
-RocketCompCfg.checkbox.Overridecenterofgrav = Schwerpunkt überschreiben:\r
-RocketCompCfg.checkbox.OverridemassandCG = Masse und Schwerpunkt für alle Unterkomponenten überschreiben\r
-RocketCompCfg.lbl.longB1 = <html>Die überschriebene Masse enthält keine Motoren.<br>\r
-RocketCompCfg.lbl.longB2 = Die Messung des Schwerpunktes beginnt am Ende von\r
-RocketCompCfg.lbl.Commentsonthe = Kommentare zu\r
-RocketCompCfg.lbl.Figurestyle = Form:\r
-RocketCompCfg.lbl.Componentcolor = Farbe:\r
-RocketCompCfg.lbl.Choosecolor = Farbe auswählen\r
-RocketCompCfg.checkbox.Usedefaultcolor = Standardfarbe verwenden\r
-RocketCompCfg.lbl.Complinestyle = Linienstil:\r
-RocketCompCfg.but.Saveasdefstyle = Als Standardstil speichern\r
-RocketCompCfg.lbl.Diameter = Durchmesser:\r
-RocketCompCfg.lbl.Length = Länge:\r
-RocketCompCfg.lbl.Thickness = Wandstärke:\r
-RocketCompCfg.checkbox.Endcapped = Verschlossenes Ende\r
-RocketCompCfg.ttip.Endcapped = Gibt an, ob das Ende der Schulter geschlossen ist.\r
-RocketCompCfg.title.Noseconeshoulder = Spitzenschulter\r
-RocketCompCfg.title.Aftshoulder = Schulter hinten\r
-RocketCompCfg.border.Foreshoulder = Schulter vorn\r
-!RocketCompCfg.lbl.Length = Length:\r
-\r
-! BulkheadConfig\r
-BulkheadCfg.tab.Radius = Radius:\r
-BulkheadCfg.tab.Thickness = Wandstärke:\r
-BulkheadCfg.tab.General = Allgemein\r
-BulkheadCfg.tab.Generalproperties = Allgemeine Eigenschaften\r
-\r
-!CenteringRingConfig\r
-CenteringRingCfg.tab.Outerdiam = Außendurchmesser:\r
-CenteringRingCfg.tab.Innerdiam = Innendurchmesser:\r
-CenteringRingCfg.tab.Thickness = Wandstärke:\r
-CenteringRingCfg.tab.General = Allgemein\r
-CenteringRingCfg.tab.Generalproperties = Allgemeine Eigenschaften\r
-\r
-!ComponentConfigDialog\r
-ComponentCfgDlg.configuration = Konfiguration\r
-ComponentCfgDlg.configuration1 =\r
-ComponentCfgDlg.Modify = Verändern\r
-\r
-!EllipticalFinSetConfig\r
-EllipticalFinSetCfg.Nbroffins = Anzahl der Leitwerke\r
-EllipticalFinSetCfg.Rotation = Rotation:\r
-EllipticalFinSetCfg.Fincant = Neigung:\r
-EllipticalFinSetCfg.Rootchord = Blatttiefe:\r
-EllipticalFinSetCfg.Height = Höhe:\r
-EllipticalFinSetCfg.Positionrelativeto = Position relativ zu:\r
-EllipticalFinSetCfg.plus = plus\r
-EllipticalFinSetCfg.FincrossSection = Querschnitt:\r
-EllipticalFinSetCfg.Thickness = Wandstärke:\r
-EllipticalFinSetCfg.General = Allgemein\r
-EllipticalFinSetCfg.Generalproperties = Allgemeine Eigenschaften\r
-EllipticalFinSetCfg.ttip.Fincant = Der Winkel, in dem die Leitwerke zum Körperrohr geneigt sind.\r
-\r
-!FreeformFinSetConfig\r
-FreeformFinSetCfg.tab.General = Allgemein\r
-FreeformFinSetCfg.tab.ttip.General = Allgemeine Eigenschaften\r
-FreeformFinSetCfg.tab.Shape = Form\r
-FreeformFinSetCfg.tab.ttip.Finshape = Leitwerksform\r
-FreeformFinSetCfg.lbl.Numberoffins = Anzahl der Leitwerke\r
-FreeformFinSetCfg.lbl.Finrotation = Rotation:\r
-FreeformFinSetCfg.lbl.Fincant = Neigung:\r
-FreeformFinSetCfg.lbl.ttip.Fincant = Der Winkel, in dem die Leitwerke zum Körperrohr geneigt sind.\r
-FreeformFinSetCfg.lbl.Posrelativeto = Position relativ zu:\r
-FreeformFinSetCfg.lbl.plus = plus\r
-FreeformFinSetCfg.lbl.FincrossSection = Querschnitt:\r
-FreeformFinSetCfg.lbl.Thickness = Wandstärke:\r
-! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle\r
-FreeformFinSetConfig.lbl.doubleClick1 = Double-click\r
-FreeformFinSetConfig.lbl.doubleClick2 = to edit\r
-FreeformFinSetConfig.lbl.clickDrag = Click+drag: Add and move points\r
-FreeformFinSetConfig.lbl.ctrlClick = Ctrl+click: Remove point\r
-\r
-\r
-!InnerTubeConfig\r
-InnerTubeCfg.tab.Motor = Motor\r
-InnerTubeCfg.tab.ttip.Motor = Motorkonfiguration\r
-InnerTubeCfg.tab.Cluster = Cluster\r
-InnerTubeCfg.tab.ttip.Cluster = Cluster-Konfiguration\r
-InnerTubeCfg.tab.Radialpos = Radiale Position\r
-InnerTubeCfg.tab.ttip.Radialpos = Radiale Position\r
-InnerTubeCfg.lbl.Selectclustercfg = Cluster-Konfiguration auswählen:\r
-InnerTubeCfg.lbl.TubeSep = Rohrtrennung\r
-InnerTubeCfg.lbl.ttip.TubeSep = Die Trennung der Rohre, 1.0 = die Rohre berühren sich\r
-InnerTubeCfg.lbl.Rotation = Rotation:\r
-InnerTubeCfg.lbl.ttip.Rotation = Rotationswinkel der Cluster-Konfiguration\r
-InnerTubeCfg.lbl.Rotangle = Rotationswinkel der Cluster-Konfiguration\r
-InnerTubeCfg.but.Splitcluster = Cluster aufteilen\r
-InnerTubeCfg.lbl.longA1 = <html>Den Cluster in einzelne Komponenten aufteilen.<br>\r
-InnerTubeCfg.lbl.longA2 = Die dupliziert alle Komponenten innerhalb dieses Innenrohrs.\r
-InnerTubeCfg.but.Resetsettings = Einstellungen zurücksetzen\r
-InnerTubeCfg.but.ttip.Resetsettings = Setzt die Aufteilung und Rotation auf die Standardwerte zurück\r
-\r
-! LaunchLugConfig\r
-LaunchLugCfg.lbl.Length = Länge:\r
-LaunchLugCfg.lbl.Outerdiam = Außendurchmesser:\r
-LaunchLugCfg.lbl.Innerdiam = Innendurchmesser:\r
-LaunchLugCfg.lbl.Thickness = Wandstärke:\r
-LaunchLugCfg.lbl.Radialpos = Radiale Position:\r
-LaunchLugCfg.lbl.Posrelativeto = Position relativ zu:\r
-LaunchLugCfg.lbl.plus = plus\r
-LaunchLugCfg.tab.General = Allgemein\r
-LaunchLugCfg.tab.Generalprop = Allgemeine Eigenschaften\r
-\r
-! MassComponentConfig\r
-MassComponentCfg.lbl.Mass = Masse\r
-MassComponentCfg.lbl.Length = Länge\r
-MassComponentCfg.lbl.Diameter = Durchmesser\r
-MassComponentCfg.lbl.PosRelativeto = Position relativ zu:\r
-MassComponentCfg.lbl.plus = plus\r
-MassComponentCfg.tab.General = Allgemein\r
-MassComponentCfg.tab.ttip.General = Allgemeine Eigenschaften\r
-MassComponentCfg.tab.Radialpos = Radiale Position\r
-MassComponentCfg.tab.ttip.Radialpos = Konfiguration der radialen Position\r
-MassComponentCfg.lbl.Radialdistance = Radialer Abstand:\r
-MassComponentCfg.lbl.Radialdirection = radiale Richtung:\r
-MassComponentCfg.but.Reset = Zurücksetzen\r
-\r
-! MotorConfig\r
-MotorCfg.checkbox.compmotormount = Diese Komponente ist eine Motorhalterung\r
-MotorCfg.lbl.Motorcfg = Motorkonfiguration\r
-MotorCfg.but.New = Neu\r
-MotorCfg.lbl.Currentmotor = Aktueller Motor:\r
-MotorCfg.lbl.Motoroverhang = Motorüberstand:\r
-MotorCfg.lbl.Ignitionat = Zündung bei:\r
-MotorCfg.lbl.plus = plus\r
-MotorCfg.lbl.seconds = Sekunden\r
-MotorCfg.lbl.longA1 = Das aktuelle Design hat im Moment nur eine Stufe.\r
-MotorCfg.lbl.longA2 = Stufen können durch Klicken auf \«Neue Stufe\« hinzugefügt werden.\r
-MotorCfg.lbl.longB1 = Das aktuelle Design hat im Moment nur eine Stufe.\r
-MotorCfg.lbl.longB2 = Stufen.\r
-MotorCfg.but.Selectmotor = Motor auswählen\r
-MotorCfg.but.Removemotor = Motor entfernen\r
-MotorCfg.lbl.motorLabel = Keiner\r
-\r
-! NoseConeConfig\r
-NoseConeCfg.lbl.Noseconeshape = Spitzenform:\r
-NoseConeCfg.lbl.Shapeparam = Formparameter:\r
-NoseConeCfg.lbl.Noseconelength = Spitzenlänge:\r
-NoseConeCfg.lbl.Basediam = Basisdurchmesser:\r
-NoseConeCfg.checkbox.Automatic = Automatisch\r
-NoseConeCfg.lbl.Wallthickness = Wandstärke:\r
-NoseConeCfg.checkbox.Filled = gefüllt\r
-NoseConeCfg.tab.General = Allgemein\r
-NoseConeCfg.tab.ttip.General = Allgemeine Eigenschaften\r
-NoseConeCfg.tab.Shoulder = Schulter\r
-NoseConeCfg.tab.ttip.Shoulder = Schultereigenschaften\r
-\r
-! ParachuteConfig\r
-ParachuteCfg.lbl.Canopy = Fallschirmkappe:\r
-ParachuteCfg.lbl.Diameter = Durchmesser:\r
-ParachuteCfg.lbl.Material = Material:\r
-ParachuteCfg.combo.MaterialModel = Das Material beeinflusst die Masse der Komponente.\r
-ParachuteCfg.lbl.longA1 = <html>Luftwiderstandskoeffizient C<sub>D</sub>:\r
-ParachuteCfg.lbl.longB1 = <html>Der Luftwiderstandsbeiwert relativ zur Gesamtfläche des Fallschirms.<br>\r
-ParachuteCfg.lbl.longB2 = Ein größerer Luftwiderstand führt zu einer kleineren Sinkrate.\r
-ParachuteCfg.lbl.longB3 = Ein typischer Wert für Fallschirme ist 0,8.\r
-ParachuteCfg.but.Reset = Zurücksetzen\r
-ParachuteCfg.lbl.Shroudlines = Fangleinen:\r
-ParachuteCfg.lbl.Numberoflines = Anzahl der Leinen:\r
-ParachuteCfg.lbl.Linelength = Länge der Leinen:\r
-ParachuteCfg.lbl.Material = Material:\r
-ParachuteCfg.lbl.Posrelativeto = Position relativ zu:\r
-ParachuteCfg.lbl.plus = plus\r
-ParachuteCfg.lbl.Packedlength = gepackte Länge:\r
-ParachuteCfg.lbl.Packeddiam = gepackter Durchmesser:\r
-ParachuteCfg.lbl.Deploysat = Auswurf bei\r
-ParachuteCfg.lbl.seconds = Sekunden\r
-ParachuteCfg.lbl.Altitude = Höhe:\r
-ParachuteCfg.tab.General = Allgemein\r
-ParachuteCfg.tab.ttip.General = Allgemeine Eigenschaften\r
-ParachuteCfg.tab.Radialpos = Radiale Position\r
-ParachuteCfg.tab.ttip.Radialpos = Konfiguration der radialen Position\r
-ParachuteCfg.lbl.Radialdistance = Radialer Abstand:\r
-ParachuteCfg.lbl.Radialdirection = radiale Richtung:\r
-ParachuteCfg.but.Reset = Zurücksetzen\r
-ParachuteCfg.lbl.plusdelay = plus\r
-\r
-! ShockCordConfig \r
-ShockCordCfg.lbl.Shockcordlength = Länge des Gummibands\r
-ShockCordCfg.lbl.Shockcordmaterial = Material des Gummibands:\r
-ShockCordCfg.lbl.Posrelativeto = Position relativ zu:\r
-ShockCordCfg.lbl.plus = plus\r
-ShockCordCfg.lbl.Packedlength = gepackte Länge:\r
-ShockCordCfg.lbl.Packeddiam = gepackter Durchmesser:\r
-ShockCordCfg.tab.General = Allgemein\r
-ShockCordCfg.tab.ttip.General = Allgemeine Eigenschaften\r
-\r
-!SleeveConfig\r
-SleeveCfg.tab.Outerdiam = Außendurchmesser:\r
-SleeveCfg.tab.Innerdiam = Innendurchmesser:\r
-SleeveCfg.tab.Wallthickness = Wandstärke:\r
-SleeveCfg.tab.Length = Länge:\r
-SleeveCfg.tab.General = Allgemein\r
-SleeveCfg.tab.Generalproperties = Allgemeine Eigenschaften\r
-\r
-! StreamerConfig\r
-StreamerCfg.lbl.Striplength = Länge des Strömers:\r
-StreamerCfg.lbl.Stripwidth = Breite des Strömers:\r
-StreamerCfg.lbl.Striparea = Fläche des Strömers:\r
-StreamerCfg.lbl.Aspectratio = Seitenverhältnis:\r
-StreamerCfg.lbl.Material = Material:\r
-StreamerCfg.combo.ttip.MaterialModel = Das Material beeinflusst die Masse der Komponente.\r
-StreamerCfg.lbl.longA1 = <html>Widerstandskoeffizient C<sub>D</sub>:\r
-StreamerCfg.lbl.longB1 = <html>Der Widerstandskoeffizient des Strömers hängt von der Gesamtfläche ab.<br>\r
-StreamerCfg.lbl.longB2 = Ein größerer Luftwiderstandskoeffizient führt zu einer kleineren Sinkrate.\r
-StreamerCfg.lbl.Automatic = Automatisch\r
-StreamerCfg.lbl.longC1 = Der Luftwiderstandskoeffizient hängt von der Fläche des Strömers ab.\r
-StreamerCfg.lbl.Posrelativeto = Position relativ zu:\r
-StreamerCfg.lbl.plus = plus\r
-StreamerCfg.lbl.Packedlength = gepackte Länge:\r
-StreamerCfg.lbl.Packeddiam = gepackter Durchmesser:\r
-StreamerCfg.lbl.Deploysat = Auswurf bei\r
-StreamerCfg.lbl.seconds = Sekunden\r
-StreamerCfg.lbl.Altitude = Höhe:\r
-StreamerCfg.tab.General = Allgemein\r
-StreamerCfg.tab.ttip.General = Allgemeine Eigenschaften\r
-StreamerCfg.tab.Radialpos = Radiale Position\r
-StreamerCfg.tab.ttip.Radialpos = Konfiguration der radialen Position\r
-StreamerCfg.lbl.Radialdistance = Radialer Abstand:\r
-StreamerCfg.lbl.Radialdirection = radiale Richtung:\r
-StreamerCfg.but.Reset = Zurücksetzen\r
-StreamerCfg.lbl.plusdelay = plus\r
-\r
-! ThicknessRingComponentConfig\r
-ThicknessRingCompCfg.tab.Outerdiam = Außendurchmesser:\r
-ThicknessRingCompCfg.tab.Innerdiam = Innendurchmesser:\r
-ThicknessRingCompCfg.tab.Wallthickness = Wandstärke:\r
-ThicknessRingCompCfg.tab.Length = Länge:\r
-ThicknessRingCompCfg.tab.General = Allgemein\r
-ThicknessRingCompCfg.tab.Generalprop = Allgemeine Eigenschaften\r
-\r
-! TransitionConfig\r
-TransitionCfg.lbl.Transitionshape = Form des Übergangs\r
-TransitionCfg.checkbox.Clipped = geklemmt\r
-TransitionCfg.lbl.Shapeparam = Formparameter:\r
-TransitionCfg.lbl.Transitionlength = Länge des Übergangs:\r
-TransitionCfg.lbl.Forediam = Vorderer Durchmesser\r
-TransitionCfg.checkbox.Automatic = Automatisch\r
-TransitionCfg.lbl.Aftdiam = Hinterer Durchmesser\r
-TransitionCfg.lbl.Wallthickness = Wandstärke:\r
-TransitionCfg.checkbox.Filled = gefüllt\r
-TransitionCfg.tab.General = Allgemein\r
-TransitionCfg.tab.Generalproperties = Allgemeine Eigenschaften\r
-TransitionCfg.tab.Shoulder = Schulter\r
-TransitionCfg.tab.Shoulderproperties = Schultereigenschaften\r
-\r
-! TrapezoidFinSetConfig\r
-TrapezoidFinSetCfg.lbl.Nbroffins = Anzahl der Leitwerke\r
-TrapezoidFinSetCfg.lbl.ttip.Nbroffins = Anzahl der Leitwerke in diesem Satz\r
-TrapezoidFinSetCfg.lbl.Finrotation = Rotation der Leitwerke\r
-TrapezoidFinSetCfg.lbl.ttip.Finrotation = Winkel des ersten Leitwerks in diesem Satz\r
-TrapezoidFinSetCfg.lbl.Fincant = Neigung:\r
-TrapezoidFinSetCfg.lbl.ttip.Fincant = Der Winkel, in dem die Leitwerke zum Körperrohr geneigt sind.\r
-TrapezoidFinSetCfg.lbl.Rootchord = Blatttiefe:\r
-TrapezoidFinSetCfg.lbl.Tipchord = Blatttiefe (Spitze)\r
-TrapezoidFinSetCfg.lbl.Height = Höhe:\r
-TrapezoidFinSetCfg.lbl.Sweeplength = Blattbreite:\r
-TrapezoidFinSetCfg.lbl.Sweepangle = Pfeilungswinkel\r
-TrapezoidFinSetCfg.lbl.FincrossSection = Leitwerksquerschnitt\r
-TrapezoidFinSetCfg.lbl.Thickness = Wandstärke:\r
-TrapezoidFinSetCfg.lbl.Posrelativeto = Position relativ zu:\r
-TrapezoidFinSetCfg.lbl.plus = plus\r
-TrapezoidFinSetCfg.tab.General = Allgemein\r
-TrapezoidFinSetCfg.tab.Generalproperties = Allgemeine Eigenschaften\r
-\r
-!MotorConfigurationModel\r
-MotorCfgModel.Editcfg = Konfiguration bearbeiten\r
-\r
-! StorageOptionChooser\r
-StorageOptChooser.lbl.Simdatatostore = Zu speichernde Simulationsdaten:\r
-StorageOptChooser.rdbut.Allsimdata = Alle Simulationsdaten\r
-StorageOptChooser.lbl.longA1 = <html>Speichert alle Simulationsdaten.<br>\r
-StorageOptChooser.lbl.longA2 = Dies kann sehr große Dateien erzeugen!\r
-StorageOptChooser.rdbut.Every = Alle Simulationsdaten\r
-StorageOptChooser.lbl.longB1 = <html>Speicher plotbare Daten in etwa diesem Abstand.<br>\r
-StorageOptChooser.lbl.longB2 = Größere Werte erzeugen kleinere Dateien.\r
-StorageOptChooser.lbl.seconds = Sekunden\r
-StorageOptChooser.rdbut.Onlyprimfig = Nur die wichtigsten Werte\r
-StorageOptChooser.lbl.longC1 = <html>Speichert nur die Werte, die in der Zusammenfassung stehen.<br>\r
-StorageOptChooser.lbl.longC2 = Dies ergibt die kleinsten Dateien\r
-StorageOptChooser.checkbox.Compfile = Datei komprimieren\r
-StorageOptChooser.lbl.UsingComp = Kompression der Datei verringert die Größe signifikant.\r
-StorageOptChooser.lbl.longD1 = Eine Schätzung der Dateigröße mit den gegebenen Optionen.\r
-StorageOptChooser.ttip.Saveopt = Speicheroptionen\r
-StorageOptChooser.lbl.Estfilesize = Voraussichtliche Dateigröße:\r
-StorageOptChooser.lbl.Saveopt = Speicheroptionen\r
-\r
-! ThrustCurveMotorSelectionPanel\r
-TCMotorSelPan.lbl.Selrocketmotor = Raketenmotor auswählen:\r
-TCMotorSelPan.checkbox.hideSimilar = Ähnliche Schubkurven verbergen\r
-TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Alle Motoren anzeigen\r
-TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Motoren anzeigen, deren Durchmesser kleiner als der der Motorhalterung ist\r
-TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Motoren anzeigen, deren Durchmesser gleich der der Motorhalterung ist\r
-TCMotorSelPan.lbl.Motormountdia = Durchmesser der Motorhalterung\r
-TCMotorSelPan.lbl.Search = Suchen:\r
-TCMotorSelPan.lbl.Selectthrustcurve = Schubkurve auswählen:\r
-TCMotorSelPan.lbl.Ejectionchargedelay = Verzögerung der Ausstoßladung:\r
-TCMotorSelPan.equalsIgnoreCase.None = keine\r
-TCMotorSelPan.lbl.NumberofsecondsorNone = (Anzahl der Sekunden oder \«keine\«)\r
-TCMotorSelPan.lbl.Totalimpulse = Gesamtimpuls:\r
-TCMotorSelPan.lbl.Avgthrust = Durchschn. Schub:\r
-TCMotorSelPan.lbl.Maxthrust = max. Schub\r
-TCMotorSelPan.lbl.Burntime = Brenndauer:\r
-TCMotorSelPan.lbl.Launchmass = Startmasse:\r
-TCMotorSelPan.lbl.Emptymass = Leermasse:\r
-TCMotorSelPan.lbl.Datapoints = Datenpunkte:\r
-TCMotorSelPan.lbl.Digest = Übersicht:\r
-TCMotorSelPan.title.Thrustcurve = Schubkurve:\r
-TCMotorSelPan.title.Thrust = Schub:\r
-TCMotorSelPan.delayBox.None = keine\r
-\r
-\r
-! PlotDialog\r
-PlotDialog.title.Flightdataplot = Flugdatenplot\r
-PlotDialog.Chart.Simulatedflight = Simulierter Flug\r
-PlotDialog.CheckBox.Showdatapoints = Datenpunkte anzeigen\r
-PlotDialog.lbl.Chart = Klicken+ziehen: runter+rechts um hinein zu zoomen, hoch+links um heraus zu zoomen \r
-\r
-\r
-! "main" prefix is used for the main application dialog\r
-\r
-# FIXME: Rename the description keys \r
-\r
-main.menu.file = Datei\r
-main.menu.file.desc = File-handling related tasks\r
-main.menu.file.new = Neu\r
-main.menu.file.new.desc = Create a new rocket design\r
-main.menu.file.open = Öffnen..\r
-BasicFrame.item.Openrocketdesign = Raketendesign öffnen\r
-main.menu.file.openExample = Beispiel öffnen..\r
-BasicFrame.item.Openexamplerocketdesign = Beispieldesign öffnen\r
-main.menu.file.save = Speichern\r
-BasicFrame.item.SavecurRocketdesign = Aktuelles Raketendesign speichern\r
-main.menu.file.saveAs = Speichern unter...\r
-BasicFrame.item.SavecurRocketdesnewfile = Aktuelles Raketendesign in eine neue Datei speichern\r
-main.menu.file.print = Drucken / als PDF exportieren...\r
-BasicFrame.item.Printpart = Komponentenliste und Leitwerkschablone drucken\r
-main.menu.file.close = Schließen\r
-BasicFrame.item.Closedesign = Aktuelles Raketendesign schließen\r
-main.menu.file.quit = Beenden\r
-BasicFrame.item.Quitprogram = Programm beenden\r
-\r
-main.menu.edit = Bearbeiten\r
-BasicFrame.menu.Rocketedt = Rakete bearbeiten\r
-main.menu.edit.undo = Rückgängig\r
-main.menu.edit.undo.desc = Undo the previous operation\r
-main.menu.edit.redo = Wiederholen\r
-main.menu.edit.redo.desc = Redo the previously undone operation\r
-main.menu.edit.cut = Ausschneiden\r
-main.menu.edit.copy = Kopieren\r
-main.menu.edit.paste = Einfügen\r
-main.menu.edit.delete = Löschen\r
-main.menu.edit.resize = Scale...\r
-main.menu.edit.resize.desc = Scale parts of the rocket design\r
-main.menu.edit.preferences = Einstellungen\r
-main.menu.edit.preferences.desc = Setup the application preferences\r
-\r
-main.menu.analyze = Analysieren\r
-main.menu.analyze.desc = Rocket analysis\r
-main.menu.analyze.componentAnalysis = Komponente analysieren\r
-main.menu.analyze.componentAnalysis.desc = Analyze the rocket components separately\r
-main.menu.analyze.optimization = Rocket optimization\r
-main.menu.analyze.optimization.desc = General rocket design optimization\r
-\r
-main.menu.help = Hilfe\r
-main.menu.help.desc = Information about OpenRocket\r
-main.menu.help.license = Lizenz\r
-main.menu.help.license.desc = OpenRocket license information\r
-main.menu.help.bugReport = Fehlerbericht\r
-main.menu.help.bugReport.desc = Information about reporting bugs in OpenRocket\r
-main.menu.help.debugLog = Debug-Log\r
-main.menu.help.debugLog.desc = View the OpenRocket debug log\r
-main.menu.help.about = Über\r
-main.menu.help.about.desc = Copyright details about OpenRocket\r
-\r
-main.menu.debug = Debug\r
-main.menu.debug.whatisthismenu = Was macht diese Menü?\r
-main.menu.debug.createtestrocket = Eine Testrakete erstellen\r
-\r
-! database\r
-! Translate here all material database\r
-!\r
-\r
-! Material database\r
-! BULK_MATERIAL\r
-Databases.materials.Acrylic = Acryl\r
-Databases.materials.Balsa = Balsa\r
-Databases.materials.Birch = Birke\r
-Databases.materials.Cardboard = Karton\r
-Databases.materials.Carbonfiber = Kohlefaser\r
-Databases.materials.Cork = Kork\r
-Databases.materials.DepronXPS = Depron (XPS)\r
-Databases.materials.Fiberglass = Glasfaser\r
-Databases.materials.Kraftphenolic = Pertinax\r
-Databases.materials.Maple = Ahorn\r
-Databases.materials.Paperoffice = Papier (Büro)\r
-Databases.materials.Pine = Kiefer\r
-Databases.materials.Plywoodbirch = Sperrholz (Birke)\r
-Databases.materials.PolycarbonateLexan = Polycarbonat (Lexan)\r
-Databases.materials.Polystyrene = Polystyrène\r
-Databases.materials.PVC = PVC\r
-Databases.materials.Spruce = Fichte\r
-Databases.materials.StyrofoamgenericEPS = Styropor (EPS)\r
-Databases.materials.StyrofoamBluefoamXPS = Styrodur (XPS)\r
-Databases.materials.Quantumtubing = Quantum tubing\r
-Databases.materials.BlueTube = Blue tube\r
-!SURFACE_MATERIAL\r
-Databases.materials.Ripstopnylon = Ripstop Nylon\r
-Databases.materials.Mylar = Mylar\r
-Databases.materials.Polyethylenethin = Polyethylen (dünn)\r
-Databases.materials.Polyethyleneheavy = Polyethylen (schwer)\r
-Databases.materials.Silk = Seide\r
-Databases.materials.Paperoffice = Papier (Büro)\r
-Databases.materials.Cellophane = Zellophan\r
-Databases.materials.Crepepaper = Krepppapier\r
-! LINE_MATERIAL\r
-Databases.materials.Threadheavy-duty = Faden (stark)\r
-Databases.materials.Elasticcordround2mm = Elastikband (rund, 2mm, 1/16 in)\r
-Databases.materials.Elasticcordflat6mm = Elastikband (flach, 6mm, 1/4 in)\r
-Databases.materials.Elasticcordflat12mm = Elastikband (flach, 12mm, 1/2 in)\r
-Databases.materials.Elasticcordflat19mm = Elastikband (flach, 19mm, 3/4 in)\r
-Databases.materials.Elasticcordflat25mm = Elastikband (flach, 25mm, 1 in)\r
-Databases.materials.Braidednylon2mm = Nylonflachband (2 mm, 1/16 in)\r
-Databases.materials.Braidednylon3mm = Nylonflachband (3 mm, 1/8 in)\r
-Databases.materials.Tubularnylon11mm = Tubular Nylon (11 mm, 7/16 in)\r
-Databases.materials.Tubularnylon14mm = Tubular Nylon (14 mm, 9/16 in)\r
-Databases.materials.Tubularnylon25mm = Tubular Nylon (25 mm, 1 in)\r
-\r
-! ExternalComponent\r
-ExternalComponent.Rough = Rau\r
-ExternalComponent.Unfinished = unbehandelt\r
-ExternalComponent.Regularpaint = normale Farbe\r
-ExternalComponent.Smoothpaint = glatte Farbe\r
-ExternalComponent.Polished = poliert\r
-\r
-! LineStyle\r
-LineStyle.Solid = durchgehend\r
-LineStyle.Dashed = gestrichelt\r
-LineStyle.Dotted = gepunktet\r
-LineStyle.Dash-dotted = Strich-Punkt\r
-LineStyle.Defaultstyle = Standardstil\r
-\r
-! Shape\r
-Shape.Conical = Konisch\r
-Shape.Conical.desc1 = Eine konische Spitze hat ein dreieckiges Profil\r
-Shape.Conical.desc2 = Ein konischer Übergang hat gerade Kanten\r
-Shape.Ogive = Ogive\r
-Shape.Ogive.desc1 = Eine ogive Spitze hat das Profil eines Kreissegments. Der Formparamter 1 erzeugt eine <b>tangentiale Ogive</b>, die einen weichen Übergang zum Körperrohr hat, Werte kleiner 1 erzeugen eine <b>sekante Ogive<b>.\r
-Shape.Ogive.desc2 = Eine ogive Spitze hat das Profil eines Kreissegments. Der Formparamter 1 erzeugt eine <b>tangentiale Ogive</b>, die einen weichen Übergang zum Körperrohr am hinteren Ende hat, Werte kleiner 1 erzeugen eine <b>sekante Ogive<b>.\r
-Shape.Ellipsoid = Ellipsoid\r
-Shape.Ellipsoid.desc1 = Eine ellipsoide Spitze hat ein Profil einer Halbellipse mit der einer Hauptachsenlänge von 2×<i>Länge</i> und <i>Durchmesser</i> \r
-Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>. If the transition is not clipped, then the profile is extended at the center by the corresponding radius. \r
-Shape.Powerseries = Power series\r
-Shape.Powerseries.desc1 = A power series nose cone has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 this is a <b>\u00BD-power</b> or <b>parabolic</b> nose cone, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 a <b>conical</b> nose cone.\r
-Shape.Powerseries.desc2 = A power series transition has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 the transition is <b>\u00BD-power</b> or <b>parabolic</b>, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 <b>conical</b>.\r
-Shape.Parabolicseries = Parabolic series\r
-Shape.Parabolicseries.desc1 = A parabolic series nose cone has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> nose cone.\r
-Shape.Parabolicseries.desc2 = A parabolic series transition has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube at the aft end, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> transition.\r
-Shape.Haackseries = Haack series\r
-Shape.Haackseries.desc1 = The Haack series nose cones are designed to minimize drag. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> nose cone, which minimizes drag for fixed length and diameter, while a value of 0.333 produces an <b>LV-Haack</b> nose cone, which minimizes drag for fixed length and volume.\r
-Shape.Haackseries.desc2 = The Haack series <i>nose cones</i> are designed to minimize drag. These transition shapes are their equivalents, but do not necessarily produce optimal drag for transitions. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> shape, while a value of 0.333 produces an <b>LV-Haack</b> shape. \r
-\r
-\r
-! RocketComponent\r
-RocketComponent.Position.TOP = oberes Ende der übergeordneten Komponente\r
-RocketComponent.Position.MIDDLE = Mitte der übergeordneten Komponente\r
-RocketComponent.Position.BOTTOM = unteres Ende der übergeordneten Komponente\r
-RocketComponent.Position.AFTER = nach der übergeordneten Komponente\r
-RocketComponent.Position.ABSOLUTE = zur Spitze\r
-\r
-! LaunchLug\r
-LaunchLug.Launchlug = Leitröhrchen\r
-! NoseCone\r
-NoseCone.NoseCone = Spitze\r
-! Transition\r
-Transition.Transition = Übergang\r
-!Stage\r
-Stage.Stage = Stufe\r
-! BodyTube\r
-BodyTube.BodyTube = Körperrohr\r
-! TubeCoupler\r
-TubeCoupler.TubeCoupler = Koppler\r
-!InnerTube\r
-InnerTube.InnerTube = Innenrohr\r
-! TrapezoidFinSet\r
-TrapezoidFinSet.TrapezoidFinSet = Trapezoide Leitwerke\r
-! FreeformFinSet\r
-FreeformFinSet.FreeformFinSet = Frei geformte Leitwerke\r
-!MassComponent\r
-MassComponent.MassComponent = Masse\r
-! Parachute\r
-Parachute.Parachute = Fallschirm\r
-! ShockCord\r
-ShockCord.ShockCord = Gummiband\r
-! Bulkhead\r
-Bulkhead.Bulkhead = Schott\r
-\r
-!Rocket\r
-Rocket.motorCount.Nomotor = [Keine Motoren]\r
-Rocket.compname.Rocket = Rakete\r
-\r
-!MotorMount\r
-MotorMount.IgnitionEvent.AUTOMATIC = Automatisch (Start oder Ausstoßladung)\r
-MotorMount.IgnitionEvent.LAUNCH = Start\r
-MotorMount.IgnitionEvent.EJECTION_CHARGE = Erste Ausstoßladung der vorherigen Stufe\r
-MotorMount.IgnitionEvent.BURNOUT = Erster Brennschluss der vorherigen Stufe\r
-MotorMount.IgnitionEvent.NEVER = Nie\r
-\r
-!ComponentIcons \r
-ComponentIcons.Nosecone = Spitze\r
-ComponentIcons.Bodytube = Körperrohr\r
-ComponentIcons.Transition = Übergang\r
-ComponentIcons.Trapezoidalfinset = Trapezoide Leitwerke\r
-ComponentIcons.Ellipticalfinset = Elliptische Leitwerke\r
-ComponentIcons.Freeformfinset = Frei geformte Leitwerke\r
-ComponentIcons.Launchlug = Leitröhrchen\r
-ComponentIcons.Innertube = Innenrohr\r
-ComponentIcons.Tubecoupler = Koppler\r
-ComponentIcons.Centeringring = Zentrierring\r
-ComponentIcons.Bulkhead = Schott\r
-ComponentIcons.Engineblock = Motorhalterung\r
-ComponentIcons.Parachute = Fallschirm\r
-ComponentIcons.Streamer = Strömer\r
-ComponentIcons.Shockcord = Gummiband\r
-ComponentIcons.Masscomponent = Masse\r
-ComponentIcons.disabled = (deaktiviert)\r
-\r
-! StageAction\r
-StageAction.Stage = Stufe\r
-\r
-! RecoveryDevice\r
-RecoveryDevice.DeployEvent.LAUNCH = Start (plus NN Sekunden)\r
-RecoveryDevice.DeployEvent.EJECTION = Erste Ausstoßladung dieser Stufe\r
-RecoveryDevice.DeployEvent.APOGEE = Apogäum\r
-RecoveryDevice.DeployEvent.ALTITUDE = Spezifische Höhe während der Landephase\r
-RecoveryDevice.DeployEvent.NEVER = Nie\r
-\r
-! FlightEvent\r
-FlightEvent.Type.LAUNCH = Start\r
-FlightEvent.Type.IGNITION = Motorzündung\r
-FlightEvent.Type.LIFTOFF = Abheben\r
-FlightEvent.Type.LAUNCHROD = Verlassen der Startrampe\r
-FlightEvent.Type.BURNOUT = Motorbrennschluss\r
-FlightEvent.Type.EJECTION_CHARGE = Ausstoßladung\r
-FlightEvent.Type.STAGE_SEPARATION = Stufentrennung\r
-FlightEvent.Type.APOGEE = Apogäum\r
-FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Auslösung des Bergungssystems\r
-FlightEvent.Type.GROUND_HIT = Landung\r
-FlightEvent.Type.SIMULATION_END = Ende der Simulation\r
-FlightEvent.Type.ALTITUDE = Höhenänderung\r
-\r
-! ThrustCurveMotorColumns\r
-TCurveMotorCol.MANUFACTURER = Hersteller\r
-TCurveMotorCol.DESIGNATION = Bezeichnung\r
-TCurveMotorCol.TYPE = Typ\r
-TCurveMotorCol.DIAMETER = Durchmesser\r
-TCurveMotorCol.LENGTH = Länge\r
-\r
-! RocketInfo\r
-RocketInfo.lengthLine.Length = Länge\r
-RocketInfo.lengthLine.maxdiameter = , max. Durchmesser\r
-RocketInfo.massText1 = Masse mit Motoren\r
-RocketInfo.massText2 = Masse ohne Motoren\r
-RocketInfo.at = bei M=\r
-RocketInfo.cgText = CG:\r
-RocketInfo.cpText = CP:\r
-RocketInfo.stabText = Stabilität:\r
-RocketInfo.Warning = Warnung:\r
-RocketInfo.Calculating = Berechne...\r
-RocketInfo.Apogee = Apogäum:\r
-RocketInfo.Maxvelocity = max. Geschwindigkeit:\r
-RocketInfo.Maxacceleration = max. Beschleunigung:\r
-RocketInfo.apogeeValue = N/A\r
-RocketInfo.Mach = (Mach\r
-RocketInfo.velocityValue = N/A\r
-RocketInfo.accelerationValue = N/A\r
-\r
-! FinSet\r
-FinSet.CrossSection.SQUARE = Quadrat\r
-FinSet.CrossSection.ROUNDED = Abgerundet\r
-FinSet.CrossSection.AIRFOIL = Tragfläche\r
-FinSet.TabRelativePosition.FRONT = Root chord leading edge\r
-FinSet.TabRelativePosition.CENTER = Root chord midpoint\r
-FinSet.TabRelativePosition.END = Root chord trailing edge\r
-\r
-! FlightDataType\r
-FlightDataType.TYPE_TIME = Zeit\r
-FlightDataType.TYPE_ALTITUDE = Höhe\r
-FlightDataType.TYPE_VELOCITY_Z = Vertikalgeschwindigkeit\r
-FlightDataType.TYPE_ACCELERATION_Z = Vertikalbeschleunigung\r
-FlightDataType.TYPE_VELOCITY_TOTAL = Gesamtgeschwindigkeit\r
-FlightDataType.TYPE_ACCELERATION_TOTAL = Gesamtbeschleunigung\r
-FlightDataType.TYPE_POSITION_X = Position upwind\r
-FlightDataType.TYPE_POSITION_Y = Position parallel to wind\r
-FlightDataType.TYPE_POSITION_XY = Lateral distance\r
-FlightDataType.TYPE_POSITION_DIRECTION = Lateral direction\r
-FlightDataType.TYPE_VELOCITY_XY = Lateral velocity\r
-FlightDataType.TYPE_ACCELERATION_XY = Lateral acceleration\r
-FlightDataType.TYPE_AOA = Angriffswinkel\r
-FlightDataType.TYPE_ROLL_RATE = Rollrate\r
-FlightDataType.TYPE_PITCH_RATE = Nickrate\r
-FlightDataType.TYPE_YAW_RATE = Gierrate\r
-FlightDataType.TYPE_MASS = Masse\r
-FlightDataType.TYPE_LONGITUDINAL_INERTIA = Longitudinal moment of inertia\r
-FlightDataType.TYPE_ROTATIONAL_INERTIA = Rotational moment of inertia\r
-FlightDataType.TYPE_CP_LOCATION = Position vom CP\r
-FlightDataType.TYPE_CG_LOCATION = Position vom CG\r
-FlightDataType.TYPE_STABILITY = Stabilität in Kalibern\r
-FlightDataType.TYPE_MACH_NUMBER = Machzahl\r
-FlightDataType.TYPE_REYNOLDS_NUMBER = Reynoldszahl\r
-FlightDataType.TYPE_THRUST_FORCE = Schub\r
-FlightDataType.TYPE_DRAG_FORCE = Luftwiderstandskraft\r
-FlightDataType.TYPE_DRAG_COEFF = Luftwiderstandskoeffizient\r
-FlightDataType.TYPE_AXIAL_DRAG_COEFF = Axial drag coefficient\r
-FlightDataType.TYPE_FRICTION_DRAG_COEFF = Reibungskoeffizient\r
-FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Pressure drag coefficient\r
-FlightDataType.TYPE_BASE_DRAG_COEFF = Base drag coefficient\r
-FlightDataType.TYPE_NORMAL_FORCE_COEFF = Normal force coefficient\r
-FlightDataType.TYPE_PITCH_MOMENT_COEFF = Pitch moment coefficient\r
-FlightDataType.TYPE_YAW_MOMENT_COEFF = Yaw moment coefficient\r
-FlightDataType.TYPE_SIDE_FORCE_COEFF = Side force coefficient\r
-FlightDataType.TYPE_ROLL_MOMENT_COEFF = Roll moment coefficient\r
-FlightDataType.TYPE_ROLL_FORCING_COEFF = Roll forcing coefficient\r
-FlightDataType.TYPE_ROLL_DAMPING_COEFF = Roll damping coefficient\r
-FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Pitch damping coefficient\r
-FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Yaw damping coefficient\r
-FlightDataType.TYPE_REFERENCE_LENGTH = Referenzlänge\r
-FlightDataType.TYPE_REFERENCE_AREA = Referenzfläche\r
-FlightDataType.TYPE_ORIENTATION_THETA = Vertical orientation (zenith)\r
-FlightDataType.TYPE_ORIENTATION_PHI = Lateral orientation (azimuth)\r
-FlightDataType.TYPE_WIND_VELOCITY = Windgeschwindigkeit\r
-FlightDataType.TYPE_AIR_TEMPERATURE = Lufttemperatur\r
-FlightDataType.TYPE_AIR_PRESSURE = Luftdruck\r
-FlightDataType.TYPE_SPEED_OF_SOUND = Schallgeschwindigkeit\r
-FlightDataType.TYPE_TIME_STEP = Simulationsintervall\r
-FlightDataType.TYPE_COMPUTATION_TIME = Berechnnungszeit\r
-FlightDataType.TYPE_LATITUDE = Latitude\r
-FlightDataType.TYPE_LONGITUDE = Longitude\r
-FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration\r
-\r
-! PlotConfiguration\r
-PlotConfiguration.Verticalmotion = Vertikale Bewegung über Zeit\r
-PlotConfiguration.Totalmotion = Gesamte Bewegung über Zeit\r
-PlotConfiguration.Flightside = Flight side profile\r
-PlotConfiguration.Stability = Stabilität über Zeit\r
-PlotConfiguration.Dragcoef = Drag coefficients vs. Mach number\r
-PlotConfiguration.Rollcharacteristics = Roll characteristics\r
-PlotConfiguration.Angleofattack = Angle of attack and orientation vs. time\r
-PlotConfiguration.Simulationtime = Simulationszeitschritt und Berechnungszeit\r
-\r
-! Warning\r
-Warning.LargeAOA.str1 = Large angle of attack encountered.\r
-Warning.LargeAOA.str2 = Large angle of attack encountered (\r
-Warning.DISCONTINUITY = Unstetigkeit im Raketendurchmesser\r
-Warning.THICK_FIN = Dicke Leitwerke können nicht präzise modelliert werden.\r
-Warning.JAGGED_EDGED_FIN = Gezackte Ecken in Leitwerken können unpräzise Ergebnisse liefern.\r
-Warning.LISTENERS_AFFECTED = Simulationsempfänger haben die Simulation beeinflusst.\r
-Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Bergungssystem wurde ausgelöst während der Motor noch gebrannt hat.\r
-Warning.FILE_INVALID_PARAMETER = Ignoriere ungültigen Parameter.\r
-\r
-\r
-! Scale dialog\r
-ScaleDialog.lbl.scaleRocket = Entire rocket\r
-ScaleDialog.lbl.scaleSubselection = Selection and all subcomponents\r
-ScaleDialog.lbl.scaleSelection = Only selected component\r
-ScaleDialog.title = Scale design\r
-ScaleDialog.lbl.scale = Scale:\r
-ScaleDialog.lbl.scale.ttip = Select whether to scale the entire design or only the selected component\r
-ScaleDialog.lbl.scaling = Scaling to apply:\r
-ScaleDialog.lbl.scaling.ttip = Resulting size, values above 100% grow and values below 100% shrink the design.\r
-! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"\r
-ScaleDialog.lbl.scaleFrom = Scale from\r
-ScaleDialog.lbl.scaleTo = to\r
-ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and resulting length.\r
-ScaleDialog.checkbox.scaleMass = Update explicit mass values\r
-ScaleDialog.checkbox.scaleMass.ttip = Scale mass component and override mass values by the cube of the scaling factor\r
-ScaleDialog.button.scale = Scale\r
-ScaleDialog.undo.scaleRocket = Scale rocket\r
-ScaleDialog.undo.scaleComponent = Scale component\r
-ScaleDialog.undo.scaleComponents = Scale components\r
-\r
-!icons\r
-Icons.Undo = Undo\r
-Icons.Redo = Redo\r
-\r
-OpenRocketPrintable.Partsdetail = Parts detail\r
-OpenRocketPrintable.Fintemplates = Fin templates\r
-OpenRocketPrintable.DesignReport = Design Report\r
-\r
-OpenRocketDocument.Redo = Redo\r
-OpenRocketDocument.Undo = Undo\r
-\r
-!EllipticalFinSet\r
-EllipticalFinSet.Ellipticalfinset = Elliptical fin set\r
-\r
-! Optimization\r
-\r
-! Modifiers\r
-\r
-optimization.modifier.nosecone.length = Length\r
-optimization.modifier.nosecone.length.desc = Optimize the nose cone length.\r
-optimization.modifier.nosecone.diameter = Diameter\r
-optimization.modifier.nosecone.diameter.desc = Optimize the nose cone base diameter.\r
-optimization.modifier.nosecone.thickness = Thickness\r
-optimization.modifier.nosecone.thickness.desc = Optimize the nose cone wall thickness.\r
-optimization.modifier.nosecone.shapeparameter = Shape parameter\r
-optimization.modifier.nosecone.shapeparameter.desc = Optimize the nose cone shape parameter.\r
-\r
-optimization.modifier.transition.length = Length\r
-optimization.modifier.transition.length.desc = Optimize the transition length.\r
-optimization.modifier.transition.forediameter = Fore diameter\r
-optimization.modifier.transition.forediameter.desc = Optimize the transition fore diameter.\r
-optimization.modifier.transition.aftdiameter = Aft diameter\r
-optimization.modifier.transition.aftdiameter.desc = Optimize the transition aft diameter.\r
-optimization.modifier.transition.thickness = Thickness\r
-optimization.modifier.transition.thickness.desc = Optimize the transition wall thickness.\r
-optimization.modifier.transition.shapeparameter = Shape parameter\r
-optimization.modifier.transition.shapeparameter.desc = Optimize the transition shape parameter.\r
-\r
-optimization.modifier.bodytube.length = Length\r
-optimization.modifier.bodytube.length.desc = Optimize the body tube length.\r
-optimization.modifier.bodytube.outerDiameter = Outer diameter\r
-optimization.modifier.bodytube.outerDiameter.desc = Optimize the body tube outer diameter while maintaining the wall thickness.\r
-optimization.modifier.bodytube.thickness = Thickness\r
-optimization.modifier.bodytube.thickness.desc = Optimize the body tube wall thickness.\r
-\r
-optimization.modifier.trapezoidfinset.rootChord = Root chord\r
-optimization.modifier.trapezoidfinset.rootChord.desc = Optimize the root chord length of the fin set (length of fin at the rocket body).\r
-optimization.modifier.trapezoidfinset.tipChord = Tip chord\r
-optimization.modifier.trapezoidfinset.tipChord.desc = Optimize the tip chord length of the fin set (length of fin at outer edge).\r
-optimization.modifier.trapezoidfinset.sweep = Sweep\r
-optimization.modifier.trapezoidfinset.sweep.desc = Optimize the sweep of the fin set (distance that the leading edge sweeps backwards).\r
-optimization.modifier.trapezoidfinset.height = Height\r
-optimization.modifier.trapezoidfinset.height.desc = Optimize the height (semi-span) of the fin set.\r
-\r
-optimization.modifier.ellipticalfinset.length = Root chord\r
-optimization.modifier.ellipticalfinset.length.desc = Optimize the root chord length of the fin set.\r
-optimization.modifier.ellipticalfinset.height = Height\r
-optimization.modifier.ellipticalfinset.height.desc = Optimize the height (semi-span) of the fin set.\r
-\r
-optimization.modifier.finset.cant = Cant angle\r
-optimization.modifier.finset.cant.desc = Optimize the cant angle of the fin set.\r
-optimization.modifier.finset.position = Position\r
-optimization.modifier.finset.position.desc = Optimize the fin set position along the rocket body.\r
-\r
-optimization.modifier.launchlug.length = Length\r
-optimization.modifier.launchlug.length.desc = Optimize the launch lug length.\r
-optimization.modifier.launchlug.outerDiameter = Outer diameter\r
-optimization.modifier.launchlug.outerDiameter.desc = Optimize the outer diameter of the launch lug.\r
-optimization.modifier.launchlug.thickness = Thickness\r
-optimization.modifier.launchlug.thickness.desc = Optimize the launch lug thickness while keeping the outer diameter constant.\r
-optimization.modifier.launchlug.position = Position\r
-optimization.modifier.launchlug.position.desc = Optimize the launch lug position along the rocket body.\r
-\r
-\r
-optimization.modifier.internalcomponent.position = Position\r
-optimization.modifier.internalcomponent.position.desc = Optimize the position of the component relative to the parent component.\r
-\r
-optimization.modifier.masscomponent.mass = Mass\r
-optimization.modifier.masscomponent.mass.desc = Optimize the mass of the mass component.\r
-\r
-optimization.modifier.parachute.diameter = Diameter\r
-optimization.modifier.parachute.diameter.desc = Optimize the parachute canopy diameter.\r
-optimization.modifier.parachute.coefficient = Drag coefficient\r
-optimization.modifier.parachute.coefficient.desc = Optimize the drag coefficient of the parachute. Typical parachutes have a drag coefficient of about 0.8.\r
-\r
-optimization.modifier.streamer.length = Length\r
-optimization.modifier.streamer.length.desc = Optimize the length of the streamer.\r
-optimization.modifier.streamer.width = Width\r
-optimization.modifier.streamer.width.desc = Optimize the width of the streamer.\r
-optimization.modifier.streamer.aspectRatio = Aspect ratio\r
-optimization.modifier.streamer.aspectRatio.desc = Optimize the aspect ratio of the streamer (length/width). You should NOT select streamer length or width at the same time with the aspect ratio.\r
-optimization.modifier.streamer.coefficient = Drag coefficient\r
-optimization.modifier.streamer.coefficient.desc = Optimize the drag coefficient of the streamer.\r
-\r
-optimization.modifier.recoverydevice.deployDelay = Deployment delay\r
-optimization.modifier.recoverydevice.deployDelay.desc = Optimize the deployment delay of the recovery device.\r
-optimization.modifier.recoverydevice.deployAltitude = Deployment altitude\r
-optimization.modifier.recoverydevice.deployAltitude.desc = Optimize the deployment altitude of the recovery device.\r
-\r
-optimization.modifier.rocketcomponent.overrideMass = Override mass\r
-optimization.modifier.rocketcomponent.overrideMass.desc = Optimize the overridden mass of the component.\r
-optimization.modifier.rocketcomponent.overrideCG = Override CG\r
-optimization.modifier.rocketcomponent.overrideCG.desc = Optimize the overridden center of gravity of the component.\r
-\r
-optimization.modifier.motormount.overhang = Motor overhang\r
-optimization.modifier.motormount.overhang.desc = Optimize the motor overhang.\r
-optimization.modifier.motormount.delay = Motor ignition delay\r
-optimization.modifier.motormount.delay.desc = Optimize the motor ignition delay.\r
-\r
-\r
-\r
-\r
-! General rocket design optimization dialog\r
-\r
-GeneralOptimizationDialog.title = Rocket optimization\r
-GeneralOptimizationDialog.goal.maximize = Maximize value\r
-GeneralOptimizationDialog.goal.minimize = Minimize value\r
-GeneralOptimizationDialog.goal.seek = Seek value of\r
-GeneralOptimizationDialog.btn.start = Start optimization\r
-GeneralOptimizationDialog.btn.stop = Stop optimization\r
-GeneralOptimizationDialog.lbl.paramsToOptimize = Parameters to optimize:\r
-GeneralOptimizationDialog.btn.add = Add\r
-GeneralOptimizationDialog.btn.add.ttip = Add the selected parameter to the optimization\r
-GeneralOptimizationDialog.btn.remove = Remove\r
-GeneralOptimizationDialog.btn.remove.ttip = Remove the selected parameter from the optimization\r
-GeneralOptimizationDialog.btn.removeAll = Remove all\r
-GeneralOptimizationDialog.btn.removeAll.ttip = Remove all parameters from the optimization\r
-GeneralOptimizationDialog.lbl.availableParams = Available parameters:\r
-GeneralOptimizationDialog.lbl.optimizationOpts = Optimization options\r
-GeneralOptimizationDialog.lbl.optimizeSim = Optimize simulation:\r
-GeneralOptimizationDialog.lbl.optimizeSim.ttip = Select which simulation to optimize\r
-GeneralOptimizationDialog.lbl.optimizeValue = Optimized value:\r
-GeneralOptimizationDialog.lbl.optimizeValue.ttip = Select what value is to be optimized\r
-GeneralOptimizationDialog.lbl.optimizeGoal = Optimization goal:\r
-GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Select the goal of the optimization\r
-GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Custom value to seek\r
-GeneralOptimizationDialog.lbl.requireStability = Required stability\r
-GeneralOptimizationDialog.lbl.requireMinStability = Minimum stability:\r
-GeneralOptimizationDialog.lbl.requireMinStability.ttip = Require a minimum static stability margin for the design\r
-GeneralOptimizationDialog.lbl.requireMaxStability = Maximum stability:\r
-GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Require a maximum static stability margin for the design\r
-GeneralOptimizationDialog.status.bestValue = Best value:\r
-GeneralOptimizationDialog.status.bestValue.ttip = Best optimization value found so far.\r
-GeneralOptimizationDialog.status.stepCount = Step count:\r
-GeneralOptimizationDialog.status.stepCount.ttip = Number of optimization steps that have been performed.\r
-GeneralOptimizationDialog.status.evalCount = Evaluations:\r
-GeneralOptimizationDialog.status.evalCount.ttip = Total number of function evaluations (simulations) that have been performed.\r
-GeneralOptimizationDialog.status.stepSize = Step size:\r
-GeneralOptimizationDialog.status.stepSize.ttip = Current optimization step size (relative to the optimization parameter ranges)\r
-GeneralOptimizationDialog.btn.plotPath = Plot path\r
-GeneralOptimizationDialog.btn.plotPath.ttip = Plot the optimization path (one and two dimensional optimization only)\r
-GeneralOptimizationDialog.btn.save = Save path\r
-GeneralOptimizationDialog.btn.save.ttip = Save the results of the function evaluations (simulations) as a CSV file.\r
-GeneralOptimizationDialog.btn.apply = Apply optimization\r
-GeneralOptimizationDialog.btn.apply.ttip = Apply the optimization results to the rocket design\r
-GeneralOptimizationDialog.btn.reset = Reset\r
-GeneralOptimizationDialog.btn.reset.ttip = Reset the rocket design to the current rocket design\r
-GeneralOptimizationDialog.btn.close = Close\r
-GeneralOptimizationDialog.btn.close.ttip = Close the dialog without modifying the rocket design\r
-GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters.\r
-GeneralOptimizationDialog.error.selectParams.title = Select optimization parameters\r
-GeneralOptimizationDialog.error.optimizationFailure.text = The optimization failed to run:\r
-GeneralOptimizationDialog.error.optimizationFailure.title = Optimization failed\r
-GeneralOptimizationDialog.undoText = Apply optimization\r
-GeneralOptimizationDialog.basicSimulationName = Basic simulation\r
-GeneralOptimizationDialog.noSimulationName = No simulation\r
-GeneralOptimizationDialog.table.col.parameter = Parameter\r
-GeneralOptimizationDialog.table.col.current = Current\r
-GeneralOptimizationDialog.table.col.min = Minimum\r
-GeneralOptimizationDialog.table.col.max = Maximum\r
-GeneralOptimizationDialog.export.header = Include header line\r
-GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions.\r
-GeneralOptimizationDialog.export.stability = Stability\r
-\r
-\r
-! Dialog for plotting optimization results\r
-OptimizationPlotDialog.title = Optimization results\r
-OptimizationPlotDialog.lbl.zoomInstructions = Click and drag down+right to zoom in, up+left to zoom out\r
-OptimizationPlotDialog.plot1d.title = Optimization result\r
-OptimizationPlotDialog.plot1d.series = Optimization result\r
-OptimizationPlotDialog.plot2d.title = Optimization path\r
-OptimizationPlotDialog.plot2d.path = Optimization path\r
-OptimizationPlotDialog.plot2d.evals = Evaluations\r
-OptimizationPlotDialog.plot.ttip.stability = Stability:\r
-OptimizationPlotDialog.plot.label.optimum = Optimum\r
-\r
-! Optimization parameters\r
-MaximumAltitudeParameter.name = Apogee altitude\r
-MaximumVelocityParameter.name = Maximum velocity\r
-MaximumAccelerationParameter.name = Maximum acceleration\r
-StabilityParameter.name = Stability\r
-GroundHitVelocityParameter.name = Ground hit speed\r
-LandingDistanceParameter.name = Landing distance\r
-TotalFlightTimeParameter.name = Total flight time\r
-DeploymentVelocityParameter.name = Velocity at parachute deployment\r
-\r
-\r
-! Compass directions drawn on a compass rose.\r
-CompassRose.lbl.north = N\r
-CompassRose.lbl.east = E\r
-CompassRose.lbl.south = S\r
-CompassRose.lbl.west = W\r
-\r
-! Compass directions with subdirections. These might not be localized even if the directions on the compass rose are.\r
-CompassSelectionButton.lbl.N = N\r
-CompassSelectionButton.lbl.NE = NE\r
-CompassSelectionButton.lbl.E = E\r
-CompassSelectionButton.lbl.SE = SE\r
-CompassSelectionButton.lbl.S = S\r
-CompassSelectionButton.lbl.SW = SW\r
-CompassSelectionButton.lbl.W = W\r
-CompassSelectionButton.lbl.NW = NW\r
-\r
-\r
-SlideShowDialog.btn.next = Next\r
-SlideShowDialog.btn.prev = Previous\r
-\r
-GuidedTourSelectionDialog.title = Guided tours\r
-GuidedTourSelectionDialog.lbl.selectTour = Select guided tour:\r
-GuidedTourSelectionDialog.lbl.description = Tour description:\r
-GuidedTourSelectionDialog.lbl.length = Number of slides:\r
-GuidedTourSelectionDialog.btn.start = Start tour!\r
+++ /dev/null
-#
-# Spanish base translation file
-# translations provided by Tripoli Spain
-#
-# Should you need to add new logical keys here is the proposed method
-#
-# className.ComponantType.componantName
-#
-#
-# Text tokens within braces should not be translated, e.g.
-# "The file '{filename}' exists."
-# They are pieces that are inserted dynamically.
-#
-
-
-! Set to the name of the current translation file (used for debugging purposes)
-debug.currentFile = messages_es.properties
-
-! RocketActions
-RocketActions.checkbox.Donotaskmeagain = No volver a preguntarme
-RocketActions.lbl.Youcanchangedefop = Puede modificar la operación por defecto con sus preferencias
-RocketActions.showConfirmDialog.lbl1 = ¿Borrar las simulaciones seleccionadas?
-RocketActions.showConfirmDialog.lbl2 = <html><i>Esta operación no puede deshacerse.</i>
-RocketActions.showConfirmDialog.title = Borrar simulaciones
-RocketActions.DelCompAct.Delete = Borrar
-RocketActions.DelCompAct.ttip.Delete = Borrar el componente seleccionado
-RocketActions.DelSimuAct.Delete = Borrar
-RocketActions.DelSimuAct.ttip.Delete = Borrar la simulación seleccionada
-RocketActions.DelAct.Delete = Borrar
-RocketActions.DelAct.ttip.Delete = Eliminar elemento seleccionado
-RocketActions.CutAction.Cut = Cortar
-RocketActions.CutAction.ttip.Cut = Quitar y copiar al portapapeles
-RocketActions.CopyAct.Copy = Copiar
-RocketActions.CopyAct.ttip.Copy = Copiar al portapapeles
-RocketActions.PasteAct.Paste = Pegar
-RocketActions.PasteAct.ttip.Paste = Pegar al portapapeles
-RocketActions.EditAct.Edit = Editar componente
-RocketActions.EditAct.ttip.Edit = Editar valores del componente seleccionado
-RocketActions.NewStageAct.Newstage = Nueva etapa
-RocketActions.NewStageAct.ttip.Newstage = Añadir una nueva etapa al diseño del cohete
-RocketActions.ActBoosterstage = Etapa booster
-RocketActions.MoveUpAct.Moveup = Mover hacia arriba
-RocketActions.MoveUpAct.ttip.Moveup = Mover este componente hacia arriba
-RocketActions.MoveDownAct.Movedown = Mover hacia abajo
-RocketActions.MoveDownAct.ttip.Movedown = Mover este componente hacia abajo
-
-! RocketPanel
-RocketPanel.FigTypeAct.Sideview = Vista lateral
-RocketPanel.FigTypeAct.ttip.Sideview = Vista desde un lateral
-RocketPanel.FigTypeAct.Backview = Vista trasera
-RocketPanel.FigTypeAct.ttip.Backview = Vista desde atrás
-RocketPanel.lbl.Motorcfg = Configuración del motor
-RocketPanel.lbl.infoMessage = <html>Click para seleccionar Mayúsculas+click para seleccionar otro Doble-click para mostrar Click+arrastrar para mover
-
-! BasicFrame
-BasicFrame.SimpleFileFilter1 = Todos los diseños de cohete(*.ork; *.rkt)
-BasicFrame.SimpleFileFilter2 = Diseños OpenRocket (*.ork)
-BasicFrame.SimpleFileFilter3 = Diseños RockSim (*.rkt)
-BasicFrame.tab.Rocketdesign = Diseño del cohete
-BasicFrame.tab.Flightsim = Simulaciones de vuelo
-BasicFrame.title.Addnewcomp = Añadir un nuevo componente
-!BasicFrame.item.Openrocketdesign = Abrir un diseño de cohete
-!BasicFrame.item.Openexamplerocketdesign = Abrir un ejemplo de diseño de cohete
-!BasicFrame.item.SavecurRocketdesign = Guardar el diseño actual
-!BasicFrame.item.SavecurRocketdesnewfile = Guardar el diseño actual como un nuevo documento
-!BasicFrame.item.Printpart = Imprimir un listado de componentes y un esquema de aleta
-!BasicFrame.item.Closedesign = Cerrar el diseño actual
-!BasicFrame.item.Quitprogram = Abandonar el programa
-!BasicFrame.menu.Rocketedt = Mostrando el cohete
-BasicFrame.dlg.lbl1 = Diseño
-BasicFrame.dlg.lbl2 = No se ha guardado
-BasicFrame.dlg.lbl3 = ¿Quiere guardarlo?
-BasicFrame.dlg.title = Diseño no guardado
-BasicFrame.StageName.Sustainer = Etapa principal
-BasicFrame.WarningDialog.txt1 = Mientras se abría, se encontraron los siguiente problemas
-BasicFrame.WarningDialog.txt2 = Algunas configuraciones de diseño no pudieron cargarse correctamente.
-BasicFrame.WarningDialog.title = Precauciones mientras se abre el archivo
-
-
-! General error messages used in multiple contexts
-error.fileExists.title = El archivo ya existe
-error.fileExists.desc = El archivo con el nombre '{filename}' ya existe. ¿Desea sobrescribir la versión anterior?
-
-error.writing.title = Error al guardar el archivo
-error.writing.desc = Ha ocurrido un error al guardar el archivo:
-
-
-! Labels used in buttons of dialog windows
-# TODO: Rename these to "btn.xxx"
-button.ok = OK
-button.cancel = Cancelar
-button.close = Cerrar
-
-! Common labels used in buttons of dialog windows
-dlg.but.ok = OK
-dlg.but.cancel = Cancelar
-dlg.but.close = Cerrar
-
-! General file type names
-filetypes.pdf = Archivos PDF
-
-
-! About Dialog
-AboutDialog.lbl.version = Versión
-! The texts below provide additional credits for the translation maintainer
-! - In AboutDialog.lbl.translation replace "English" with the current language.
-! - AboutDialog.lbl.translator is the translator / group name (may be empty)
-! - AboutDialog.lbl.translatorWebsite is a URL to the translator / group (may be empty)
-! - AboutDialog.lbl.translatorIcon is the file name of an icon under pix/translators/ (may be empty)
-AboutDialog.lbl.translation = Traducido al español por:
-AboutDialog.lbl.translator = Tripoli Spain
-AboutDialog.lbl.translatorWebsite = http://www.tripoli-spain.org/
-AboutDialog.lbl.translatorIcon = logoTripoliSpain.png
-
-
-! Print dialog
-PrintDialog.title = Imprimir o exportar
-PrintDialog.but.previewAndPrint = Vista previa e Imprimir
-PrintDialog.checkbox.showByStage = Mostrar por etapas
-PrintDialog.lbl.selectElements = Seleccionar elementos a incluir:
-printdlg.but.saveaspdf = Guardar como PDF
-printdlg.but.preview = Previsualizar
-printdlg.but.settings = Configuración
-PrintDialog.error.preview.title = Imposible abrir vista previa
-PrintDialog.error.preview.desc1 = Imposible abrir vista previa en PDF.
-PrintDialog.error.preview.desc2 = Por favor use la opción Guardar como PDF.
-
-
-!PrintSettingsDialog
-PrintSettingsDialog.title = Imprimir puesta a punto
-PrintSettingsDialog.lbl.Templatefillcolor = Plantilla de colores:
-PrintSettingsDialog.lbl.Templatebordercolor = Color del borde de la plantilla:
-PrintSettingsDialog.lbl.Papersize = Tamaño del papel:
-PrintSettingsDialog.lbl.Paperorientation = Orientación del papel:
-PrintSettingsDialog.but.Reset = Reiniciar
-PrintSettingsDialog.but.Close = Cerrar
-
-
-! Bug Report dialog
-bugreport.dlg.title = Informe de errores
-bugreport.dlg.but.Sendbugreport = Enviar informe de error
-bugreport.dlg.but.Sendbugreport.Ttip = Enviar automáticamente un informe de error a los creadores de Open Rocket
-bugreport.dlg.successmsg1 = Informe de error enviado con éxito
-bugreport.dlg.successmsg2 = ¡Gracias por ayudar a mejorar Open Rocket!
-bugreport.dlg.successmsg3 = Informe de error enviado
-bugreport.dlg.connectedInternet = <html>Si está conectado a Internet, haga Clik en <em>Enviar informe de errores</em>.
-bugreport.dlg.otherwise = De otro modo, también puede copiar y enviar el texto a la dirección:
-bugreport.lbl.Theinformation = La información que ha detallado se incluirá en un informe de error público. Asegúrese de que no contiene ninguna información que usted no desee hacer pública.
-bugreport.dlg.failedmsg1 = OpenRocket fue incapaz de enviar el informe de error:
-bugreport.dlg.failedmsg2 = Por favor envíe manualmente el informe a
-bugreport.dlg.failedmsg3 = Error al enviar el informe
-bugreport.reportDialog.txt = <html><b>Puede realizar un informe de errores escribiendo en el formulario de abajo y enviarlo.</b><br>También puede informar de los errores adjuntando el archivo de su proyecto por email.
-bugreport.reportDialog.txt2 = <html><b>Por favor incluya una breve descripción de lo que estaba haciendo cuando ocurrió el error.</b>
-bugreport.dlg.provideDescription = Por favor, primero proporcione una descripción del error.
-bugreport.dlg.provideDescription.title = Descripción del error omitida
-
-
-! Debug log dialog
-debuglogdlg.but.clear = Limpiar
-debuglogdlg.OpenRocketdebuglog = Registro de sucesos
-debuglogdlg.Displayloglines = Mostrar líneas de registro:
-debuglogdlg.Follow = Seguir
-debuglogdlg.col.Time = Hora
-debuglogdlg.col.Level = Nivel
-debuglogdlg.col.Location = Localización
-debuglogdlg.col.Message = Mensaje
-debuglogdlg.lbl.Loglinenbr = Número de línea de registro:
-debuglogdlg.lbl.Time = Hora:
-debuglogdlg.lbl.Level = Nivel:
-debuglogdlg.lbl.Location = Localización:
-debuglogdlg.lbl.Logmessage = Texto del mensaje:
-debuglogdlg.lbl.Stacktrace = Trazabilidad de la pila:
-
-
-! Edit Motor configuration dialog
-edtmotorconfdlg.but.removemotor = Quitar motor
-edtmotorconfdlg.but.Selectmotor = Seleccionar motor
-edtmotorconfdlg.but.Removeconfiguration = Quitar configuración
-edtmotorconfdlg.but.Newconfiguration = Nueva configuración
-edtmotorconfdlg.lbl.Motormounts = <html><b>Porta motor:</b>
-edtmotorconfdlg.title.Editmotorconf = Mostrar las configuraciones de motor
-edtmotorconfdlg.selectcomp = <html>Seleccionar qué componentes tienen la función de porta motor:
-edtmotorconfdlg.lbl.Motorconfig = <html><b>Configuraciones del motor:</b>
-edtmotorconfdlg.lbl.Configname = Nombre de la configuración:
-edtmotorconfdlg.lbl.Leavenamedefault = Dejar el nombre por defecto.
-
-! Example design dialog
-exdesigndlg.but.open = Abrir
-exdesigndlg.lbl.Selectexample = Al abrir seleccione ejemplos de diseños:
-exdesigndlg.lbl.Openexampledesign = Abra un diseño como ejemplo
-exdesigndlg.lbl.Exampledesignsnotfound = Los ejemplos de diseño podrían no encontrarse.
-exdesigndlg.lbl.Examplesnotfound = Ejemplos no encontrados
-
-
-! Material edit panel
-matedtpan.but.new = Nuevo
-matedtpan.but.edit = Editar
-matedtpan.but.delete = Borrar
-matedtpan.but.revertall = Invertir todo
-matedtpan.col.Material = Material
-matedtpan.col.Type = Tipo
-matedtpan.col.Density = Densidad
-matedtpan.col.but.ttip.New = Añadir un nuevo material
-matedtpan.title.Addcustmaterial = Añadir un material hecho en casa
-matedtpan.but.ttip.edit = Editar un material existente
-matedtpan.title.Editmaterial = Editar material
-matedtpan.title2.Editmaterial = Los materiales construidos no se pueden modificar
-matedtpan.but.ttip.delete = Borrar un material predefinido
-matedtpan.but.ttip.revertall = Borrar todos los materiales predefinidos
-matedtpan.title.Deletealluser-defined = ¿Borrar todos los materiales predefinidos?
-matedtpan.title.Revertall = ¿Revertir todo?
-matedtpan.lbl.edtmaterials = Editar materiales que no afectaran los diseños existentes.
-
-!MaterialModel
-MaterialModel.title.Material = Material
-MaterialModel.title.Defcustmat = Definir material hecho en casa
-
-
-! Preference dialog
-pref.dlg.but.add = Agregar
-pref.dlg.but.reset = Reiniciar
-pref.dlg.but.checknow = Comprobar ahora
-pref.dlg.but.defaultmetric = Sistema Métrico por defecto
-pref.dlg.but.defaultimperial = Sistema Imperial por defecto
-pref.dlg.title.Preferences = Preferencias
-pref.dlg.tab.Units = Unidades
-pref.dlg.tab.Defaultunits = Unidades por defecto
-pref.dlg.tab.Materials = Materiales
-pref.dlg.tab.Custommaterials = Materiales hechos en casa
-pref.dlg.tab.Options = Opciones
-pref.dlg.tab.Miscellaneousoptions = Otras opciones
-pref.dlg.lbl.Positiontoinsert = Posición para introducir nuevos componentes del fuselaje:
-pref.dlg.lbl.Confirmdeletion = Confirmar borrar simulaciones:
-pref.dlg.lbl.User-definedthrust = Curvas de potencia definidas por el usuario:
-pref.dlg.Allthrustcurvefiles = Todos los ficheros de curvas de potencia (*.eng; *.rse; *.zip; directorios)
-pref.dlg.RASPfiles = Ficheros de motor RASP (*.eng)
-pref.dlg.RockSimfiles = Ficheros de motor Rocksim (*.rse)
-pref.dlg.ZIParchives = Archivos ZIP (*.zip)
-pref.dlg.checkbox.Checkupdates = Comprobar actualizaciones de software al arrancar
-pref.dlg.ttip.Checkupdatesnow = Comprobar actualizaciones de software ahora
-pref.dlg.lbl.Selectprefunits = Seleccione sus unidades preferidas:
-pref.dlg.lbl.Rocketdimensions = Dimensiones del cohete:
-pref.dlg.lbl.Linedensity = Densidad:
-pref.dlg.lbl.Motordimensions = Dimensiones del motor:
-pref.dlg.lbl.Surfacedensity = Densidad superficial:
-pref.dlg.lbl.Distance = Distancia:
-pref.dlg.lbl.Bulkdensity = Densidad media:
-pref.dlg.lbl.Velocity = Velocidad:
-pref.dlg.lbl.Surfaceroughness = Rugosidad de la superficie:
-pref.dlg.lbl.Acceleration = Aceleración:
-pref.dlg.lbl.Area = Área:
-pref.dlg.lbl.Mass = Masa:
-pref.dlg.lbl.Angle = Ángulo:
-pref.dlg.lbl.Force = Fuerza:
-pref.dlg.lbl.Rollrate = Valor de rotación:
-pref.dlg.lbl.Totalimpulse = Impulso total:
-pref.dlg.lbl.Temperature = Temperatura:
-pref.dlg.lbl.Momentofinertia = Momento de inercia:
-pref.dlg.lbl.Pressure = Presión:
-pref.dlg.lbl.Stability = Estabilidad:
-pref.dlg.lbl.FlightTime = Tiempo de vuelo:
-pref.dlg.lbl.effect1 = Los cambios tendrán efecto cuando se abra nuevamente una ventana.
-pref.dlg.lbl.Checkingupdates = Comprobando actualizaciones...
-pref.dlg.lbl.msg1 = Ocurrió un error mientras se comunicaba con el servidor.
-pref.dlg.lbl.msg2 = Incapaz de recuperar la información de las actualizaciones
-pref.dlg.lbl.msg3 = Usted está utilizando la última versión de Open Rocket.
-pref.dlg.lbl.msg4 = No hay actualizaciones disponibles
-pref.dlg.PrefChoiseSelector1 = Preguntar siempre
-pref.dlg.PrefChoiseSelector2 = Insertar en medio
-pref.dlg.PrefChoiseSelector3 = Añadir al final
-pref.dlg.PrefBooleanSelector1 = Borrar
-pref.dlg.PrefBooleanSelector2 = Confirmar
-pref.dlg.Add = Añadir
-pref.dlg.DescriptionArea.Adddirectories = Añadir directorios, archivos de motor RASP (*.eng), archivos de motor RockSim (*.rse) o archivos ZIP separados por punto y coma (;) para cargar curvas de empuje externas. Los cambios tendrán efecto la próxima vez que abra OpenRocket.
-
-PreferencesDialog.lbl.language = Idioma de la interfaz:
-PreferencesDialog.languages.default = Idioma por defecto
-PreferencesDialog.lbl.languageEffect = El idioma cambiará la próxima vez que abra OpenRocket.
-
-! Simulation edit dialog
-simedtdlg.but.runsimulation = Lanzar la simulación
-simedtdlg.but.resettodefault = Restaurar por defecto
-simedtdlg.but.add = Agregar
-simedtdlg.but.remove = Quitar
-simedtdlg.title.Editsim = Mostrar la simulación
-simedtdlg.lbl.Simname = Nombre de la simulación
-simedtdlg.tab.Launchcond = Condiciones del lanzamiento
-simedtdlg.tab.Simopt = Opciones de simulación
-simedtdlg.tab.Plotdata = Datos del gráfico
-simedtdlg.tab.Exportdata = Exportar datos
-simedtdlg.lbl.Motorcfg = Configuración del motor:
-simedtdlg.lbl.ttip.Motorcfg = Seleccionar la configuración del motor a usar
-simedtdlg.combo.ttip.motorconf = Seleccione la configuración del motor a usar
-simedtdlg.lbl.Wind = Viento
-simedtdlg.lbl.Averwindspeed = Velocidad media del viento
-simedtdlg.lbl.ttip.Averwindspeed = Velocidad media del viento en relación al suelo
-simedtdlg.lbl.Stddeviation = Desviación estándar
-simedtdlg.lbl.ttip.Stddeviation = <html>Desviación estándar de la velocidad del viento.<br>La velocidad del viento se encuentra dentro del doble de la desviación media en un 95% del tiempo.
-simedtdlg.lbl.Turbulenceintensity = Intensidad de la turbulencia
-simedtdlg.lbl.ttip.Turbulenceintensity1 = <html>La intensidad de la turbulencia es la desviación estándar dividida por la velocidad media del viento.<br>
-simedtdlg.lbl.ttip.Turbulenceintensity2 = Valores típicos en el campo
-simedtdlg.lbl.ttip.Turbulenceintensity3 = a
-simedtdlg.border.Atmoscond = Condiciones atmosféricas
-simedtdlg.checkbox.InterStdAtmosphere = Usar los patrones de Atmosfera Internacional
-simedtdlg.checkbox.ttip.InterStdAtmosphere1 = <html>Seleccionar para usar el modelo de la International Standard Atmosphere.<br>Este modelo tiene una temperatura de
-simedtdlg.checkbox.ttip.InterStdAtmosphere2 = Y una presión de
-simedtdlg.checkbox.ttip.InterStdAtmosphere3 = A nivel del mar.
-simedtdlg.lbl.Temperature = Temperatura:
-simedtdlg.lbl.ttip.Temperature = Temperatura en el lugar del lanzamiento.
-simedtdlg.lbl.Pressure = Presión:
-simedtdlg.lbl.ttip.Pressure = Presión atmosférica en el lugar del lanzamiento
-simedtdlg.lbl.Launchsite = Lugar del lanzamiento
-simedtdlg.lbl.Latitude = Latitud:
-simedtdlg.lbl.ttip.Latitude = <html>La latitud del lugar de lanzamiento afecta la atracción terrestre.<br>Los valores positivos se dan en el hemisferio Norte, los negativos en el hemisferio Sur.
-
-simedtdlg.lbl.Longitude = Longitud:
-simedtdlg.lbl.ttip.Longitude = <html>Requerido para modelos de elevación y predicción meteorológica.
-
-simedtdlg.lbl.Altitude = Altitud:
-simedtdlg.lbl.ttip.Altitude = <html>Los valores por encima del nivel del mar <br>afectan al modelado de las condicones atmosféricas.
-simedtdlg.border.Launchrod = Varilla para lanzar
-simedtdlg.lbl.Length = Longitud:
-simedtdlg.lbl.ttip.Length = Longitud de la varilla de lanzamiento
-simedtdlg.lbl.Angle = Ángulo:
-simedtdlg.lbl.ttip.Angle = El ángulo de la varilla de lanzamiento con respecto a la vertical.
-simedtdlg.lbl.Direction = Dirección:
-simedtdlg.lbl.ttip.Direction1 = <html>Dirección de la varilla de lanzamiento relativa al viento.<br>
-simedtdlg.lbl.ttip.Direction2 = Contra el viento
-simedtdlg.lbl.ttip.Direction3 = A favor del viento
-simedtdlg.border.Simopt = Opciones del simulador
-simedtdlg.lbl.Calcmethod = Método de cálculo
-simedtdlg.lbl.ttip.Calcmethod = <html>El método Barrowman extendido considera las fuerzas aerodinámicas <br>que actúan sobre cuerpos cilíndricos en cohetes que vuelan con un <br>ángulo de ataque (AOA) superior a 10 grados.
-simedtdlg.lbl.ExtBarrowman = Barrowman Extendido
-simedtdlg.lbl.Simmethod = Método de simulación:
-simedtdlg.lbl.ttip.Simmethod1 = <html>El simulador de seis-grados-de-libertad permite al cohete una total libertad durante el vuelo.<br>
-simedtdlg.lbl.ttip.Simmethod2 = La integración mejora usando el método de integración numérica Runge-Kutta de cuarto orden.
-simedtdlg.lbl.GeodeticMethod = Cálculos geodésicos:
-simedtdlg.lbl.ttip.GeodeticMethodTip = En relación al cálculo de las coordenadas terrestres. Esto también activa los cálculos del Efecto Coriolis.
-simedtdlg.lbl.Timestep = Duración de la etapa
-simedtdlg.lbl.ttip.Timestep1 = <html>Tiempo entre etapas de simulación.<br>Un tiempo mas corto de etapa origina una simulación mas exacta pero mas lenta.<br>
-simedtdlg.lbl.ttip.Timestep2 = Con 4<sup>th</sup> el método de ordenar en la simulación es bastante preciso con un tiempo de etapa de
-simedtdlg.but.ttip.resettodefault = Restituir el tiempo de etapa a su valor por defecto (
-simedtdlg.border.Simlist = Extensiones del simulador
-simedtdlg.txt.longA1 = <html><i>Extensiones del simulador</i> es una característica avanzada que permite que el código escrito por un usuario pueda conectar e interactuar con la simulación mientras ésta se está ejecutando.
-simedtdlg.txt.longA2 = Para más detalles sobre las Extensiones, vea la documentación técnica de Open Rocket.
-simedtdlg.lbl.Curlist = Extensiones actuales
-simedtdlg.lbl.Addsimlist = Añadir una Extensión al simulador
-simedtdlg.lbl.Noflightdata = No hay datos disponibles del vuelo.
-simedtdlg.lbl.runsimfirst = Por favor accione la simulación primero.
-simedtdlg.chart.Simflight = Vuelo simulado
-simedtdlg.dlg.Simres = Resultados de la simulación
-simedtdlg.IntensityDesc.None = Ninguno
-simedtdlg.IntensityDesc.Verylow = Muy pesado
-simedtdlg.IntensityDesc.Low = Pesado
-simedtdlg.IntensityDesc.Medium = Medio
-simedtdlg.IntensityDesc.High = Alto
-simedtdlg.IntensityDesc.Veryhigh = Muy alto
-simedtdlg.IntensityDesc.Extreme = Extremo
-
-GeodeticComputationStrategy.none.name = Ninguna
-GeodeticComputationStrategy.none.desc = No incluir computaciones geodésicas.
-GeodeticComputationStrategy.spherical.name = Aproximación esférica
-GeodeticComputationStrategy.spherical.desc = <html>Al incluir las computaciones geodésicas se considera una Tierra esférica.<br>Este aspecto es bastante preciso en la mayoría de los proyectos.
-GeodeticComputationStrategy.wgs84.name = Elipsoidal WGS84
-GeodeticComputationStrategy.wgs84.desc = <html>Incluye las computaciones geodésicas sobre la referencia elipsoidal WGS84 utilizando el método de Vicenty.<br>Este aspecto es lento e innecesario en la mayoría de los casos.
-
-
-
-
-! Simulation Panel
-simpanel.but.newsimulation = Nueva simulación
-simpanel.but.editsimulation = Editar la simulación
-simpanel.but.runsimulations = Lanzar las simulaciones
-simpanel.but.deletesimulations = Borrar las simulaciones
-simpanel.but.plotexport = Exportar / Gráfica
-simpanel.but.ttip.newsimulation = Añadir una nueva simulación
-simpanel.but.ttip.editsim = Mostrar la simulación seleccionada
-simpanel.but.ttip.runsimu = Ejecutar de nuevo las simulaciones seleccionadas
-simpanel.but.ttip.deletesim = Borrar las simulaciones seleccionadas
-simpanel.checkbox.donotask = No preguntarme de nuevo
-simpanel.lbl.defpref = Puede cambiar la operación por defecto por las preferencias
-simpanel.dlg.lbl.DeleteSim1 = ¿Borrar las simulaciones seleccionadas?
-simpanel.dlg.lbl.DeleteSim2 = <html><i>Esta operación no puede deshacerse.</i>
-simpanel.dlg.lbl.DeleteSim3 = Borrar las simulaciones
-simpanel.col.Name = Nombre
-simpanel.col.Motors = Motores
-simpanel.col.Apogee = Apogeo
-simpanel.col.Maxvelocity = Velocidad máxima
-simpanel.col.Maxacceleration = Aceleración máxima
-simpanel.col.Timetoapogee = Tiempo hasta el apogeo
-simpanel.col.Flighttime = Duración del vuelo
-simpanel.col.Groundhitvelocity = Velocidad de llegada a tierra
-
-! SimulationRunDialog
-SimuRunDlg.title.RunSim = Ejecutar simulaciones
-SimuRunDlg.lbl.Running = Ejecutar
-SimuRunDlg.lbl.Simutime = Duración de la simulación:
-SimuRunDlg.lbl.Altitude = Altitud:
-SimuRunDlg.lbl.Velocity = Velocidad:
-SimuRunDlg.msg.Unabletosim = Incapaz de simular:
-SimuRunDlg.msg.errorOccurred = Ha ocurrido un error durante la simulación:
-SimuRunDlg.msg.AnException1 = Ha ocurrido una excepción durante la simulación:
-SimuRunDlg.msg.AnException2 = Por favor anote esto debajo como un error con todos los detalles.
-SimuRunDlg.msg.AssertionError1 = Se ha producido un error informático durante la simulación.
-SimuRunDlg.msg.AssertionError2 = Por favor anote esto debajo como un error con todos los detalles.
-SimuRunDlg.msg.unknownerror1 = Se ha detectado un error desconocido durante la simulación.
-SimuRunDlg.msg.unknownerror2 = El programa puede ser inestable, Guarde todos sus diseños y reinicie OpenRocket
-
-
-! SimulationExportPanel
-SimExpPan.desc = Documentos separados por comas (*.csv)
-SimExpPan.border.Vartoexport = Variables para exportar
-SimExpPan.but.Selectall = Seleccionar todo
-SimExpPan.but.Selectnone = No seleccionar nada
-SimExpPan.border.Fieldsep = Separador de campo
-SimExpPan.lbl.Fieldsepstr = Caracter separador de campo
-SimExpPan.lbl.longA1 = <html>Caracter para separar campos en el documento exportado.<br>
-SimExpPan.lbl.longA2 = Para valores separados en archivo (CSV) use comas ','.
-SimExpPan.checkbox.Includesimudesc = Incluir descripción de la simulación
-SimExpPan.checkbox.ttip.Includesimudesc = Incluye un comentario en el inicio del documento describiendo la simulación.
-SimExpPan.border.Comments = Comentarios
-SimExpPan.checkbox.Includefielddesc = Incluir descripciones del campo
-SimExpPan.checkbox.ttip.Includefielddesc = Incluye una línea de comentario con las descripciones de las variables exportadas.
-SimExpPan.checkbox.Incflightevents = Incluir los eventos del vuelo
-SimExpPan.checkbox.ttip.Incflightevents = Incluye una línea de comentario para cada evento del vuelo
-SimExpPan.lbl.Commentchar = Carácter de comentario
-SimExpPan.lbl.ttip.Commentchar = Características que marcan una línea de comentario.
-SimExpPan.but.Exporttofile = Exportar al documento ...
-SimExpPan.Fileexists.desc1 = Archivo \"
-SimExpPan.Fileexists.desc2 = \" ya existe. ¿Desea sobrescribir?
-SimExpPan.Fileexists.title = El archivo ya existe
-SimExpPan.ExportingVar.desc1 = Exportar variables
-SimExpPan.ExportingVar.desc2 = Exportar
-SimExpPan.ExportingVar.desc3 = variables de
-SimExpPan.Col.Variable = Variable
-SimExpPan.Col.Unit = Unidad
-
-
-CsvOptionPanel.separator.space = SPACE
-CsvOptionPanel.separator.tab = TAB
-
-
-
-! MotorPlot
-MotorPlot.title.Motorplot = Curva del motor
-MotorPlot.but.Select = Seleccionar la configuración del motor a usar
-MotorPlot.Chart.Motorthrustcurve = Curva de empuje del motor
-MotorPlot.Chart.Time = Tiempo / s
-MotorPlot.Chart.Thrust = Empuje / N
-MotorPlot.txt.Designation = Designación:
-MotorPlot.txt.Manufacturer = Fabricante:
-MotorPlot.txt.Type = Tipo:
-MotorPlot.txt.Delays = Retardos:
-MotorPlot.txt.Comment = Comentario:\n
-
-
-
-! Simulation plot panel
-simplotpanel.lbl.Presetplotconf = Configuración de la gráfica:
-simplotpanel.lbl.Xaxistype = Tipo de eje X:
-simplotpanel.lbl.Unit = Unidad:
-simplotpanel.lbl.Yaxistypes = Tipo de eje Y:
-simplotpanel.lbl.Flightevents = Eventos del vuelo:
-simplotpanel.but.All = Todo
-simplotpanel.but.None = Ninguno
-simplotpanel.but.NewYaxisplottype = Añadir nuevo eje Y en la gráfica
-simplotpanel.but.Plotflight = Ver gráfica
-simplotpanel.lbl.Axis = Ejes:
-simplotpanel.but.ttip.Removethisplot = Eliminar esta curva
-simplotpanel.Desc = Si no hay línea de tiempo, los datos aparecerán en el eje X según el instante en que se producen.
-simplotpanel.OptionPane.lbl1 = Se permite un máximo de 15 impresiones
-simplotpanel.OptionPane.lbl2 = No puede añadirse la curva
-simplotpanel.AUTO_NAME = Auto
-simplotpanel.LEFT_NAME = Izquierda
-simplotpanel.RIGHT_NAME = Derecha
-simplotpanel.CUSTOM = Personalizado
-
-! Component add buttons
-compaddbuttons.Bodycompandfinsets = Componentes del fuselaje y aletas
-compaddbuttons.Nosecone = Ojiva
-compaddbuttons.Bodytube = Cuerpo\ntubular
-compaddbuttons.Transition = Transición
-compaddbuttons.Trapezoidal = Trapezoidal
-compaddbuttons.Elliptical = Elíptica
-compaddbuttons.Freeform = Forma libre
-compaddbuttons.Launchlug = Soporte\npara guía
-compaddbuttons.Innercomponent = Componentes internos
-compaddbuttons.Innertube = Tubo\ninterior
-compaddbuttons.Coupler = Acoplador
-compaddbuttons.Centeringring = Anillo\nde centrado
-compaddbuttons.Bulkhead = Disco\nde enganche
-compaddbuttons.Engineblock = Retén\nde motor
-compaddbuttons.Massobjects = Accesorios
-compaddbuttons.Parachute = Paracaídas
-compaddbuttons.Streamer = Banderola
-compaddbuttons.Shockcord = Tirante de\nsuspensión
-compaddbuttons.Masscomponent = Componente\nmasa
-compaddbuttons.Donotaskmeagain = No me pregunte de nuevo
-compaddbuttons.Selectcomppos = Seleccionar la posición del componente
-compaddbuttons.lbl.Youcanchange = Puede cambiar la operación con las preferencias por defecto
-compaddbuttons.lbl.insertcomp = ¿Insertar el componente después del actual o al final?
-compaddbuttons.askPosition.Inserthere = Insertar aquí
-compaddbuttons.askPosition.Addtotheend = Añadir al final
-compaddbuttons.askPosition.Cancel = Cancelar
-
-! Component Analysis Dialog
-componentanalysisdlg.componentanalysis = Análisis de los componentes
-componentanalysisdlg.lbl.winddir = Dirección del viento:
-componentanalysisdlg.TitledBorder.warnings = Advertencias:
-componentanalysisdlg.ToggleBut.worst = Peor
-componentanalysisdlg.lbl.angleofattack = Ángulo de ataque:
-componentanalysisdlg.lbl.machnumber = Número Mach:
-componentanalysisdlg.lbl.rollrate = Valor de rotación:
-componentanalysisdlg.lbl.activestages = Etapas activas:
-componentanalysisdlg.lbl.motorconf = Configuración del Motor:
-componentanalysisdlg.TabStability.Col = Componente
-componentanalysisdlg.TabStability = Estabilidad
-componentanalysisdlg.TabStability.ttip = Información de Estabilidad
-componentanalysisdlg.dragTableModel.Col.Component = Componente
-componentanalysisdlg.dragTableModel.Col.Pressure = <html>Presión C<sub>D</sub>
-componentanalysisdlg.dragTableModel.Col.Base = <html>Base C<sub>D</sub>
-componentanalysisdlg.dragTableModel.Col.friction = <html>Rozamiento C<sub>D</sub>
-componentanalysisdlg.dragTableModel.Col.total = <html>Total C<sub>D</sub>
-componentanalysisdlg.dragTabchar = Características de rozamiento
-componentanalysisdlg.dragTabchar.ttip = Coeficientes de arrastre de los componentes.
-componentanalysisdlg.rollTableModel.Col.component = Componente
-componentanalysisdlg.rollTableModel.Col.rollforc = Coeficiente de rotación
-componentanalysisdlg.rollTableModel.Col.rolldamp = Coeficiente de corrección
-componentanalysisdlg.rollTableModel.Col.total = <html>Total C<sub>l</sub>
-componentanalysisdlg.rollTableModel = Dinámica de rotación
-componentanalysisdlg.rollTableModel.ttip = Dinámica del movimiento de rotación del cohete (spin)
-componentanalysisdlg.println.closingmethod = Llamar al método de cierre:
-componentanalysisdlg.println.settingnam = CONFIGURANDO VALORES NAN
-componentanalysisdlg.lbl.reflenght = Diámetro de referencia:
-componentanalysisdlg.lbl.refarea = Área de referencia:
-!componentanalysisdlg.But.close = Cerrar
-componentanalysisdlg.TabStability.Col.Component = Componente
-
-! Custom Material dialog
-custmatdlg.title.Custommaterial = Material hecho en casa
-custmatdlg.lbl.Materialname = Nombre del material:
-custmatdlg.lbl.Materialtype = Tipo de material:
-custmatdlg.lbl.Materialdensity = Densidad del material:
-custmatdlg.checkbox.Addmaterial = Agregar este material a la base de datos
-
-
-! Ring Component Config
-ringcompcfg.OuterRadius = Radio exterior:
-ringcompcfg.Automatic = Automático
-ringcompcfg.InnerRadius = Radio interior:
-ringcompcfg.Thickness = Espesor:
-ringcompcfg.Length = Longitud:
-ringcompcfg.Positionrelativeto = Posición relativa a:
-ringcompcfg.plus = Localización:
-ringcompcfg.PositionValue = Valor de posición:
-ringcompcfg.Radialdistance = Distancia radial:
-ringcompcfg.Distancefrom = Distancia desde la línea central del cohete:
-ringcompcfg.Radialdirection = Dirección radial:
-ringcompcfg.radialdirectionfrom = En dirección radial desde la línea central del cohete
-ringcompcfg.but.Reset = Reiniciar
-ringcompcfg.but.Resetcomponant = Reubicar el componente en la línea central del cohete
-ringcompcfg.EngineBlock.desc = <html>Un <b>retén de motor</b> impide que el motor se desplace hacia delante, por dentro del tubo porta motor.<br><br>Para añadir un motor, cree un <b>Cuerpo tubular</b> o <b>Tubo interior</b> y desígnelo como porta motor en el casillero <em>Motor</em>.
-ringcompcfg.note.desc = Nota: El tubo interior no afectará a la aerodinámica del cohete salvo que esté situado fuera del fuselaje.
-
-
-! Body Tube Config
-BodyTubecfg.lbl.Bodytubelength = Longitud del tubo:
-BodyTubecfg.lbl.Outerdiameter = Diámetro exterior:
-BodyTubecfg.lbl.Innerdiameter = Diámetro interior:
-BodyTubecfg.lbl.Wallthickness = Espesor de la pared:
-BodyTubecfg.tab.General = General
-BodyTubecfg.tab.Generalproperties = Propiedades generales
-BodyTubecfg.tab.Motor = Motor
-BodyTubecfg.tab.Motormountconf = Configuración del porta motor
-BodyTubecfg.checkbox.Automatic = Automático
-BodyTubecfg.checkbox.Filled = Sólido
-
-! FinSetConfig
-FinSetConfig.tab.Fintabs = Raíz de aleta
-FinSetConfig.tab.Through-the-wall = Parte de la aleta por dentro del fuselaje
-FinSetConfig.but.Converttofreeform = Convertir a forma libre
-FinSetConfig.but.Converttofreeform.ttip = Convertir esta forma de aleta a una forma libre
-FinSetConfig.Convertfinset = Convertir la configuración de aleta
-FinSetConfig.but.Splitfins = Separar las aletas
-FinSetConfig.but.Splitfins.ttip = Dividir la configuración de aleta en varias separadas
-FinSetConfig.lbl.Through-the-wall = Raíces de aleta a través de la pared:
-FinSetConfig.lbl.Tablength = Longitud de la raíz:
-FinSetConfig.ttip.Tablength = La longitud de la raíz de aleta.
-FinSetConfig.lbl.Tabheight = Altura de la raíz:
-FinSetConfig.ttip.Tabheight = Envergadura en altura de la raíz de aleta.
-FinSetConfig.lbl.Tabposition = Posición de la raíz:
-FinSetConfig.ttip.Tabposition = Posición de la raíz de aleta.
-FinSetConfig.lbl.relativeto = Relativo a
-
-! MotorDatabaseLoadingDialog
-MotorDbLoadDlg.title = Carga de motores
-MotorDbLoadDlg.Loadingmotors = Cargando motores...
-
-! RocketConfig
-RocketCfg.lbl.Designname = Nombre del proyecto:
-RocketCfg.lbl.Designer = Proyectista:
-RocketCfg.lbl.Comments = Comentarios:
-RocketCfg.lbl.Revisionhistory = Histórico de la revisión:
-RocketCfg.lbl.Material = Material:
-
-! ShockCordConfig
-ShockCordCfg.lbl.Shockcordlength = Longitud del tirante de suspensión
-
-! RocketComponentConfig
-RocketCompCfg.lbl.Componentname = Nombre del componente:
-RocketCompCfg.ttip.Thecomponentname = El nombre del componente.
-RocketCompCfg.tab.Override = Masa y CG
-RocketCompCfg.tab.MassandCGoverride = Especificar la Masa y el CG del componente.
-RocketCompCfg.tab.Figure = Estilo
-RocketCompCfg.tab.Figstyleopt = Opciones de estilo de la figura
-RocketCompCfg.tab.Comment = Comentarios
-RocketCompCfg.tab.Specifyacomment = Especifique un comentario para el componente
-RocketCompCfg.lbl.Mass = Masa:
-RocketCompCfg.lbl.Componentmass = Masa del componente:
-RocketCompCfg.lbl.overriddento = (Elegido para
-RocketCompCfg.lbl.overriddenby = (Elegido por
-RocketCompCfg.lbl.Componentmaterial = Material del componente:
-RocketCompCfg.lbl.Componentfinish = Acabado:
-RocketCompCfg.lbl.ttip.componentmaterialaffects = El material del componente afecta su peso.
-RocketCompCfg.combo.ttip.componentmaterialaffects = El material del componente afecta su peso.
-RocketCompCfg.lbl.longA1 = <html>El acabado del componente afecta a su coeficiente de rozamiento.<br>
-RocketCompCfg.lbl.longA2 = El valor indicado es el promedio de la rugosidad en altura de la superficie.
-RocketCompCfg.but.Setforall = Aplicar a todos
-RocketCompCfg.but.ttip.Setforall = Aplicar este acabado a todos los componentes del cohete.
-RocketCompCfg.lbl.Overridemassorcenter = Especificar la masa y el CG del componente
-RocketCompCfg.checkbox.Overridemass = Especificar la masa:
-RocketCompCfg.checkbox.Overridecenterofgrav = Especificar el CG:
-RocketCompCfg.checkbox.OverridemassandCG = Incluir la masa y el CG de todos los subcomponentes
-RocketCompCfg.lbl.longB1 = <html>En la masa especificada no se incluye la de los motores.<br>
-RocketCompCfg.lbl.longB2 = El CG se mide desde el extremo frontal del componente
-RocketCompCfg.lbl.Commentsonthe = Comentarios sobre
-RocketCompCfg.lbl.Figurestyle = Estilo de dibujo:
-RocketCompCfg.lbl.Componentcolor = Color del componente:
-RocketCompCfg.lbl.Choosecolor = Elija color
-RocketCompCfg.checkbox.Usedefaultcolor = Usar color por defecto
-RocketCompCfg.lbl.Complinestyle = Estilo de línea del componente:
-RocketCompCfg.but.Saveasdefstyle = Guardar como estilo por defecto
-RocketCompCfg.lbl.Diameter = Diámetro:
-RocketCompCfg.lbl.Length = Longitud:
-RocketCompCfg.lbl.Thickness = Espesor:
-RocketCompCfg.checkbox.Endcapped = Extremo truncado
-RocketCompCfg.ttip.Endcapped = Si el extremo del soporte está truncado.
-RocketCompCfg.title.Noseconeshoulder = Acople de la ojiva
-RocketCompCfg.title.Aftshoulder = Trasera del acople
-RocketCompCfg.border.Foreshoulder = Delantera del acople
-!RocketCompCfg.lbl.Length = Longitud:
-
-! BulkheadConfig
-BulkheadCfg.tab.Diameter = Diámetro:
-BulkheadCfg.tab.Thickness = Espesor:
-BulkheadCfg.tab.General = General
-BulkheadCfg.tab.Generalproperties = Propiedades generales
-
-!CenteringRingConfig
-CenteringRingCfg.tab.Outerdiam = Diámetro exterior:
-CenteringRingCfg.tab.Innerdiam = Diámetro interior:
-CenteringRingCfg.tab.Thickness = Espesor:
-CenteringRingCfg.tab.General = General
-CenteringRingCfg.tab.Generalproperties = Propiedades generales
-
-!ComponentConfigDialog
-ComponentCfgDlg.configuration =
-ComponentCfgDlg.configuration1 = Configuración
-ComponentCfgDlg.Modify = Modificar
-
-!EllipticalFinSetConfig
-EllipticalFinSetCfg.Nbroffins = Número de aletas:
-EllipticalFinSetCfg.Rotation = Rotación de las aletas:
-EllipticalFinSetCfg.Fincant = Inclinación de las aletas:
-EllipticalFinSetCfg.Rootchord = Longitud línea base:
-EllipticalFinSetCfg.Height = Altura:
-EllipticalFinSetCfg.Positionrelativeto = Posición relativa a:
-EllipticalFinSetCfg.plus = Localización:
-EllipticalFinSetCfg.FincrossSection = Borde de la aleta:
-EllipticalFinSetCfg.Thickness = Espesor:
-EllipticalFinSetCfg.General = General
-EllipticalFinSetCfg.Generalproperties = Propiedades generales
-EllipticalFinSetCfg.ttip.Fincant = El ángulo de inclinación de las aletas respecto al eje central del fuselaje.
-
-!FreeformFinSetConfig
-FreeformFinSetCfg.tab.General = General
-FreeformFinSetCfg.tab.ttip.General = Propiedades generales
-FreeformFinSetCfg.tab.Shape = Forma
-FreeformFinSetCfg.tab.ttip.Finshape = Forma de la aleta
-FreeformFinSetCfg.lbl.Numberoffins = Número de aletas:
-FreeformFinSetCfg.lbl.Finrotation = Rotación de las aletas:
-FreeformFinSetCfg.lbl.Fincant = Inclinación de las aletas:
-FreeformFinSetCfg.lbl.ttip.Fincant = El ángulo de inclinación de las aletas respecto al eje central del fuselaje.
-FreeformFinSetCfg.lbl.Posrelativeto = Posición relativa a:
-FreeformFinSetCfg.lbl.plus = Localización:
-FreeformFinSetCfg.lbl.FincrossSection = Borde de la aleta:
-FreeformFinSetCfg.lbl.Thickness = Espesor:
-!DobleClic 1 + 2 en el mensaje "Doble-Click para editar", corta aproximadamente por la mitad
-FreeformFinSetCfg.lbl.doubleClick1 = Doble Click en la lista
-FreeformFinSetCfg.lbl.doubleClick2 = para editar
-FreeformFinSetCfg.lbl.clickDrag = Click (sobre línea)+arrastrar: Agregar punto
-FreeformFinSetCfg.lbl.ctrlClick = Control+Click (sobre punto): Eliminar punto
-
-
-!InnerTubeConfig
-InnerTubeCfg.tab.Motor = Motor
-InnerTubeCfg.tab.ttip.Motor = Configuración del porta motor
-InnerTubeCfg.tab.Cluster = Cluster
-InnerTubeCfg.tab.ttip.Cluster = Configuración del cluster
-InnerTubeCfg.tab.Radialpos = Posición radial
-InnerTubeCfg.tab.ttip.Radialpos = Posición radial
-InnerTubeCfg.lbl.Selectclustercfg = Elija la configuración del cluster:
-InnerTubeCfg.lbl.TubeSep = Separación del tubo:
-InnerTubeCfg.lbl.ttip.TubeSep = Una separación de los tubos con valor 1.0 indica que están tocándose unos con otros
-InnerTubeCfg.lbl.Rotation = Rotación:
-InnerTubeCfg.lbl.ttip.Rotation = Configuración del ángulo de rotación del cluster
-InnerTubeCfg.lbl.Rotangle = Angulo de rotación del cluster
-InnerTubeCfg.but.Splitcluster = Tubos independientes
-InnerTubeCfg.lbl.longA1 = <html>Separar los tubos del cluster para convertirlos en componentes internos independientes.<br>
-InnerTubeCfg.lbl.longA2 = Esto también duplica todos los componentes unidos a este tubo interior.
-InnerTubeCfg.but.Resetsettings = Reiniciar configuración
-InnerTubeCfg.but.ttip.Resetsettings = Reiniciar la separación y la rotación con los valores predeterminados
-
-! LaunchLugConfig
-LaunchLugCfg.lbl.Length = Longitud:
-LaunchLugCfg.lbl.Outerdiam = Diámetro exterior:
-LaunchLugCfg.lbl.Innerdiam = Diámetro interior:
-LaunchLugCfg.lbl.Thickness = Espesor:
-LaunchLugCfg.lbl.Radialpos = Posición radial:
-LaunchLugCfg.lbl.Posrelativeto = Posición relativa a:
-LaunchLugCfg.lbl.plus = Localización:
-LaunchLugCfg.tab.General = General
-LaunchLugCfg.tab.Generalprop = Propiedades generales
-
-! MassComponentConfig
-MassComponentCfg.lbl.Mass = Masa:
-MassComponentCfg.lbl.Length = Longitud:
-MassComponentCfg.lbl.Diameter = Diámetro:
-MassComponentCfg.lbl.PosRelativeto = Posición relativa a:
-MassComponentCfg.lbl.plus = Localización:
-MassComponentCfg.tab.General = General
-MassComponentCfg.tab.ttip.General = Propiedades generales
-MassComponentCfg.tab.Radialpos = Posición radial
-MassComponentCfg.tab.ttip.Radialpos = Configuración de la posición radial
-MassComponentCfg.lbl.Radialdistance = Distancia radial:
-MassComponentCfg.lbl.Radialdirection = Dirección radial:
-MassComponentCfg.but.Reset = Reiniciar
-
-! MotorConfig
-MotorCfg.checkbox.compmotormount = Este componente es un porta motor
-MotorCfg.lbl.Motorcfg = Configuración del motor:
-MotorCfg.but.New = Nuevo
-MotorCfg.lbl.Currentmotor = Motor actual:
-MotorCfg.lbl.Motoroverhang = Sobresalida del motor:
-MotorCfg.lbl.Ignitionat = Encendido en:
-MotorCfg.lbl.plus = Retardo:
-MotorCfg.lbl.seconds = segundos.
-MotorCfg.lbl.longA1 = El diseño actual tiene una sola etapa.
-MotorCfg.lbl.longA2 = Pueden agregarse etapas haciendo Click en \"Nueva etapa\".
-MotorCfg.lbl.longB1 = El diseño actual tiene
-MotorCfg.lbl.longB2 = etapas.
-MotorCfg.but.Selectmotor = Seleccionar motor
-MotorCfg.but.Removemotor = Quitar motor
-MotorCfg.lbl.motorLabel = Ninguno
-
-! NoseConeConfig
-NoseConeCfg.lbl.Noseconeshape = Forma:
-NoseConeCfg.lbl.Shapeparam = Valor de forma:
-NoseConeCfg.lbl.Noseconelength = Longitud:
-NoseConeCfg.lbl.Basediam = Diámetro de la base:
-NoseConeCfg.checkbox.Automatic = Automático
-NoseConeCfg.lbl.Wallthickness = Espesor de la pared:
-NoseConeCfg.checkbox.Filled = Sólido
-NoseConeCfg.tab.General = General
-NoseConeCfg.tab.ttip.General = Propiedades generales
-NoseConeCfg.tab.Shoulder = Acoplamiento
-NoseConeCfg.tab.ttip.Shoulder = Propiedades del acople
-
-! ParachuteConfig
-ParachuteCfg.lbl.Canopy = Pabellón
-ParachuteCfg.lbl.Diameter = Diámetro:
-ParachuteCfg.lbl.Material = Material:
-ParachuteCfg.combo.MaterialModel = El material del componente afecta a su peso.
-ParachuteCfg.lbl.longA1 = <html>Coeficiente de arrastre C<sub>D</sub>:
-ParachuteCfg.lbl.longB1 = <html>Coeficiente de rozamiento relativo al área total del paracaídas.<br>
-ParachuteCfg.lbl.longB2 = Un mayor coeficiente de rozamiento genera un valor de descenso más lento.
-ParachuteCfg.lbl.longB3 = Un valor típico para los paracaídas es 0,8.
-ParachuteCfg.but.Reset = Reiniciar
-ParachuteCfg.lbl.Shroudlines = Cuerdas:
-ParachuteCfg.lbl.Numberoflines = Número de cuerdas:
-ParachuteCfg.lbl.Linelength = Longitud de cuerda:
-ParachuteCfg.lbl.Material = Material:
-ParachuteCfg.lbl.Posrelativeto = Posición relativa a:
-ParachuteCfg.lbl.plus = Localización:
-ParachuteCfg.lbl.Packedlength = Longitud empaquetado:
-ParachuteCfg.lbl.Packeddiam = Diámetro del empaquetado:
-ParachuteCfg.lbl.Deploysat = Despliegue en:
-ParachuteCfg.lbl.seconds = segundos.
-ParachuteCfg.lbl.Altitude = Altitud:
-ParachuteCfg.tab.General = General
-ParachuteCfg.tab.ttip.General = Propiedades generales
-ParachuteCfg.tab.Radialpos = Posición radial
-ParachuteCfg.tab.ttip.Radialpos = Configuración de la posición radial
-ParachuteCfg.lbl.Radialdistance = Distancia radial:
-ParachuteCfg.lbl.Radialdirection = Dirección radial:
-ParachuteCfg.but.Reset = Reiniciar
-ParachuteCfg.lbl.plusdelay = Retardo:
-
-
-! ShockCordConfig
-ShockCordCfg.lbl.Shockcordlength = Longitud del tirante de suspensión
-ShockCordCfg.lbl.Shockcordmaterial = Material del tirante de suspensión:
-ShockCordCfg.lbl.Posrelativeto = Posición relativa a:
-ShockCordCfg.lbl.plus = Localización:
-ShockCordCfg.lbl.Packedlength = Longitud del empaquetado:
-ShockCordCfg.lbl.Packeddiam = Diámetro del empaquetado:
-ShockCordCfg.tab.General = General
-ShockCordCfg.tab.ttip.General = Propiedades generales
-
-!SleeveConfig
-SleeveCfg.tab.Outerdiam = Diámetro exterior:
-SleeveCfg.tab.Innerdiam = Diámetro interior:
-SleeveCfg.tab.Wallthickness = Espesor de la pared:
-SleeveCfg.tab.Length = Longitud:
-SleeveCfg.tab.General = General
-SleeveCfg.tab.Generalproperties = Propiedades generales
-
-! StreamerConfig
-StreamerCfg.lbl.Striplength = Longitud de la cinta:
-StreamerCfg.lbl.Stripwidth = Ancho de la cinta:
-StreamerCfg.lbl.Striparea = Área de la cinta:
-StreamerCfg.lbl.Aspectratio = Relación de aspecto:
-StreamerCfg.lbl.Material = Material:
-StreamerCfg.combo.ttip.MaterialModel = El material del componente afecta a su peso.
-StreamerCfg.lbl.longA1 = <html>Coeficiente de rozamiento C<sub>D</sub>:
-StreamerCfg.lbl.longB1 = <html>Coeficiente de rozamiento relativo al área total de la banderola.<br>
-StreamerCfg.lbl.longB2 = Un mayor coeficiente de rozamiento genera un valor de descenso más lento.
-StreamerCfg.lbl.Automatic = Automático
-StreamerCfg.lbl.longC1 = El coeficiente de rozamiento depende del área de la banderola.
-StreamerCfg.lbl.Posrelativeto = Posición relativa a:
-StreamerCfg.lbl.plus = Localización:
-StreamerCfg.lbl.Packedlength = Longitud de empaquetado:
-StreamerCfg.lbl.Packeddiam = Diámetro de empaquetado:
-StreamerCfg.lbl.Deploysat = Despliegue en:
-StreamerCfg.lbl.seconds = segundos.
-StreamerCfg.lbl.Altitude = Altitud:
-StreamerCfg.tab.General = General
-StreamerCfg.tab.ttip.General = Propiedades generales
-StreamerCfg.tab.Radialpos = Posición radial
-StreamerCfg.tab.ttip.Radialpos = Configuración de posición radial
-StreamerCfg.lbl.Radialdistance = Distancia radial:
-StreamerCfg.lbl.Radialdirection = Dirección radial:
-StreamerCfg.but.Reset = Reiniciar
-StreamerCfg.lbl.plusdelay = Retardo:
-
-! ThicknessRingComponentConfig
-ThicknessRingCompCfg.tab.Outerdiam = Diámetro exterior:
-ThicknessRingCompCfg.tab.Innerdiam = Diámetro Interior:
-ThicknessRingCompCfg.tab.Wallthickness = Espesor de la pared:
-ThicknessRingCompCfg.tab.Length = Longitud:
-ThicknessRingCompCfg.tab.General = General
-ThicknessRingCompCfg.tab.Generalprop = Propiedades generales
-
-! TransitionConfig
-TransitionCfg.lbl.Transitionshape = Forma de la transición:
-TransitionCfg.checkbox.Clipped = Acortado
-TransitionCfg.lbl.Shapeparam = Valor de forma:
-TransitionCfg.lbl.Transitionlength = Longitud de la transición:
-TransitionCfg.lbl.Forediam = Diámetro delantero:
-TransitionCfg.checkbox.Automatic = Automático
-TransitionCfg.lbl.Aftdiam = Diámetro trasero:
-TransitionCfg.lbl.Wallthickness = Espesor de la pared:
-TransitionCfg.checkbox.Filled = Sólido
-TransitionCfg.tab.General = General
-TransitionCfg.tab.Generalproperties = Propiedades generales
-TransitionCfg.tab.Shoulder = Acoplamiento
-TransitionCfg.tab.Shoulderproperties = Propiedades del acople
-
-! TrapezoidFinSetConfig
-TrapezoidFinSetCfg.lbl.Nbroffins = Número de aletas:
-TrapezoidFinSetCfg.lbl.ttip.Nbroffins = Número de aletas en la base de aletas.
-TrapezoidFinSetCfg.lbl.Finrotation = Rotación de las aletas:
-TrapezoidFinSetCfg.lbl.ttip.Finrotation = Posición de las aletas alrededor del fuselaje.
-TrapezoidFinSetCfg.lbl.Fincant = Inclinación de las aletas:
-TrapezoidFinSetCfg.lbl.ttip.Fincant = El ángulo de inclinación de las aletas respecto al eje central del fuselaje.
-TrapezoidFinSetCfg.lbl.Rootchord = Longitud de la línea base:
-TrapezoidFinSetCfg.lbl.Tipchord = Longitud del borde superior:
-TrapezoidFinSetCfg.lbl.Height = Altura:
-TrapezoidFinSetCfg.lbl.Sweeplength = Desplazamiento borde superior:
-TrapezoidFinSetCfg.lbl.Sweepangle = Ángulo del borde de ataque:
-TrapezoidFinSetCfg.lbl.FincrossSection = Borde de la aleta:
-TrapezoidFinSetCfg.lbl.Thickness = Espesor:
-TrapezoidFinSetCfg.lbl.Posrelativeto = Posición relativa a:
-TrapezoidFinSetCfg.lbl.plus = Localización:
-TrapezoidFinSetCfg.tab.General = General
-TrapezoidFinSetCfg.tab.Generalproperties = Propiedades generales
-
-!MotorConfigurationModel
-MotorCfgModel.Editcfg = Editar configuraciones
-
-! StorageOptionChooser
-StorageOptChooser.lbl.Simdatatostore = Almacenar datos simulados
-StorageOptChooser.rdbut.Allsimdata = Todos los datos simulados
-StorageOptChooser.lbl.longA1 = <html>Almacenar todos los datos simulados.<br>
-StorageOptChooser.lbl.longA2 = puede generar archivos muy grandes
-StorageOptChooser.rdbut.Every = Cada
-StorageOptChooser.lbl.longB1 = <html>Almacenar los valores de impresión de este apartado.<br>
-StorageOptChooser.lbl.longB2 = Genera valores grandes en archivos más pequeños.
-StorageOptChooser.lbl.seconds = Segundos
-StorageOptChooser.rdbut.Onlyprimfig = Sólo figuras principales
-StorageOptChooser.lbl.longC1 = <html>Almacenar sólo los valores en la tabla resumen.<br>
-StorageOptChooser.lbl.longC2 = Estos resultados se guardan en archivos mas pequeños.
-StorageOptChooser.checkbox.Compfile = Archivo comprimido
-StorageOptChooser.lbl.UsingComp = Usando la compresión reducimos el tamaño de los archivos.
-StorageOptChooser.lbl.longD1 = Una estimación de cuan grande será un archivo podría tenerse con las presentes opciones.
-StorageOptChooser.ttip.Saveopt = Guardar opciones
-StorageOptChooser.lbl.Estfilesize = Estimación del tamaño del archivo:
-StorageOptChooser.lbl.Saveopt = Guardar opciones
-
-! ThrustCurveMotorSelectionPanel
-TCMotorSelPan.lbl.Selrocketmotor = Seleccione el motor del cohete:
-TCMotorSelPan.checkbox.hideSimilar = Borrar las curvas muy similares
-TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Mostrar todos los motores
-TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Mostrar motores con diámetro inferior al del tubo portamotor
-TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Mostrar motores con diámetro igual al del tubo portamotor
-TCMotorSelPan.lbl.Motormountdia = Diámetro del portamotor:
-TCMotorSelPan.lbl.Search = Buscar:
-TCMotorSelPan.lbl.Selectthrustcurve = Seleccione curva de empuje:
-TCMotorSelPan.lbl.Ejectionchargedelay = Retardo de la carga de eyección:
-TCMotorSelPan.equalsIgnoreCase.None = Ninguno
-TCMotorSelPan.lbl.NumberofsecondsorNone = (Número de segundos o \"Ninguno\")
-TCMotorSelPan.lbl.Totalimpulse = Impulso total:
-TCMotorSelPan.lbl.Avgthrust = Empuje medio:
-TCMotorSelPan.lbl.Maxthrust = Empuje máximo:
-TCMotorSelPan.lbl.Burntime = Tiempo de quemado:
-TCMotorSelPan.lbl.Launchmass = Masa total:
-TCMotorSelPan.lbl.Emptymass = Masa carcasa:
-TCMotorSelPan.lbl.Datapoints = Datos de los puntos:
-TCMotorSelPan.lbl.Digest = Resumen:
-TCMotorSelPan.title.Thrustcurve = Curva de empuje:
-TCMotorSelPan.title.Thrust = Empuje
-TCMotorSelPan.delayBox.None = Ninguno
-
-
-! PlotDialog
-PlotDialog.title.Flightdataplot = Representar los datos de vuelo
-PlotDialog.Chart.Simulatedflight = Vuelo simulado
-PlotDialog.CheckBox.Showdatapoints = Mostrar los datos de los puntos
-PlotDialog.lbl.Chart = Click+bajar el rozamiento+derecha ampliar, arriba+izquierda disminuir
-
-
-! "main" prefix is used for the main application dialog
-
-# FIXME: Rename the description keys
-
-main.menu.file = Archivo
-main.menu.file.desc = Tareas relacionadas con el manejo de archivos
-main.menu.file.new = Nuevo
-main.menu.file.new.desc = Crear un nuevo diseño de cohete
-main.menu.file.open = Abrir ...
-BasicFrame.item.Openrocketdesign = Abrir un diseño de cohete
-main.menu.file.openExample = Abrir ejemplo ...
-BasicFrame.item.Openexamplerocketdesign = Abrir un ejemplo de diseño de cohete
-main.menu.file.save = Guardar
-BasicFrame.item.SavecurRocketdesign = Guardar el diseño actual
-main.menu.file.saveAs = Guardar como ...
-BasicFrame.item.SavecurRocketdesnewfile = Guardar el diseño actual como un nuevo documento
-main.menu.file.print = Imprimir ...
-BasicFrame.item.Printpart = Imprimir un listado de componentes y un esquema de aleta
-main.menu.file.close = Cerrar
-BasicFrame.item.Closedesign = Cerrar el diseño actual
-main.menu.file.quit = Salir
-BasicFrame.item.Quitprogram = Salir del programa
-
-main.menu.edit = Edición
-BasicFrame.menu.Rocketedt = Mostrar el cohete
-main.menu.edit.undo = Deshacer
-main.menu.edit.undo.desc = Deshacer la operación anterior
-main.menu.edit.redo = Rehacer
-main.menu.edit.redo.desc = Rehacer la operación anterior
-main.menu.edit.cut = Cortar
-main.menu.edit.copy = Copiar
-main.menu.edit.paste = Pegar
-main.menu.edit.delete = Borrar
-main.menu.edit.resize = Dimensionar...
-main.menu.edit.resize.desc = Dimensionar las partes del diseño del cohete
-main.menu.edit.preferences = Preferencias
-main.menu.edit.preferences.desc = Configurar las preferencias de la aplicación
-
-main.menu.analyze = Analizar
-main.menu.analyze.desc = Análisis del cohete
-main.menu.analyze.componentAnalysis = Análisis de los componentes
-main.menu.analyze.componentAnalysis.desc = Analiza los componentes del cohete por separado
-main.menu.analyze.optimization = Optimización del diseño
-main.menu.analyze.optimization.desc = Optimización global del diseño del cohete
-main.menu.help = Ayuda
-main.menu.help.desc = Información acerca del cohete
-main.menu.help.license = Licencia
-main.menu.help.license.desc = Información de la licencia de OpenRocket
-main.menu.help.bugReport = Informe de errores
-main.menu.help.bugReport.desc = Informar sobre errores encontrados en OpenRocket
-main.menu.help.debugLog = Registro de sucesos
-main.menu.help.debugLog.desc = Visualizar el registro de depuración de OpenRocket
-main.menu.help.about = Acerca de
-main.menu.help.about.desc = Detalles del Copyright de OpenRocket
-
-main.menu.debug = Recuperación
-main.menu.debug.whatisthismenu = ¿Que es este menú?
-main.menu.debug.createtestrocket = Crear una prueba de modelo
-
-! database
-! Translate here all material database
-!
-
-! Material database
-! BULK_MATERIAL
-Databases.materials.Acrylic = Acrílico
-Databases.materials.Balsa = Balsa
-Databases.materials.Birch = Abedul
-Databases.materials.Cardboard = Cartón
-Databases.materials.Carbonfiber = Fibra de Carbono
-Databases.materials.Cork = Corcho
-Databases.materials.DepronXPS = Depron (XPS)
-Databases.materials.Fiberglass = Fibra de vidrio
-Databases.materials.Kraftphenolic = Cartón fenólico
-Databases.materials.Maple = Arce
-Databases.materials.Paperoffice = Papel (oficina)
-Databases.materials.Pine = Pino
-Databases.materials.Plywoodbirch = Contrachapado
-Databases.materials.PolycarbonateLexan = Policarbonato (Lexan)
-Databases.materials.Polystyrene = Poliestireno
-Databases.materials.PVC = PVC
-Databases.materials.Spruce = Pícea (Abeto común)
-Databases.materials.StyrofoamgenericEPS = Porex (generico EPS)
-Databases.materials.StyrofoamBluefoamXPS = Porex \"Foam azul\" (XPS)
-Databases.materials.Quantumtubing = Quantum tubing
-Databases.materials.BlueTube = Tubo azul (PML)
-!SURFACE_MATERIAL
-Databases.materials.Ripstopnylon = Ripstop nylon
-Databases.materials.Mylar = Mylar
-Databases.materials.Polyethylenethin = Polietileno (delgado)
-Databases.materials.Polyethyleneheavy = Polietileno (grueso)
-Databases.materials.Silk = Seda
-Databases.materials.Paperoffice = Papel (oficina)
-Databases.materials.Cellophane = Celofán
-Databases.materials.Crepepaper = Crespón de papel
-! LINE_MATERIAL
-Databases.materials.Threadheavy-duty = Trenzado (Alta resistencia)
-Databases.materials.Elasticcordround2mm = Cordón elástico (aprox. 2mm, 1/16 in)
-Databases.materials.Elasticcordflat6mm = Cordón elástico plano (6mm, 1/4 in)
-Databases.materials.Elasticcordflat12mm = Cordón elástico plano (12mm, 1/2 in)
-Databases.materials.Elasticcordflat19mm = Cordón elástico plano (19mm, 3/4 in)
-Databases.materials.Elasticcordflat25mm = Cordón elástico plano (25mm, 1 in)
-Databases.materials.Braidednylon2mm = Nylon trenzado (2 mm, 1/16 in)
-Databases.materials.Braidednylon3mm = Nylon trenzado (3 mm, 1/8 in)
-Databases.materials.Tubularnylon11mm = Nylon tubular (11 mm, 7/16 in)
-Databases.materials.Tubularnylon14mm = Nylon tubular (14 mm, 9/16 in)
-Databases.materials.Tubularnylon25mm = Nylon tubular (25 mm, 1 in)
-
-! ExternalComponent
-ExternalComponent.Rough = Rugoso
-ExternalComponent.Unfinished = Inacabado
-ExternalComponent.Regularpaint = Pintura normal
-ExternalComponent.Smoothpaint = Pintura fina
-ExternalComponent.Polished = Pulido
-
-! LineStyle
-LineStyle.Solid = Sólido
-LineStyle.Dashed = Discontinuo
-LineStyle.Dotted = Punteado
-LineStyle.Dash-dotted = Discontinuo con puntos
-LineStyle.Defaultstyle = Estilo por defecto
-
-! Shape
-Shape.Conical = Cónico
-Shape.Conical.desc1 = Una ojiva cónica de perfil triangular
-Shape.Conical.desc2 = Transición cónica de lados rectos
-Shape.Ogive = Ojival
-Shape.Ogive.desc1 = Ojiva con perfil de arco de circunferencia. Un valor de forma igual a 1 produce una <b>Ojiva tangente</b>, mientras que un valor inferior a 1 produce una <b>Ojiva secante</b> con un perfil más afilado.
-Shape.Ogive.desc2 = Transición con perfil de arco de circunferencia. Un valor de forma igual a 1 produce una <b>Transición tangente</b>, mientras que un valor inferior a 1 produce una <b>Transición secante</b> con un perfil más afilado.
-Shape.Ellipsoid = Elíptica
-Shape.Ellipsoid.desc1 = Ojiva con perfil de media elipse. Por defecto, una elipse de <i>longitud</i> igual al triple de su <i>diámetro</i>.
-Shape.Ellipsoid.desc2 = Transición con perfil de media elipse. Por defecto, una elipse de <i>longitud</i> igual al triple de su <i>diámetro</i>.
-Shape.Powerseries = Serie potencial
-Shape.Powerseries.desc1 = Ojiva cuyo perfil es una curva obtenida a partir de una función potencial f(<i>x</i>)<sup><i>k</i></sup>. Un valor de forma k=0.5 produce una ojiva con perfil de parábola, para k=0.75 se produce una ojiva con <b>perfil potencial</b>, y para k=1 se produce una ojiva con perfil recto u <b>Ojiva cónica</b>.
-Shape.Powerseries.desc2 = Transición cuyo perfil es una curva obtenida a partir de una función potencial de <i>Radio</i> =; (<i>x</i> / <i>L</i>)<sup><i>k</i></sup> donde <i>k</i> es el parámetro de forma. Para <i>k</i>=0.5 la transición es <b>\u00BD-potencial</b> o <b>parabólica</b>, para <i>k</i>=0.75 a <b>\u00BE-potencia</b>, y para <i>k</i>=1 <b>cónica</b>.
-Shape.Parabolicseries = Serie parabólica
-Shape.Parabolicseries.desc1 = Ojiva con perfil de arco de parábola. Un valor de forma igual a 1 produce una <b>Ojiva tangente</b>, un valor igual a 0.75 produce una <b>parábola de 3/4</b>, un valor igual a 0.5 produce una <b>parábola de 1/2</b>, y un valor igual a 0 produce un perfil recto u <b>Ojiva cónica</b>.
-Shape.Parabolicseries.desc2 = Una transición de serie parabólica tiene un perfil de parábola. El valor de forma defien el tipo de parábola a utilizar. Un valor de forma de 1.0 produce una parábola completa que es tangente al cuerpo tubular en el extremo trasero, un valor de 0.75 produce una <b>parábola de 3/4</b>, un valor de 0.5 produce una <b>parábola de 1/2</b>, y un valor de 0 produce una transición cónica.
-Shape.Haackseries = Haack series
-Shape.Haackseries.desc1 = Ojiva con perfil de mínimo arrastre aerodinámico recomendado para vuelos supersónicos. Un valor de forma igual a 0 produce una <b>Ojiva LD Haack</b> u <b>Ojiva Von Karman</b> que minimiza el arrastre aerodinámico para una determinada longitud y diámetro de la base, mientras que un valor igual a 0.333 produce una <b>Ojiva LV-Haack</b> que minimiza el arrastre aerodinámico para una determinada longitud y volumen de la ojiva.
-Shape.Haackseries.desc2 = Las transiciones Haack series están diseñadas para minimizar el arrastre aerodinámico. Estas transiciones poseen sus equivalentes, pero no necesariamente producen un arrastre óptimo. Un valor de forma 0 produce una transición <b>LD-Haack</b> o <b>Von Karman</b>, mientras que un valor de 0.333 produce una forma <b>LV-Haack</b>.
-
-
-! RocketComponent
-RocketComponent.Position.TOP = Parte superior del componente
-RocketComponent.Position.MIDDLE = Parte media del componente
-RocketComponent.Position.BOTTOM = Extremo inferior del componente
-RocketComponent.Position.AFTER = Después del componente
-RocketComponent.Position.ABSOLUTE = Extremo de la ojiva
-
-! LaunchLug
-LaunchLug.Launchlug = Soporte para Guía
-! NoseCone
-NoseCone.NoseCone = Ojiva
-! Transition
-Transition.Transition = Transición
-!Stage
-Stage.Stage = Etapa
-! BodyTube
-BodyTube.BodyTube = Cuerpo tubular
-! TubeCoupler
-TubeCoupler.TubeCoupler = Acoplador
-!InnerTube
-InnerTube.InnerTube = Tubo interior
-! TrapezoidFinSet
-TrapezoidFinSet.TrapezoidFinSet = Aleta trapezoidal
-! FreeformFinSet
-FreeformFinSet.FreeformFinSet = Aleta de forma libre
-!MassComponent
-MassComponent.MassComponent = Masa
-! Parachute
-Parachute.Parachute = Paracaídas
-! ShockCord
-ShockCord.ShockCord = Tirante de suspensión
-! Bulkhead
-Bulkhead.Bulkhead = Disco de enganche
-
-!Rocket
-Rocket.motorCount.Nomotor = [Sin motores]
-Rocket.compname.Rocket = Cohete
-
-!MotorMount
-MotorMount.IgnitionEvent.AUTOMATIC = Automático (Lanzamiento o carga de eyección)
-MotorMount.IgnitionEvent.LAUNCH = Lanzamiento
-MotorMount.IgnitionEvent.EJECTION_CHARGE = Primera carga de eyección de la etapa previa
-MotorMount.IgnitionEvent.BURNOUT = Primer encendido de la etapa previa
-MotorMount.IgnitionEvent.NEVER = Nunca
-
-!ComponentIcons
-ComponentIcons.Nosecone = Ojiva
-ComponentIcons.Bodytube = Cuerpo tubular
-ComponentIcons.Transition = Transición
-ComponentIcons.Trapezoidalfinset = Aleta trapezoidal
-ComponentIcons.Ellipticalfinset = Aleta elíptica
-ComponentIcons.Freeformfinset = Aleta de forma libre
-ComponentIcons.Launchlug = Tubo para Guía
-ComponentIcons.Innertube = Tubo interior
-ComponentIcons.Tubecoupler = Tubo de acoplamiento
-ComponentIcons.Centeringring = Anillo de centrado
-ComponentIcons.Bulkhead = Disco de enganche
-ComponentIcons.Engineblock = Retén de motor
-ComponentIcons.Parachute = Paracaídas
-ComponentIcons.Streamer = Banderola
-ComponentIcons.Shockcord = Tirante de suspensión
-ComponentIcons.Masscomponent = Componente masa
-ComponentIcons.disabled = (Desconectado)
-
-! StageAction
-StageAction.Stage = Etapa
-
-! RecoveryDevice
-RecoveryDevice.DeployEvent.LAUNCH = Lanzamiento (NN segundos)
-RecoveryDevice.DeployEvent.EJECTION = Primera carga de eyección de esta etapa
-RecoveryDevice.DeployEvent.APOGEE = Apogeo
-RecoveryDevice.DeployEvent.ALTITUDE = Altura específica durante el descenso
-RecoveryDevice.DeployEvent.NEVER = Nunca
-
-! FlightEvent
-FlightEvent.Type.LAUNCH = Lanzamiento
-FlightEvent.Type.IGNITION = Encendido del motor
-FlightEvent.Type.LIFTOFF = Despegue
-FlightEvent.Type.LAUNCHROD = Abandono de la Guía de lanzamiento
-FlightEvent.Type.BURNOUT = Apagado del motor
-FlightEvent.Type.EJECTION_CHARGE = Carga de eyección
-FlightEvent.Type.STAGE_SEPARATION = Separación de etapa
-FlightEvent.Type.APOGEE = Apogeo
-FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Despliegue del sistema de recuperación
-FlightEvent.Type.GROUND_HIT = Contacto con el suelo
-FlightEvent.Type.SIMULATION_END = Fin de la simulación
-FlightEvent.Type.ALTITUDE = Altitud
-
-! ThrustCurveMotorColumns
-TCurveMotorCol.MANUFACTURER = Fabricante
-TCurveMotorCol.DESIGNATION = Designación
-TCurveMotorCol.TYPE = Tipo
-TCurveMotorCol.DIAMETER = Diámetro
-TCurveMotorCol.LENGTH = Longitud
-
-! RocketInfo
-RocketInfo.lengthLine.Length = Longitud
-RocketInfo.lengthLine.maxdiameter = Diámetro máximo
-RocketInfo.massText1 = Masa con motores
-RocketInfo.massText2 = Masa sin motores
-RocketInfo.at = a M=
-RocketInfo.cgText = CG:
-RocketInfo.cpText = CP:
-RocketInfo.stabText = Estabilidad:
-RocketInfo.Warning = Peligro, cohete inestable.
-RocketInfo.Calculating = Calculando...
-RocketInfo.Apogee = Apogeo:
-RocketInfo.Maxvelocity = Velocidad Máx.:
-RocketInfo.Maxacceleration = Aceleración Máx.:
-RocketInfo.apogeeValue = N/A
-RocketInfo.Mach = Número Mach.
-RocketInfo.velocityValue = N/A
-RocketInfo.accelerationValue = N/A
-
-! FinSet
-FinSet.CrossSection.SQUARE = Cuadrado
-FinSet.CrossSection.ROUNDED = Redondeado
-FinSet.CrossSection.AIRFOIL = Aerodinámico
-FinSet.TabRelativePosition.FRONT = Borde principal del extremo de anclaje
-FinSet.TabRelativePosition.CENTER = Borde principal del anclaje
-FinSet.TabRelativePosition.END = Borde principal de tracción
-
-! FlightDataType
-FlightDataType.TYPE_TIME = Tiempo
-FlightDataType.TYPE_ALTITUDE = Altitud
-FlightDataType.TYPE_VELOCITY_Z = Velocidad vertical
-FlightDataType.TYPE_ACCELERATION_Z = Aceleración vertical
-FlightDataType.TYPE_VELOCITY_TOTAL = Velocidad total
-FlightDataType.TYPE_ACCELERATION_TOTAL = Aceleración total
-FlightDataType.TYPE_POSITION_X = Posición contra el viento
-FlightDataType.TYPE_POSITION_Y = Posición a favor del viento
-FlightDataType.TYPE_POSITION_XY = Distancia lateral
-FlightDataType.TYPE_POSITION_DIRECTION = Dirección lateral
-FlightDataType.TYPE_VELOCITY_XY = Velocidad lateral
-FlightDataType.TYPE_ACCELERATION_XY = Aceleración lateral
-FlightDataType.TYPE_AOA = Ángulo de ataque
-FlightDataType.TYPE_ROLL_RATE = Relación de rotación
-FlightDataType.TYPE_PITCH_RATE = Relación de pico
-FlightDataType.TYPE_YAW_RATE = Relación de desvío
-FlightDataType.TYPE_MASS = Masa
-FlightDataType.TYPE_LONGITUDINAL_INERTIA = Momento de inercia longitudinal
-FlightDataType.TYPE_ROTATIONAL_INERTIA = Momento de inercia rotacional
-FlightDataType.TYPE_CP_LOCATION = Situación del CP
-FlightDataType.TYPE_CG_LOCATION = Situación del CG
-FlightDataType.TYPE_STABILITY = Calibración del margen de estabilidad
-FlightDataType.TYPE_MACH_NUMBER = Número Mach
-FlightDataType.TYPE_REYNOLDS_NUMBER = Número de Reynolds
-FlightDataType.TYPE_THRUST_FORCE = Empuje
-FlightDataType.TYPE_DRAG_FORCE = Fuerza de rozamiento
-FlightDataType.TYPE_DRAG_COEFF = Coeficiente de rozamiento
-FlightDataType.TYPE_AXIAL_DRAG_COEFF = Coeficiente de rozamiento axial
-FlightDataType.TYPE_FRICTION_DRAG_COEFF = Coeficiente de rozamiento por fricción
-FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Presión del coeficiente de rozamiento
-FlightDataType.TYPE_BASE_DRAG_COEFF = Coeficiente de rozamiento base
-FlightDataType.TYPE_NORMAL_FORCE_COEFF = Coeficiente de rozamiento normal
-FlightDataType.TYPE_PITCH_MOMENT_COEFF = Pico del coeficiente de rozamiento
-FlightDataType.TYPE_YAW_MOMENT_COEFF = Coeficiente de rozamiento de desviación
-FlightDataType.TYPE_SIDE_FORCE_COEFF = Coeficiente de fuerza lateral
-FlightDataType.TYPE_ROLL_MOMENT_COEFF = Coeficiente del momento de rotación
-FlightDataType.TYPE_ROLL_FORCING_COEFF = Fuerza del coeficiente de rotación
-FlightDataType.TYPE_ROLL_DAMPING_COEFF = Disminución del coeficiente de rotación
-FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Disminución del coeficiente de pico
-FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Disminución del coeficiente de desviación
-FlightDataType.TYPE_REFERENCE_LENGTH = Longitud de referencia
-FlightDataType.TYPE_REFERENCE_AREA = Área de referencia
-FlightDataType.TYPE_ORIENTATION_THETA = Orientación vertical (zenit)
-FlightDataType.TYPE_ORIENTATION_PHI = Orientación lateral (azimut)
-FlightDataType.TYPE_WIND_VELOCITY = Velocidad del viento
-FlightDataType.TYPE_AIR_TEMPERATURE = Temperatura del aire
-FlightDataType.TYPE_AIR_PRESSURE = Presión del aire
-FlightDataType.TYPE_SPEED_OF_SOUND = Velocidad del sonido
-FlightDataType.TYPE_TIME_STEP = Simulación del tiempo de etapa
-FlightDataType.TYPE_COMPUTATION_TIME = Cálculo del tiempo
-FlightDataType.TYPE_LATITUDE = Latitud
-FlightDataType.TYPE_LONGITUDE = Longitud
-FlightDataType.TYPE_CORIOLIS_ACCELERATION = Aceleración Coriolis
-
-! PlotConfiguration
-PlotConfiguration.Verticalmotion = Movimiento vertical vs. Tiempo
-PlotConfiguration.Totalmotion = Movimiento total vs. Tiempo
-PlotConfiguration.Flightside = Perfil lateral de vuelo
-PlotConfiguration.Stability = Estabilidad vs. Tiempo
-PlotConfiguration.Dragcoef = Coeficiente de rozamiento vs. Número Mach
-PlotConfiguration.Rollcharacteristics = Características de rotación
-PlotConfiguration.Angleofattack = Ángulo de orientación y ataque vs. Tiempo
-PlotConfiguration.Simulationtime = Simulación del tiempo de etapa y cálculo del tiempo
-
-! Warning
-Warning.LargeAOA.str1 = Evaluación de la amplitud del ángulo de ataque.
-Warning.LargeAOA.str2 = La amplitud del ángulo de ataque es excesiva (
-Warning.DISCONTINUITY = Discontinuidad en el diámetro del fuselaje.
-Warning.THICK_FIN = Las aletas gruesas no están correctamente modeladas.
-Warning.JAGGED_EDGED_FIN = El perfil afilado de las aletas puede ser inexacto.
-Warning.LISTENERS_AFFECTED = Las Extensiones se ejecutaron con la simulación del vuelo
-Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Sistema de recuperación abierto en fase de impulso, mientras el motor aún empujaba
-Warning.FILE_INVALID_PARAMETER = Parámetro encontrado no válido. Ignorado.
-
-
-! Scale dialog
-ScaleDialog.lbl.scaleRocket = El Cohete entero
-ScaleDialog.lbl.scaleSubselection = Todos los componentes seleccionados
-ScaleDialog.lbl.scaleSelection = Sólo el componente seleccionado
-ScaleDialog.title = Dimensión del diseño
-ScaleDialog.lbl.scale = Dimensión:
-ScaleDialog.lbl.scale.ttip = Indique si desea dimensionar el diseño completo o sólo los componentes seleccionados
-ScaleDialog.lbl.scaling = Dimensión a aplicar:
-ScaleDialog.lbl.scaling.ttip = Tamaño resultante, valores por encima del 100% aumentan el tamaño, y valores por debajo de 100% reduce el diseño.
-! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"
-ScaleDialog.lbl.scaleFrom = Dimensionar desde
-ScaleDialog.lbl.scaleTo = hasta
-ScaleDialog.lbl.scaleFromTo.ttip = Definir la dimensión en base a una longitud conocida u original.
-ScaleDialog.checkbox.scaleMass = Actualizar valores de Masa especificada
-ScaleDialog.checkbox.scaleMass.ttip = Dimensionar la Masa del componente y recalcular los valores de Masa por el cubo del factor de la escala
-ScaleDialog.button.scale = Dimensionar
-ScaleDialog.undo.scaleRocket = Dimensionar el cohete
-ScaleDialog.undo.scaleComponent = Dimensionar el componente
-ScaleDialog.undo.scaleComponents = Dimensionar los componentes
-
-!icons
-Icons.Undo = Deshacer
-Icons.Redo = Rehacer
-
-OpenRocketPrintable.Partsdetail = Detalle de las partes
-OpenRocketPrintable.Fintemplates = Plantilla de las aletas
-OpenRocketPrintable.DesignReport = Informe del Diseño
-
-OpenRocketDocument.Redo = Rehacer
-OpenRocketDocument.Undo = Deshacer
-
-!EllipticalFinSet
-EllipticalFinSet.Ellipticalfinset = Grupo de aletas elípticas
-
-! Optimization
-
-! Modifiers
-
-optimization.modifier.nosecone.length = Longitud de la ojiva
-optimization.modifier.nosecone.length.desc = Optimizar la longitud de la ojiva.
-optimization.modifier.nosecone.diameter = Diámetro de la ojiva optimization.modifier.nosecone.diameter.desc = Optimizar el diámetro de la base de la ojiva.
-optimization.modifier.nosecone.thickness = Grosor de la ojiva
-optimization.modifier.nosecone.thickness.desc = Optimizar el grosor de la pared de la ojiva.
-optimization.modifier.nosecone.shapeparameter = Parámetro de forma
-optimization.modifier.nosecone.shapeparameter.desc = Optimiza el parámetro de forma de la ojiva.
-
-optimization.modifier.transition.length = Longitud
-optimization.modifier.transition.length.desc = Optimiza la longitud de la transición.
-optimization.modifier.transition.forediameter = Diámetro delantero
-optimization.modifier.transition.forediameter.desc = Optimiza el diámetro delantero de la transición.
-optimization.modifier.transition.aftdiameter = Diámetro trasero
-optimization.modifier.transition.aftdiameter.desc = Optimiza el diámetro trasero de la transición.
-optimization.modifier.transition.thickness = Grosor
-optimization.modifier.transition.thickness.desc = Optimiza el grosor de la pared de la transición.
-optimization.modifier.transition.shapeparameter = Parámetro de forma
-optimization.modifier.transition.shapeparameter.desc = Optimizar el parámetro de forma de la transición.
-
-optimization.modifier.bodytube.length = Longitud
-optimization.modifier.bodytube.length.desc = Optimizar la longitud del cuerpo.
-optimization.modifier.bodytube.outerDiameter = Diámetro exterior
-optimization.modifier.bodytube.outerDiameter.desc = Optimizar el diámetro exterior del cuerpo manteniendo el grosor de la pared.
-optimization.modifier.bodytube.thickness = Grosor
-optimization.modifier.bodytube.thickness.desc = Optimizar el grosor de la pared del cuerpo.
-
-optimization.modifier.trapezoidfinset.rootChord = Longitud línea base
-optimization.modifier.trapezoidfinset.rootChord.desc = Optiminizar la longitud de la línea base de las aletas (longitud de la aleta sobre la superficie del cuerpo).
-optimization.modifier.trapezoidfinset.tipChord = Longitud borde superior
-optimization.modifier.trapezoidfinset.tipChord.desc = Optimizar la longitud del borde superior de las aletas (longitd del borde exterior de la aleta).
-optimization.modifier.trapezoidfinset.sweep = Desplazamiento borde superior
-optimization.modifier.trapezoidfinset.sweep.desc = Optimiza el desplazamiento del borde superior de las aletas (desplazamiento del borde superior de la aleta respecto del extremo delantero de la línea base).
-optimization.modifier.trapezoidfinset.height = Altura
-optimization.modifier.trapezoidfinset.height.desc = Optimizar la altura de las aletas (semi-spam).
-
-optimization.modifier.ellipticalfinset.length = Longitud línea base
-optimization.modifier.ellipticalfinset.length.desc = Optiminizar la longitud de la línea base de las aletas
-optimization.modifier.ellipticalfinset.height = Altura
-optimization.modifier.ellipticalfinset.height.desc = Optimizar la altura de las aletas (semi-spam).
-
-optimization.modifier.finset.cant = Angulo de ataque
-optimization.modifier.finset.cant.desc = Optimiza el ángulo de ataque de las aletas.
-optimization.modifier.finset.position = Posición
-optimization.modifier.finset.position.desc = Optimiza la posición de las aletas a lo largo del cuerpo del cohete.
-
-optimization.modifier.launchlug.length = Longitud
-optimization.modifier.launchlug.length.desc = Optimiza la longitud del tubo para la Guía.
-optimization.modifier.launchlug.outerDiameter = Diámetro exterior
-optimization.modifier.launchlug.outerDiameter.desc = Optimiza el diámetro exterior del tubo para la Guía.
-optimization.modifier.launchlug.thickness = Grosor
-optimization.modifier.launchlug.thickness.desc = Optimiza el grosor del tubo para la Guía manteniendo el diámetro exterior.
-optimization.modifier.launchlug.position = Posición
-optimization.modifier.launchlug.position.desc = Optimiza la posición del soporte para la guía a lo largo del cuerpo del cohete.
-
-
-optimization.modifier.internalcomponent.position = Posición
-optimization.modifier.internalcomponent.position.desc = Optimiza la posición del componente interno respecto del componente que lo contiene.
-
-optimization.modifier.masscomponent.mass = Masa
-optimization.modifier.masscomponent.mass.desc = Optimiza la masa del componente Masa.
-
-optimization.modifier.parachute.diameter = Diámetro
-optimization.modifier.parachute.diameter.desc = Optimiza el diámetro del pabellón del paracaídas.
-optimization.modifier.parachute.coefficient = Coeficiente de rozamiento
-optimization.modifier.parachute.coefficient.desc = Optimiza el coeficiente de rozamiento del paracaídas. Un paracaídas típico posee un coeficiente de 0.8.
-
-optimization.modifier.streamer.length = Longitud
-optimization.modifier.streamer.length.desc = Optimiza la longitud de la banderola.
-optimization.modifier.streamer.width = Anchura
-optimization.modifier.streamer.width.desc = Optimiza la anchura de la banderola.
-optimization.modifier.streamer.aspectRatio = Relación de aspecto
-optimization.modifier.streamer.aspectRatio.desc = Optimiza la relación de aspecto de la banderola (longitud/anchura). Usted NO debe seleccionar una longitud o anchura de la banderola al mismo tiempo que una relación de aspecto.
-optimization.modifier.streamer.coefficient = Coeficiente de rozamiento
-optimization.modifier.streamer.coefficient.desc = Optimiza el coeficiente de rozamiento de la banderola.
-
-optimization.modifier.recoverydevice.deployDelay = Retardo de eyección
-optimization.modifier.recoverydevice.deployDelay.desc = Optimiza el tiempo de retardo de eyección del sistema de recuperación.
-optimization.modifier.recoverydevice.deployAltitude = Altitud de eyección
-optimization.modifier.recoverydevice.deployAltitude.desc = Optimiza la altitud de la eyección del sistema de recuperación.
-
-optimization.modifier.rocketcomponent.overrideMass = Masa especificada
-optimization.modifier.rocketcomponent.overrideMass.desc = Optimiza la Masa especificada del componente.
-optimization.modifier.rocketcomponent.overrideCG = CG especificado
-optimization.modifier.rocketcomponent.overrideCG.desc = Optimiza la localización del Centro de Gravedad especificado en el componente.
-
-optimization.modifier.motormount.overhang = Sobresalida del motor
-optimization.modifier.motormount.overhang.desc = Optimiza la sobresalida del motor hacia el exterior.
-optimization.modifier.motormount.delay = Retardo de ignición
-optimization.modifier.motormount.delay.desc = Optimiza el retardo de la ingnición del motor.
-
-
-
-
-! General rocket design optimization dialog
-
-GeneralOptimizationDialog.title = Optimización del cohete
-GeneralOptimizationDialog.goal.maximize = Maximizar el valor
-GeneralOptimizationDialog.goal.minimize = Minimizar el valor
-GeneralOptimizationDialog.goal.seek = Buscar el valor de
-GeneralOptimizationDialog.btn.start = Iniciar optimización
-GeneralOptimizationDialog.btn.stop = Detener optimización
-GeneralOptimizationDialog.lbl.paramsToOptimize = Parámetros de optimización:
-GeneralOptimizationDialog.btn.add = Agregar
-GeneralOptimizationDialog.btn.add.ttip = Agregar el parámetro de optimizacaión
-GeneralOptimizationDialog.btn.remove = Eliminar
-GeneralOptimizationDialog.btn.remove.ttip = Eliminar el parámetro seleccionado de la optimización.
-GeneralOptimizationDialog.btn.removeAll = Eliminar todo
-GeneralOptimizationDialog.btn.removeAll.ttip = Eliminar todos los parámetros de optimización.
-GeneralOptimizationDialog.lbl.availableParams = Parámetros disponibles:
-GeneralOptimizationDialog.lbl.optimizationOpts = Opciones de optimización
-GeneralOptimizationDialog.lbl.optimizeSim = Optimizar simulación:
-GeneralOptimizationDialog.lbl.optimizeSim.ttip = Seleccionar la simulación a optimizar.
-GeneralOptimizationDialog.lbl.optimizeValue = Valor optimizado:
-GeneralOptimizationDialog.lbl.optimizeValue.ttip = Seleccionar el valor a optimizar.
-GeneralOptimizationDialog.lbl.optimizeGoal = Objetivo de optimización:
-GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Seleccionar el objetivo de la optimización.
-GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Buscar valor personalizado
-GeneralOptimizationDialog.lbl.requireStability = Estabilidad requerida
-GeneralOptimizationDialog.lbl.requireMinStability = Mínima estabilidad:
-GeneralOptimizationDialog.lbl.requireMinStability.ttip = Requerir un margen mínimo de estabilidad para el diseño.
-GeneralOptimizationDialog.lbl.requireMaxStability = Máxima estabilidad:
-GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Requerir un margen máximo de estabilidad para el diseño.
-GeneralOptimizationDialog.status.bestValue = El mejor valor:
-GeneralOptimizationDialog.status.bestValue.ttip = El mejor valor de optimización encontrado.
-GeneralOptimizationDialog.status.stepCount = Número de pasos:
-GeneralOptimizationDialog.status.stepCount.ttip = Número de pasos que deben realizarse para la optimización.
-GeneralOptimizationDialog.status.evalCount = Evaluaciones:
-GeneralOptimizationDialog.status.evalCount.ttip = Número total de evaluaciones (simulaciones) que deben realizarse.
-GeneralOptimizationDialog.status.stepSize = Tamaño del paso:
-GeneralOptimizationDialog.status.stepSize.ttip = Tamaño actual del paso de optimización (respecto al rango de parámetros de optimización).
-GeneralOptimizationDialog.btn.plotPath = Gráfica del proceso
-GeneralOptimizationDialog.btn.plotPath.ttip = Gráfica del proceso de optimización (sólo para 1 o 2 dimensiones).
-GeneralOptimizationDialog.btn.save = Guardar resultados
-GeneralOptimizationDialog.btn.save.ttip = Guardar los resultados de las evaluaciones (simulaciones) en un archivo CSV.
-GeneralOptimizationDialog.btn.apply = Aplicar optimización
-GeneralOptimizationDialog.btn.apply.ttip = Aplicar los resultados de la optimización al diseño del cohete.
-GeneralOptimizationDialog.btn.reset = Reiniciar
-GeneralOptimizationDialog.btn.reset.ttip = Reiniciar el diseño actual del cohete con el diseño optimizado.
-GeneralOptimizationDialog.btn.close = Cerrar
-GeneralOptimizationDialog.btn.close.ttip = Cerrar el cuadro de diálogo sin modificar el diseño actual del cohete.
-GeneralOptimizationDialog.error.selectParams.text = Primero seleccione algunos parámetros a optimizar de entre todos los parámetros disponibles.
-GeneralOptimizationDialog.error.selectParams.title = Seleccionar los parámetros de optimización
-GeneralOptimizationDialog.error.optimizationFailure.text = Falló la ejecución de la optimización:
-GeneralOptimizationDialog.error.optimizationFailure.title = Fallo de la optimización
-GeneralOptimizationDialog.undoText = Aplicar la optimización
-GeneralOptimizationDialog.basicSimulationName = Simulación básica
-GeneralOptimizationDialog.noSimulationName = Sin simulación
-GeneralOptimizationDialog.table.col.parameter = Parámetro
-GeneralOptimizationDialog.table.col.current = Actual
-GeneralOptimizationDialog.table.col.min = Mínimo
-GeneralOptimizationDialog.table.col.max = Máximo
-GeneralOptimizationDialog.export.header = Incluir línea de cabecera
-GeneralOptimizationDialog.export.header.ttip = Incluir una línea de cabecera en la que se indican las descripciones.
-GeneralOptimizationDialog.export.stability = Estabilidad
-
-
-! Dialog for plotting optimization results
-OptimizationPlotDialog.title = Resultados de la optimización
-OptimizationPlotDialog.lbl.zoomInstructions = Click y arrastrar abajo+derecha para acercar Zoom, arriba+izquierda para alejar Zoom
-OptimizationPlotDialog.plot1d.title = Resultado de la optimización
-OptimizationPlotDialog.plot1d.series = Resultado de la optimización
-OptimizationPlotDialog.plot2d.title = Trazabilidad de la optimización
-OptimizationPlotDialog.plot2d.path = Trazabilidad de la optimización
-OptimizationPlotDialog.plot2d.evals = Evaluaciones
-OptimizationPlotDialog.plot.ttip.stability = Estabilidad:
-OptimizationPlotDialog.plot.label.optimum = Óptimo
-
-! Optimization parameters
-MaximumAltitudeParameter.name = Altitud en apogeo
-MaximumVelocityParameter.name = Velocidad máxima
-MaximumAccelerationParameter.name = Aceleración máxima
-StabilityParameter.name = Estabilidad
-GroundHitVelocityParameter.name = Velocidad de aterrizaje
-LandingDistanceParameter.name = Distancia de aterrizaje
-TotalFlightTimeParameter.name = Tiempo total de vuelo
-DeploymentVelocityParameter.name = Velocidad durante la eyección
-
-
-! Compass directions drawn on a compass rose.
-CompassRose.lbl.north = N
-CompassRose.lbl.east = E
-CompassRose.lbl.south = S
-CompassRose.lbl.west = W
-
-! Compass directions with subdirections. These might not be localized even if the directions on the compass rose are.
-CompassSelectionButton.lbl.N = N
-CompassSelectionButton.lbl.NE = NE
-CompassSelectionButton.lbl.E = E
-CompassSelectionButton.lbl.SE = SE
-CompassSelectionButton.lbl.S = S
-CompassSelectionButton.lbl.SW = SW
-CompassSelectionButton.lbl.W = W
-CompassSelectionButton.lbl.NW = NW
-
-
-SlideShowDialog.btn.next = Next
-SlideShowDialog.btn.prev = Previous
-
-GuidedTourSelectionDialog.title = Guided tours
-GuidedTourSelectionDialog.lbl.selectTour = Select guided tour:
-GuidedTourSelectionDialog.lbl.description = Tour description:
-GuidedTourSelectionDialog.lbl.length = Number of slides:
-GuidedTourSelectionDialog.btn.start = Start tour!
-
+++ /dev/null
-\r
-#\r
-# French base translation file\r
-# Translated by Tripoli France\r
-# Should you need to add new logical keys here is the proposed method\r
-#\r
-# className.ComponentType.componentName\r
-#\r
-#\r
-# Text tokens within braces should not be translated, e.g.\r
-# "The file '{filename}' exists."\r
-# They are pieces that are inserted dynamically.\r
-#\r
-\r
-! Set to the name of the current translation file (used for debugging purposes)\r
-debug.currentFile = messages_fr.properties\r
-\r
-! RocketActions\r
-RocketActions.checkbox.Donotaskmeagain = Ne plus me demander\r
-RocketActions.lbl.Youcanchangedefop = Vous pouvez changer le mode opératoire par defaut dans les préferences.\r
-RocketActions.showConfirmDialog.lbl1 = Supprimer les simulations sélectionnées?\r
-RocketActions.showConfirmDialog.lbl2 = <html><i>Cette opération n'est pas réversible.</i>\r
-RocketActions.showConfirmDialog.title = Effacer les simulations\r
-RocketActions.DelCompAct.Delete = Effacer\r
-RocketActions.DelCompAct.ttip.Delete = Effacer la pièce sélectionnée.\r
-RocketActions.DelSimuAct.Delete = Effacer\r
-RocketActions.DelSimuAct.ttip.Delete = Effacer la simulation sélectionnée.\r
-RocketActions.DelAct.Delete = Effacer \r
-RocketActions.DelAct.ttip.Delete = Effacer la pièce ou la simulation sélectionnée.\r
-RocketActions.CutAction.Cut = Couper\r
-RocketActions.CutAction.ttip.Cut = Couper cette pièce ou simulation, l'ajouter au presse papier et l'enlever du projet\r
-RocketActions.CopyAct.Copy = Copier\r
-RocketActions.CopyAct.ttip.Copy = Copier les pièces (et les pièces liées) dans le presse papier.\r
-RocketActions.PasteAct.Paste = Coller\r
-RocketActions.PasteAct.ttip.Paste = Coller la pièce ou simulation présente dans le presse papier dans le projet.\r
-RocketActions.EditAct.Edit = Modifier\r
-RocketActions.EditAct.ttip.Edit = Modifier la pièce sélectionnée.\r
-RocketActions.NewStageAct.Newstage = Nouvel étage\r
-RocketActions.NewStageAct.ttip.Newstage = Ajouter un nouvel étage au projet.\r
-RocketActions.ActBoosterstage = Etage Booster\r
-RocketActions.MoveUpAct.Moveup = Monter\r
-RocketActions.MoveUpAct.ttip.Moveup = Monter la pièce.\r
-RocketActions.MoveDownAct.Movedown = Descendre\r
-RocketActions.MoveDownAct.ttip.Movedown = Descendre la pièce.\r
-\r
-! RocketPanel\r
-RocketPanel.FigTypeAct.Sideview = Vue de coté\r
-RocketPanel.FigTypeAct.ttip.Sideview = Vue de coté\r
-RocketPanel.FigTypeAct.Backview = Vue arrière\r
-RocketPanel.FigTypeAct.ttip.Backview = Vue arrière \r
-RocketPanel.lbl.Motorcfg = Configuration Moteur:\r
-RocketPanel.lbl.infoMessage = <html>Cliquer pour sélectionner Shift+cliquer pour sélectionner plusieurs Double-cliquer pour modifier Click+déplacer pour déplacer\r
-\r
-\r
-! BasicFrame\r
-BasicFrame.SimpleFileFilter1 = Tous les fichiers fusée (*.ork; *.rkt)\r
-BasicFrame.SimpleFileFilter2 = Fichiers OpenRocket (*.ork)\r
-BasicFrame.SimpleFileFilter3 = Fichiers RockSim (*.rkt)\r
-BasicFrame.tab.Rocketdesign = Projet fusée\r
-BasicFrame.tab.Flightsim = Simulations de vol\r
-BasicFrame.title.Addnewcomp = Ajouter une nouvelle pièce\r
-BasicFrame.dlg.lbl1 = Le projet '\r
-BasicFrame.dlg.lbl2 = ' N'a pas été sauvegardé.\r
-BasicFrame.dlg.lbl3 = Voulez vous le sauvegarder?\r
-BasicFrame.dlg.title = Projet non sauvegardé\r
-BasicFrame.StageName.Sustainer = Sustainer\r
-BasicFrame.WarningDialog.txt1 = Les problèmes suivant sont survenus lors de l'ouverture de\r
-BasicFrame.WarningDialog.txt2 = Certains éléments du projet n'ont peut être pas été chargé correctement.\r
-BasicFrame.WarningDialog.title = Avertissement lors de l'ouverture du fichier\r
-\r
-! General error messages used in multiple contexts\r
-error.fileExists.title = Le fichier existe déjà\r
-error.fileExists.desc = Le fichier '{filename}' existe déjà. Voulez vous l'ecraser?\r
-\r
-error.writing.title = Erreur d'éciture du fichier\r
-error.writing.desc = Une erreur est survenue lors de l'écriture dans le fichier:\r
-\r
-! Labels used in buttons of dialog windows\r
-button.ok = OK\r
-button.cancel = Annuler\r
-button.close = Fermer\r
-\r
-! Common labels used in buttons of dialog windows\r
-dlg.but.ok = Accepter\r
-dlg.but.cancel = Annuler\r
-dlg.but.close = Fermer\r
-\r
-\r
-! General file type names\r
-filetypes.pdf = fichier PDF\r
-\r
-\r
-! About Dialog\r
-AboutDialog.lbl.version = Version\r
-! The texts below provide additional credits for the translation maintainer\r
-! - In AboutDialog.lbl.translation replace "English" with the current language.\r
-! - AboutDialog.lbl.translator is the translator / group name (may be empty)\r
-! - AboutDialog.lbl.translatorWebsite is a URL to the translator / group (may be empty)\r
-! - AboutDialog.lbl.translatorIcon is the file name of an icon under pix/translators/ (may be empty)\r
-AboutDialog.lbl.translation = Traduit en français par:\r
-AboutDialog.lbl.translator = Tripoli France\r
-AboutDialog.lbl.translatorWebsite = http://tripoli.france.free.fr/\r
-AboutDialog.lbl.translatorIcon = logoTripoliFrance.png\r
-\r
-! Print dialog\r
-PrintDialog.title = Imprimer ou exporter\r
-PrintDialog.but.previewAndPrint = Pré-visualiser et imprimer\r
-PrintDialog.checkbox.showByStage = Montrer par étage\r
-PrintDialog.lbl.selectElements = Choisir les éléments à inclure:\r
-printdlg.but.saveaspdf = Sauvegarder en PDF\r
-printdlg.but.preview = Prévisualisation\r
-printdlg.but.settings = Configuration\r
-PrintDialog.error.preview.title = Impossible d'ouvrir la prévisualisation\r
-PrintDialog.error.preview.desc1 = Impossible d'ouvrir la prévisualisation PDF.\r
-PrintDialog.error.preview.desc2 = S'il vous plait utilisez l'option "Sauvegarder en PDF" à la place.\r
-\r
-\r
-!PrintSettingsDialog\r
-PrintSettingsDialog.title = Configuration impression\r
-PrintSettingsDialog.lbl.Templatefillcolor = Couleur de remplissage du modèle:\r
-PrintSettingsDialog.lbl.Templatebordercolor = Couleur des bords du modèle:\r
-PrintSettingsDialog.lbl.Papersize = Dimensions du papier:\r
-PrintSettingsDialog.lbl.Paperorientation = Orientation du papier:\r
-PrintSettingsDialog.but.Reset = Réinitialiser\r
-PrintSettingsDialog.but.Close = Fermer\r
-\r
-\r
-! Bug Report dialog\r
-bugreport.dlg.title = Rapport d'erreurs\r
-bugreport.dlg.but.Sendbugreport = Envoyer un rapport d'erreurs\r
-bugreport.dlg.but.Sendbugreport.Ttip = Envoyer automatiquement un rapport d'erreurs aux développeurs d'OpenRocket\r
-bugreport.dlg.successmsg1 = Rapport d'erreurs envoyé avec succès.\r
-bugreport.dlg.successmsg2 = Merci d'avoir contribué à l'amélioration d'OpenRocket!\r
-bugreport.dlg.successmsg3 = Rapport d'erreurs envoyé\r
-bugreport.dlg.connectedInternet = <html>Si vous êtes connecté sur Internet, vous pouvez tout simplement cliquer sur <em>Envoyer un rapport d'erreurs</em>.\r
-bugreport.dlg.otherwise = Sinon envoyez le texte ci-dessous à l'adresse:\r
-bugreport.lbl.Theinformation = Les informations ci-dessus sont susceptibles d'être incluse dans un rapport d'erreur publique. Assurez-vous qu'il ne contienne pas d'informations sensibles que vous ne voulez pas rendre publique.\r
-bugreport.dlg.failedmsg1 = OpenRocket n'a pas réussi à envoyer le rapport d'erreur:\r
-bugreport.dlg.failedmsg2 = S'il vous plait envoyez le rapport manuellement à\r
-bugreport.dlg.failedmsg3 = Erreur d'envoi du rapport\r
-bugreport.reportDialog.txt = <html><b>Vous pouvez signaler une erreur avec OpenRocket en remplissant et en envoyant le message ci-dessous.</b><br>Vous pouvez également signaler des erreurs et inclure des pièces jointes sur le site web du projet.\r
-bugreport.reportDialog.txt2 = <html><b>S'il vous plait ajoutez une courte description de ce que vous faisiez lorsque l'erreur s'est produite.</b>\r
-bugreport.dlg.provideDescription = S'il vous plait veuillez fournir d'abord une description du bug.\r
-bugreport.dlg.provideDescription.title = La description du bug est absente\r
-\r
-\r
-! Debug log dialog\r
-debuglogdlg.but.clear = Effacer\r
-debuglogdlg.OpenRocketdebuglog = Fichier debug d'OpenRocket\r
-debuglogdlg.Displayloglines = Afficher les numéros des lignes:\r
-debuglogdlg.Follow = Suivre\r
-debuglogdlg.col.Time = Heure\r
-debuglogdlg.col.Level = Niveau\r
-debuglogdlg.col.Location = Emplacement\r
-debuglogdlg.col.Message = Message\r
-debuglogdlg.lbl.Loglinenbr = Numéro de la ligne:\r
-debuglogdlg.lbl.Time = Heure:\r
-debuglogdlg.lbl.Level = Niveau:\r
-debuglogdlg.lbl.Location = Emplacement:\r
-debuglogdlg.lbl.Logmessage = Texte du message:\r
-debuglogdlg.lbl.Stacktrace = Stack trace:\r
-\r
-\r
-! Edit Motor configuration dialog\r
-edtmotorconfdlg.but.removemotor = Enlever le moteur\r
-edtmotorconfdlg.but.Selectmotor = Choisir le moteur\r
-edtmotorconfdlg.but.Removeconfiguration = Supprimer la configuration\r
-edtmotorconfdlg.but.Newconfiguration = Nouvelle configuration\r
-edtmotorconfdlg.lbl.Motormounts = <html><b>Portes moteur:</b>\r
-edtmotorconfdlg.title.Editmotorconf = Changer la configuration moteur\r
-edtmotorconfdlg.selectcomp = <html>Choisir les pièces utilisées par le porte moteur:\r
-edtmotorconfdlg.lbl.Motorconfig = <html><b>Configurations moteur:</b>\r
-edtmotorconfdlg.lbl.Configname = Nom de la configuration:\r
-edtmotorconfdlg.lbl.Leavenamedefault = Laisser le champ vide par défaut.\r
-\r
-! Example design dialog\r
-exdesigndlg.but.open = Ouvrir\r
-exdesigndlg.lbl.Selectexample = Choisir l'exemple de projet à ouvrir:\r
-exdesigndlg.lbl.Openexampledesign = Ouvrir un exemple de projet\r
-exdesigndlg.lbl.Exampledesignsnotfound = Impossible de trouver les exemples de projets.\r
-exdesigndlg.lbl.Examplesnotfound = Exemples non trouvés\r
-\r
-\r
-! Material edit panel\r
-matedtpan.but.new = Nouveau\r
-matedtpan.but.edit = Editer\r
-matedtpan.but.delete = Effacer\r
-matedtpan.but.revertall = Revenir aux valeurs précédentes\r
-matedtpan.col.Material = Matériaux\r
-matedtpan.col.Type = Type\r
-matedtpan.col.Density = Densité\r
-matedtpan.col.but.ttip.New = Ajouter un nouveau matériau\r
-matedtpan.title.Addcustmaterial = Ajouter un matériau personnalisé\r
-matedtpan.but.ttip.edit = Modifier un matériau existant\r
-matedtpan.title.Editmaterial = Modifier un matériau\r
-matedtpan.title2.Editmaterial = Les matériaux prédéfinis ne peuvent pas être modifiés.\r
-matedtpan.but.ttip.delete = Supprimer un matériau personnalisé\r
-matedtpan.but.ttip.revertall = Supprimer tous les matériaux personnalisés\r
-matedtpan.title.Deletealluser-defined = Effacer tous les matériaux personalisés?\r
-matedtpan.title.Revertall = Revenir aux valeurs précédentes?\r
-matedtpan.lbl.edtmaterials = Modifier les matériaux n'affectera pas les projets fusée existants.\r
-\r
-!MaterialModel\r
-MaterialModel.title.Material = Matériau\r
-MaterialModel.title.Defcustmat = Définir un matériau personnalisé\r
-\r
-\r
-! Preference dialog\r
-pref.dlg.but.add = Ajouter\r
-pref.dlg.but.reset = Réinitialiser\r
-pref.dlg.but.checknow = Vérifier maintenant\r
-pref.dlg.but.defaultmetric = Système métrique\r
-pref.dlg.but.defaultimperial = Système impérial\r
-pref.dlg.title.Preferences = Préférences \r
-pref.dlg.tab.Units = Unités\r
-pref.dlg.tab.Defaultunits = Unités par défaut\r
-pref.dlg.tab.Materials = Matériaux\r
-pref.dlg.tab.Custommaterials = Matériaux personnalisés\r
-pref.dlg.tab.Options = Options\r
-pref.dlg.tab.Miscellaneousoptions = Autres options\r
-pref.dlg.lbl.Positiontoinsert = Position pour insérer des composants internes:\r
-pref.dlg.lbl.Confirmdeletion = Confirmer l'effacement des simulations:\r
-pref.dlg.lbl.User-definedthrust = Courbes de poussée personnalisées:\r
-pref.dlg.Allthrustcurvefiles = Tous les fichiers de courbes de poussée (*.eng; *.rse; *.zip; répertoires)\r
-pref.dlg.RASPfiles = Fichiers moteur RASP (*.eng)\r
-pref.dlg.RockSimfiles = Fichiers moteur RockSim (*.rse)\r
-pref.dlg.ZIParchives = Archives ZIP (*.zip)\r
-pref.dlg.checkbox.Checkupdates = Rechercher les mises à jour au démarrage\r
-pref.dlg.ttip.Checkupdatesnow = Recherchez les mises à jour maintenant\r
-pref.dlg.lbl.Selectprefunits = Choisissez vos unités favorites:\r
-pref.dlg.lbl.Rocketdimensions = Dimensions de la fusée:\r
-pref.dlg.lbl.Linedensity = Epaisseur des lignes:\r
-pref.dlg.lbl.Motordimensions = Dimensions du moteur:\r
-pref.dlg.lbl.Surfacedensity = Densité de la Surface:\r
-pref.dlg.lbl.Distance = Distance:\r
-pref.dlg.lbl.Bulkdensity = Densité apparente:\r
-pref.dlg.lbl.Velocity = Vitesse:\r
-pref.dlg.lbl.Surfaceroughness = Rugosité de la Surface:\r
-pref.dlg.lbl.Acceleration = Accélération:\r
-pref.dlg.lbl.Area = Surface:\r
-pref.dlg.lbl.Mass = Masse:\r
-pref.dlg.lbl.Angle = Angle:\r
-pref.dlg.lbl.Force = Force:\r
-pref.dlg.lbl.Rollrate = Taux de roulis:\r
-pref.dlg.lbl.Totalimpulse = Impulsion totale:\r
-pref.dlg.lbl.Temperature = Température:\r
-pref.dlg.lbl.Momentofinertia = Moment d'inertie:\r
-pref.dlg.lbl.Pressure = Pression:\r
-pref.dlg.lbl.Stability = Stabilité:\r
-pref.dlg.lbl.FlightTime = Durée du vol:\r
-pref.dlg.lbl.effect1 = Les changements prendront effet la prochaine fois que vous ouvrirez une fenêtre.\r
-pref.dlg.lbl.Checkingupdates = Recherche des mises à jour...\r
-pref.dlg.lbl.msg1 = Une erreur est survenue durant la communication avec le serveur.\r
-pref.dlg.lbl.msg2 = Incapable de récupérer les informations de mise à jour\r
-pref.dlg.lbl.msg3 = Vous utilisez la dernière version d'OpenRocket.\r
-pref.dlg.lbl.msg4 = Pas de mises à jour disponible\r
-pref.dlg.PrefChoiseSelector1 = Toujours demander\r
-pref.dlg.PrefChoiseSelector2 = Insérer au milieu\r
-pref.dlg.PrefChoiseSelector3 = Ajouter à la fin\r
-pref.dlg.PrefBooleanSelector1 = Supprimer\r
-pref.dlg.PrefBooleanSelector2 = Confirmer\r
-pref.dlg.Add = Ajouter\r
-pref.dlg.DescriptionArea.Adddirectories = Ajouter des répertoires, des fichiers moteurs RASP (*.eng), des fichiers moteurs RockSim (*.rse) ou des fichiers archives ZIP séparés par un point virgule (;) pour charger des courbes de poussées externes. Les changements prendront effet au prochain démarrage d'OpenRocket.\r
-\r
-PreferencesDialog.lbl.language = Langue du programme:\r
-PreferencesDialog.languages.default = Valeur système par défaut\r
-PreferencesDialog.lbl.languageEffect = La langue sera changée après avoir redémarré OpenRocket.\r
-\r
-! Simulation edit dialog\r
-simedtdlg.but.runsimulation = Lancer la simulation\r
-simedtdlg.but.resettodefault = Restaurer les paramètres par défaut\r
-simedtdlg.but.add = Ajouter\r
-simedtdlg.but.remove = Enlever\r
-simedtdlg.title.Editsim = Modifier la simulation\r
-simedtdlg.lbl.Simname = Nom de la simulation:\r
-simedtdlg.tab.Launchcond = Conditions de lancement\r
-simedtdlg.tab.Simopt = Options de simulation\r
-simedtdlg.tab.Plotdata = Tracer les données\r
-simedtdlg.tab.Exportdata = Exporter les données\r
-simedtdlg.lbl.Motorcfg = Configuration moteur:\r
-simedtdlg.lbl.ttip.Motorcfg = Choisir la configuration moteur à utiliser.\r
-simedtdlg.combo.ttip.motorconf = Choisir la configuration moteur à utiliser.\r
-simedtdlg.lbl.Wind = Vent\r
-simedtdlg.lbl.Averwindspeed = Vitesse moyenne du vent:\r
-simedtdlg.lbl.ttip.Averwindspeed = Vitesse moyenne du vent par rapport au sol.\r
-simedtdlg.lbl.Stddeviation = Dérive standard:\r
-simedtdlg.lbl.ttip.Stddeviation = <html>La dérive standard de la vitesse du vent.<br>La vitesse du vent est le double de l'écart-type de la moyenne dans 95% des cas.\r
-simedtdlg.lbl.Turbulenceintensity = Intensité de la turbulence:\r
-simedtdlg.lbl.ttip.Turbulenceintensity1 = <html>L'intensité de la turbulence résulte de la division de la dérive par la vitesse moyenne de vent.<br>\r
-simedtdlg.lbl.ttip.Turbulenceintensity2 = Les valeurs typiques vont de \r
-simedtdlg.lbl.ttip.Turbulenceintensity3 = à\r
-simedtdlg.border.Atmoscond = Conditions atmosphériques\r
-simedtdlg.checkbox.InterStdAtmosphere = Utiliser les paramètres de l'Atmosphère Standard\r
-simedtdlg.checkbox.ttip.InterStdAtmosphere1 = <html>Sélectionner pour utiliser les paramètres de l'Atmosphère Standard.<br>Ce modèle à une température de\r
-simedtdlg.checkbox.ttip.InterStdAtmosphere2 = et une pression de \r
-simedtdlg.checkbox.ttip.InterStdAtmosphere3 = au niveau de la mer.\r
-simedtdlg.lbl.Temperature = Température:\r
-simedtdlg.lbl.ttip.Temperature = Température du site de lancement.\r
-simedtdlg.lbl.Pressure = Pression:\r
-simedtdlg.lbl.ttip.Pressure = Pression atmosphérique du site de lancement.\r
-simedtdlg.lbl.Launchsite = Site de lancement\r
-simedtdlg.lbl.Latitude = Latitude:\r
-simedtdlg.lbl.ttip.Latitude = <html>La latitude du site de lancement affecte l'attraction gravitationnelle de la Terre.<br>> Les valeurs positives sont dans l'hémisphère Nord, les valeurs négatives sur l'hémisphère Sud.\r
-\r
-simedtdlg.lbl.Longitude = Longitude:\r
-simedtdlg.lbl.ttip.Longitude = <html>Nécessaire pour les prédictions du temps and elevation models.\r
-\r
-simedtdlg.lbl.Altitude = Altitude:\r
-simedtdlg.lbl.ttip.Altitude = <html>Altitude du site de lancement par rapport au niveau de la mer.<br>Cela affecte la position de la fusée dans le modèle atmosphérique.\r
-simedtdlg.border.Launchrod = Rampe de lancement\r
-simedtdlg.lbl.Length = Longueur:\r
-simedtdlg.lbl.ttip.Length = Longueur de la rampe.\r
-simedtdlg.lbl.Angle = Angle:\r
-simedtdlg.lbl.ttip.Angle = Angle de la rampe de lancement par rapport à la verticale.\r
-simedtdlg.lbl.Direction = Direction:\r
-simedtdlg.lbl.ttip.Direction1 = <html>Direction de la rampe de lance par rapport au vent.<br>\r
-simedtdlg.lbl.ttip.Direction2 = = Face au vent,\r
-simedtdlg.lbl.ttip.Direction3 = = vent arrière.\r
-simedtdlg.border.Simopt = Options de simulation\r
-simedtdlg.lbl.Calcmethod = Méthode de calcul:\r
-simedtdlg.lbl.ttip.Calcmethod = <html>La méthode Barrowman étendue calcule les forces aérodynamique selon <br>les équations de Barrowman étendues pour arranger plus de pièces.\r
-simedtdlg.lbl.ExtBarrowman = Barrowman étendu\r
-simedtdlg.lbl.Simmethod = Méthode de Simulation:\r
-simedtdlg.lbl.ttip.Simmethod1 = <html>Le simulateur de six degrés de liberté permet la liberté totale de fusée en vol.<br>\r
-simedtdlg.lbl.ttip.Simmethod2 = Integration is performed using a 4<sup>th</sup> order Runge-Kutta 4 numerical integration.\r
-simedtdlg.lbl.GeodeticMethod = Calculs Geodetic:\r
-simedtdlg.lbl.ttip.GeodeticMethodTip = Relate to the calculation of coordinates on the earth. This also enables coriolis effect computations.\r
-simedtdlg.lbl.Timestep = Réglage du pas de temps:\r
-simedtdlg.lbl.ttip.Timestep1 = <html>Le temps entre les étapes de la simulation.<br>Avec un pas de temps plus petit la simulation est plus lente mais également plus précise.<br>\r
-simedtdlg.lbl.ttip.Timestep2 = The 4<sup>th</sup> order simulation method is quite accurate with a time step of\r
-simedtdlg.but.ttip.resettodefault = Réinitialiser le pas de temps à sa valeur par défaut (\r
-simedtdlg.border.Simlist = Auditeurs de simulation\r
-simedtdlg.txt.longA1 = <html><i>Les auditeurs de simulation</i> sont une fonction avancé qui permet à l'utilisateur d'écrire du code pour suivre et interagir avec la simulation. \r
-simedtdlg.txt.longA2 = Pour plus de détails sur les auditeurs de simulation, reférez vous à la documentation technique d'OpenRocket.\r
-simedtdlg.lbl.Curlist = Auditeurs de simulation actuel:\r
-simedtdlg.lbl.Addsimlist = Ajouter un "auditeur de simulation"\r
-simedtdlg.lbl.Noflightdata = Aucune donnée de vol disponible.\r
-simedtdlg.lbl.runsimfirst = S'il vous plait faites tourner la simulation d'abord.\r
-simedtdlg.chart.Simflight = Vol simulé\r
-simedtdlg.dlg.Simres = Résultats de la simulation\r
-simedtdlg.IntensityDesc.None = Aucune\r
-simedtdlg.IntensityDesc.Verylow = Très basse\r
-simedtdlg.IntensityDesc.Low = Basse\r
-simedtdlg.IntensityDesc.Medium = Moyenne\r
-simedtdlg.IntensityDesc.High = Haute\r
-simedtdlg.IntensityDesc.Veryhigh = Très haute\r
-simedtdlg.IntensityDesc.Extreme = Extrême\r
-\r
-GeodeticComputationStrategy.none.name = Aucune\r
-GeodeticComputationStrategy.none.desc = Ne pas faire de calculs geodetic.\r
-GeodeticComputationStrategy.spherical.name = Approximation sphérique\r
-GeodeticComputationStrategy.spherical.desc = <html>Perform geodetic computations assuming a spherical Earth.<br>This is sufficiently accurate for almost all purposes.\r
-GeodeticComputationStrategy.wgs84.name = ellipsoïde WGS84\r
-GeodeticComputationStrategy.wgs84.desc = <html>Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.<br>Slower and unnecessary in most cases.\r
-\r
-\r
-\r
-! Simulation Panel\r
-simpanel.but.newsimulation = Nouvelle simulation\r
-simpanel.but.editsimulation = Modifier la simulation\r
-simpanel.but.runsimulations = Lancer les simulations\r
-simpanel.but.deletesimulations = Effacer les simulations\r
-simpanel.but.plotexport = Tracer / exporter\r
-simpanel.but.ttip.newsimulation = Ajouter une nouvelle simulation\r
-simpanel.but.ttip.editsim = Modifier la simulation sélectionnée\r
-simpanel.but.ttip.runsimu = Recommencer la simulation sélectionnée\r
-simpanel.but.ttip.deletesim = Effacer les simulations sélectionnées\r
-simpanel.checkbox.donotask = Ne plus me demander\r
-simpanel.lbl.defpref = Vous pouvez changer le mode opératoire par défaut dans préférences.\r
-simpanel.dlg.lbl.DeleteSim1 = Effacer les simulations sélectionnées?\r
-simpanel.dlg.lbl.DeleteSim2 = <html><i>Cette opération n'est pas réversible.</i>\r
-simpanel.dlg.lbl.DeleteSim3 = Effacer les simulations\r
-simpanel.col.Name = Nom\r
-simpanel.col.Motors = Moteurs\r
-simpanel.col.Apogee = Apogée\r
-simpanel.col.Maxvelocity = Vitesse Max.\r
-simpanel.col.Maxacceleration = Accélération Max.\r
-simpanel.col.Timetoapogee = Temps pour atteindre l'apogée\r
-simpanel.col.Flighttime = Temps de vol\r
-simpanel.col.Groundhitvelocity = Vitesse à l'atterrissage\r
-\r
-! SimulationRunDialog\r
-SimuRunDlg.title.RunSim = Simulations en cour...\r
-SimuRunDlg.lbl.Running = En cour ...\r
-SimuRunDlg.lbl.Simutime = Temps de simulation:\r
-SimuRunDlg.lbl.Altitude = Altitude:\r
-SimuRunDlg.lbl.Velocity = Vitesse:\r
-SimuRunDlg.msg.Unabletosim = Simulation impossible:\r
-SimuRunDlg.msg.errorOccurred = Une erreur s'est produite durant la simulation:\r
-SimuRunDlg.msg.AnException1 = Une exception s'est produite lors de la simulation:\r
-SimuRunDlg.msg.AnException2 = S'il vous plaît faites un rapport d'erreurs avec les détails ci-dessous.\r
-SimuRunDlg.msg.AssertionError1 = Une erreur de calcul s'est produite lors de la simulation.\r
-SimuRunDlg.msg.AssertionError2 = S'il vous plaît faites un rapport d'erreurs avec les détails ci-dessous.\r
-SimuRunDlg.msg.unknownerror1 = Une erreur inconnue s'est produite lors de la simulation.\r
-SimuRunDlg.msg.unknownerror2 = Le programme peut être instable, vous devez enregistrer toutes vos créations et redémarrez OpenRocket maintenant!\r
-\r
-\r
-\r
-! SimulationExportPanel\r
-SimExpPan.desc = Fichiers dont les données sont séparées par une virgule (*.csv)\r
-SimExpPan.border.Vartoexport = Variables à exporter\r
-SimExpPan.but.Selectall = Tout sélectionner\r
-SimExpPan.but.Selectnone = Ne rien sélectionner\r
-SimExpPan.border.Fieldsep = Séparateur de champ\r
-SimExpPan.lbl.Fieldsepstr = Séparateur de champ:\r
-SimExpPan.lbl.longA1 = <html>La chaîne utilisée pour séparer les champs dans le fichier exporté.<br>\r
-SimExpPan.lbl.longA2 = Utiliser ',' pour un fichier (CSV).\r
-SimExpPan.checkbox.Includesimudesc = Inclure la description de la simulation\r
-SimExpPan.checkbox.ttip.Includesimudesc = Inclure un commentaire au début du fichier pour décrire la simulation.\r
-SimExpPan.border.Comments = Commentaires\r
-SimExpPan.checkbox.Includefielddesc = Inclure les descriptions des champs\r
-SimExpPan.checkbox.ttip.Includefielddesc = Inclure une ligne de commentaire avec la description des variables exportées.\r
-SimExpPan.checkbox.Incflightevents = Inclure les événements de vol\r
-SimExpPan.checkbox.ttip.Incflightevents = Inclure une ligne de commentaire pour chaque évènement de vol.\r
-SimExpPan.lbl.Commentchar = Symbole pour les commentaires:\r
-SimExpPan.lbl.ttip.Commentchar = Le symbole utilisé pour une ligne de commentaires.\r
-SimExpPan.but.Exporttofile = Exporter dans un fichier...\r
-SimExpPan.Fileexists.desc1 = Le fichier \"\r
-SimExpPan.Fileexists.desc2 = \" existe déjà. Ecraser?\r
-SimExpPan.Fileexists.title = Le fichier existe\r
-SimExpPan.ExportingVar.desc1 = Exporter 1 variable sur un total de\r
-SimExpPan.ExportingVar.desc2 = Exportation\r
-SimExpPan.ExportingVar.desc3 = variable sur un total de\r
-SimExpPan.Col.Variable = Variable\r
-SimExpPan.Col.Unit = Unité\r
-\r
-\r
-CsvOptionPanel.separator.space = SPACE\r
-CsvOptionPanel.separator.tab = TAB\r
-\r
-\r
-\r
-! MotorPlot\r
-MotorPlot.title.Motorplot = Courbe du moteur\r
-MotorPlot.but.Select = Sélection\r
-MotorPlot.Chart.Motorthrustcurve = Courbe de poussée moteur\r
-MotorPlot.Chart.Time = Temps / s\r
-MotorPlot.Chart.Thrust = Poussée / N\r
-MotorPlot.txt.Designation = Désignation:\r
-MotorPlot.txt.Manufacturer = Manufacturer:\r
-MotorPlot.txt.Type = Type:\r
-MotorPlot.txt.Delays = Retards:\r
-MotorPlot.txt.Comment = Commentaires:\n\r
-\r
-\r
-\r
-! Simulation plot panel\r
-simplotpanel.lbl.Presetplotconf = Prédéfinir les paramètres du tracé:\r
-simplotpanel.lbl.Xaxistype = Axe des X:\r
-simplotpanel.lbl.Unit = Unités:\r
-simplotpanel.lbl.Yaxistypes = Axe des Y:\r
-simplotpanel.lbl.Flightevents = Evénements du vol:\r
-simplotpanel.but.All = Tous\r
-simplotpanel.but.None = Aucun\r
-simplotpanel.but.NewYaxisplottype = Nouveau type de tracé de l'axe Y\r
-simplotpanel.but.Plotflight = Tracer le vol\r
-simplotpanel.lbl.Axis = Axes:\r
-simplotpanel.but.ttip.Removethisplot = Effacer le tracé\r
-simplotpanel.Desc = Les données seront tracées en fonction du temps même si le type d'Axe des abscisses n'est pas le temps.\r
-simplotpanel.OptionPane.lbl1 = Un maximum de 15 tracés est permis. \r
-simplotpanel.OptionPane.lbl2 = Impossible d'ajouter le tracé\r
-simplotpanel.AUTO_NAME = Auto\r
-simplotpanel.LEFT_NAME = Gauche\r
-simplotpanel.RIGHT_NAME = Droite\r
-simplotpanel.CUSTOM = Personnalisé\r
-\r
-! Component add buttons\r
-compaddbuttons.Bodycompandfinsets = Pièces du corps et ailerons\r
-compaddbuttons.Nosecone = Cône\r
-compaddbuttons.Bodytube = Tube du\ncorps\r
-compaddbuttons.Transition = Transition\r
-compaddbuttons.Trapezoidal = Trapézoïdale\r
-compaddbuttons.Elliptical = Elliptique\r
-compaddbuttons.Freeform = Forme libre\r
-compaddbuttons.Launchlug = Tube de\nguidage\r
-compaddbuttons.Innercomponent = Pièces internes\r
-compaddbuttons.Innertube = Tube interne\r
-compaddbuttons.Coupler = Coupleur\r
-compaddbuttons.Centeringring = Anneau de\ncentrage\r
-compaddbuttons.Bulkhead = Cloison\r
-compaddbuttons.Engineblock = Bague de\nrétention\nmoteur\r
-compaddbuttons.Massobjects = Pièces pleines\r
-compaddbuttons.Parachute = Parachute\r
-compaddbuttons.Streamer = Banderole\r
-compaddbuttons.Shockcord = Cordon\namortisseur\r
-compaddbuttons.Masscomponent = Poids\r
-compaddbuttons.Donotaskmeagain = Ne plus me poser la question\r
-compaddbuttons.Selectcomppos = Position de la pièce\r
-compaddbuttons.lbl.Youcanchange = Vous pouvez modifier le fonctionnement par défaut dans les préférences.\r
-compaddbuttons.lbl.insertcomp = Insérez la pièce après l'élément actuel ou en tant que dernier élément?\r
-compaddbuttons.askPosition.Inserthere = Ajouter ici\r
-compaddbuttons.askPosition.Addtotheend = Ajouter à la fin\r
-compaddbuttons.askPosition.Cancel = Annuler\r
-\r
-! Component Analysis Dialog\r
-componentanalysisdlg.componentanalysis = Analyse pièce\r
-componentanalysisdlg.lbl.winddir = Direction du vent:\r
-componentanalysisdlg.TitledBorder.warnings = Avertissements:\r
-componentanalysisdlg.ToggleBut.worst = Pire\r
-componentanalysisdlg.lbl.angleofattack = Angle d'attaque:\r
-componentanalysisdlg.lbl.machnumber = Mach number:\r
-componentanalysisdlg.lbl.rollrate = Taux de roulis:\r
-componentanalysisdlg.lbl.activestages = Etages actifs:\r
-componentanalysisdlg.lbl.motorconf = Configuration moteur:\r
-componentanalysisdlg.TabStability.Col.Component = Pièce\r
-componentanalysisdlg.TabStability = Stabilité\r
-componentanalysisdlg.TabStability.ttip = Information de stabilité\r
-componentanalysisdlg.dragTableModel.Col.Component = Pièce\r
-componentanalysisdlg.dragTableModel.Col.Pressure = <html>Pression C<sub>D</sub>\r
-componentanalysisdlg.dragTableModel.Col.Base = <html>Base C<sub>D</sub>\r
-componentanalysisdlg.dragTableModel.Col.friction = <html>Friction C<sub>D</sub>\r
-componentanalysisdlg.dragTableModel.Col.total = <html>Total C<sub>D</sub>\r
-componentanalysisdlg.dragTabchar = Caractéristiques de traînée\r
-componentanalysisdlg.dragTabchar.ttip = Caractéristiques de traînée\r
-componentanalysisdlg.rollTableModel.Col.component = Pièce\r
-componentanalysisdlg.rollTableModel.Col.rollforc = Coefficient de forçage de roulis\r
-componentanalysisdlg.rollTableModel.Col.rolldamp = Coefficient amortisseur de roulis\r
-componentanalysisdlg.rollTableModel.Col.total = <html>Total C<sub>l</sub>\r
-componentanalysisdlg.rollTableModel = Dynamique du roulis\r
-componentanalysisdlg.rollTableModel.ttip = Dynamique du roulis\r
-componentanalysisdlg.println.closingmethod = Méthode de clôture appelée:\r
-componentanalysisdlg.println.settingnam = SETTING NAN VALUES\r
-componentanalysisdlg.lbl.reflenght = Longueur de référence: \r
-componentanalysisdlg.lbl.refarea = Aire de référence: \r
-!componentanalysisdlg.but.close =Fermer\r
-componentanalysisdlg.TabStability.Col.Component = Pièce\r
-\r
-! Custom Material dialog\r
-custmatdlg.title.Custommaterial = Matériau personnalisé\r
-custmatdlg.lbl.Materialname = Nom du matériau: \r
-custmatdlg.lbl.Materialtype = Type de matériau:\r
-custmatdlg.lbl.Materialdensity = Densité du matériau:\r
-custmatdlg.checkbox.Addmaterial = Ajouter la pièce dans la base de données\r
-\r
-\r
-! Ring Component Config\r
-ringcompcfg.OuterRadius = Diamètre extérieur\r
-ringcompcfg.Automatic = Automatique\r
-ringcompcfg.InnerRadius = Diamètre intérieur\r
-ringcompcfg.Thickness = Epaisseur\r
-ringcompcfg.Length = Longueur\r
-ringcompcfg.Positionrelativeto = Position relative à:\r
-ringcompcfg.plus = plus\r
-!ringcompcfg.PositionValue = PositionValue\r
-ringcompcfg.Radialdistance = Rayon:\r
-ringcompcfg.Distancefrom = Distance de l'axe central de la fusée\r
-ringcompcfg.Radialdirection = Azimut\r
-ringcompcfg.radialdirectionfrom = Sens par rapport à l'axe central de la fusée\r
-ringcompcfg.but.Reset = Réinitialisation\r
-ringcompcfg.but.Resetcomponant = Réinitialiser la pièce à l'axe de la fusée\r
-ringcompcfg.EngineBlock.desc = <html>Un <b>bloc moteur </b> empêche le moteur de se déplacer vers l'avant dans le tube porte moteur.<br><br>Pour ajouter un moteur, créer un <b>tube</b> ou un <b>tube interne</b> et marquer le comme porte moteur dans l'onglet <em>Moteur</em>.\r
-ringcompcfg.note.desc = A noter: Un tube interne n'affectera pas l'aérodynamisme de la fusée même si il est situé en dehors du tube.\r
-\r
-\r
-! Body Tube Config\r
-BodyTubecfg.lbl.Bodytubelength = Longueur du tube:\r
-BodyTubecfg.lbl.Outerdiameter = Diamètre externe:\r
-BodyTubecfg.lbl.Innerdiameter = Diamètre interne:\r
-BodyTubecfg.lbl.Wallthickness = Epaisseur des parois:\r
-BodyTubecfg.tab.General = Général\r
-BodyTubecfg.tab.Generalproperties = Propriétés générales\r
-BodyTubecfg.tab.Motor = Moteur\r
-BodyTubecfg.tab.Motormountconf = Configuration du porte moteur\r
-BodyTubecfg.checkbox.Automatic = Automatique\r
-BodyTubecfg.checkbox.Filled = Aspérités bouchées\r
-\r
-! FinSetConfig\r
-FinSetConfig.tab.Fintabs = Pattes des ailerons\r
-FinSetConfig.tab.Through-the-wall = Ailerons traversant le fuselage\r
-FinSetConfig.but.Converttofreeform = Convertir en forme libre\r
-FinSetConfig.but.Converttofreeform.ttip = Convertir ce jeu d'ailerons en forme libre\r
-FinSetConfig.Convertfinset = Convertir le jeu d'ailerons\r
-FinSetConfig.but.Splitfins = Séparer les ailerons\r
-FinSetConfig.but.Splitfins.ttip = Diviser le jeu d'ailerons en aileron indépendant\r
-FinSetConfig.lbl.Through-the-wall = Ailerons traversant le fuselage:\r
-FinSetConfig.lbl.Tablength = Longueur de la patte:\r
-FinSetConfig.ttip.Tablength = La longueur de la patte de l'aileron.\r
-FinSetConfig.lbl.Tabheight = Hauteur de la patte:\r
-FinSetConfig.ttip.Tabheight = La hauteur de l'envergure de la patte de l'aileron.\r
-FinSetConfig.lbl.Tabposition = Position de la patte:\r
-FinSetConfig.ttip.Tabposition = La position de la patte de l'aileron.\r
-FinSetConfig.lbl.relativeto = relative à\r
-\r
-! MotorDatabaseLoadingDialog\r
-MotorDbLoadDlg.title = Chargement des moteurs\r
-MotorDbLoadDlg.Loadingmotors = Chargement des moteurs...\r
-\r
-! RocketConfig\r
-RocketCfg.lbl.Designname = Nom du projet:\r
-RocketCfg.lbl.Designer = Concepteur:\r
-RocketCfg.lbl.Comments = Commentaires:\r
-RocketCfg.lbl.Revisionhistory = Historique des modifications:\r
-RocketCfg.lbl.Material = Matériaux:\r
-\r
-! ShockCordConfig\r
-ShockCordCfg.lbl.Shockcordlength = Longueur du cordon amortisseur\r
-\r
-! RocketComponentConfig\r
-RocketCompCfg.lbl.Componentname = Nom de la pièce:\r
-RocketCompCfg.ttip.Thecomponentname = Le nom de la pièce.\r
-RocketCompCfg.tab.Override = Forcer la valeur\r
-RocketCompCfg.tab.MassandCGoverride = Forçage de la Masse et du CG\r
-RocketCompCfg.tab.Figure = Forme\r
-RocketCompCfg.tab.Figstyleopt = Options de la forme\r
-RocketCompCfg.tab.Comment = Commentaires\r
-RocketCompCfg.tab.Specifyacomment = Commentaires concernant la pièce\r
-RocketCompCfg.lbl.Mass = Masse:\r
-RocketCompCfg.lbl.Componentmass = Masse de la pièce:\r
-RocketCompCfg.lbl.overriddento = (forcé à\r
-RocketCompCfg.lbl.overriddenby = (forcé par\r
-RocketCompCfg.lbl.Componentmaterial = Matériaux composant la pièce:\r
-RocketCompCfg.lbl.Componentfinish = Finition de la pièce:\r
-RocketCompCfg.lbl.ttip.componentmaterialaffects = Les matériaux utilisés pour la pièce affectent le poids de la pièce.\r
-RocketCompCfg.combo.ttip.componentmaterialaffects = Les matériaux utilisés pour la pièce affectent le poids de la pièce.\r
-RocketCompCfg.lbl.longA1 = <html>La finition de la pièce affecte l'aérodynamisme de la pièce.<br>\r
-RocketCompCfg.lbl.longA2 = La valeur indiquée est la hauteur moyenne de la rugosité de la surface.\r
-RocketCompCfg.but.Setforall = Appliquer à tous\r
-RocketCompCfg.but.ttip.Setforall = Régler la finition pour tous les composants de la fusée.\r
-RocketCompCfg.lbl.Overridemassorcenter = Forcer la masse ou le centre de gravité du \r
-RocketCompCfg.checkbox.Overridemass = Forcer la masse:\r
-RocketCompCfg.checkbox.Overridecenterofgrav = Forcer le centre de gravité:\r
-RocketCompCfg.checkbox.OverridemassandCG = Forcer la masse et le centre de gravité de tous les sous composants\r
-RocketCompCfg.lbl.longB1 = <html>Le forçage de la masse n'inclus pas le ou les moteurs.<br>\r
-RocketCompCfg.lbl.longB2 = Le centre de gravité est mesuré à partir de l'extrémité avant de la fusée\r
-RocketCompCfg.lbl.Commentsonthe = Commentaires à propos du \r
-RocketCompCfg.lbl.Figurestyle = Modèle de forme:\r
-RocketCompCfg.lbl.Componentcolor = Couleur de la pièce:\r
-RocketCompCfg.lbl.Choosecolor = Choisir la couleur\r
-RocketCompCfg.checkbox.Usedefaultcolor = Utiliser la couleur par défaut\r
-RocketCompCfg.lbl.Complinestyle = Style de lignes pour les pièces:\r
-RocketCompCfg.but.Saveasdefstyle = Sauver le modèle par défaut\r
-RocketCompCfg.lbl.Diameter = Diamètre:\r
-RocketCompCfg.lbl.Length = Longueur:\r
-RocketCompCfg.lbl.Thickness = Epaisseur:\r
-RocketCompCfg.checkbox.Endcapped = Arrière clos \r
-RocketCompCfg.ttip.Endcapped = Précise si l'arrière du cône est clos.\r
-RocketCompCfg.title.Noseconeshoulder = Accotement du cône\r
-RocketCompCfg.title.Aftshoulder = Accotement arrière\r
-RocketCompCfg.border.Foreshoulder = Accotement avant \r
-!RocketCompCfg.lbl.Length = Length:\r
-\r
-! BulkheadConfig\r
-BulkheadCfg.tab.Radius = Rayon:\r
-BulkheadCfg.tab.Thickness = Epaisseur:\r
-BulkheadCfg.tab.General = Général\r
-BulkheadCfg.tab.Generalproperties = Propriétés générales\r
-\r
-!CenteringRingConfig\r
-CenteringRingCfg.tab.Outerdiam = Diamètre externe:\r
-CenteringRingCfg.tab.Innerdiam = Diamètre interne:\r
-CenteringRingCfg.tab.Thickness = Epaisseur:\r
-CenteringRingCfg.tab.General = Général\r
-CenteringRingCfg.tab.Generalproperties = Propriétés Générales\r
-\r
-!ComponentConfigDialog\r
-ComponentCfgDlg.configuration =\r
-ComponentCfgDlg.configuration1 = configuration\r
-ComponentCfgDlg.Modify = Modifier\r
-\r
-!EllipticalFinSetConfig\r
-EllipticalFinSetCfg.Nbroffins = Nombre d'ailerons:\r
-EllipticalFinSetCfg.Rotation = Rotation:\r
-EllipticalFinSetCfg.Fincant = Inclinaison de l'aileron:\r
-EllipticalFinSetCfg.Rootchord = Emplanture:\r
-EllipticalFinSetCfg.Height = Hauteur:\r
-EllipticalFinSetCfg.Positionrelativeto = Position relative à:\r
-EllipticalFinSetCfg.plus = plus\r
-EllipticalFinSetCfg.FincrossSection = Coupe de l'aileron:\r
-EllipticalFinSetCfg.Thickness = Epaisseur:\r
-EllipticalFinSetCfg.General = Général\r
-EllipticalFinSetCfg.Generalproperties = Propriétés Générales\r
-EllipticalFinSetCfg.ttip.Fincant = Angle d'inclinaison des ailerons par rapport au corps de la fusée\r
-\r
-!FreeformFinSetConfig\r
-FreeformFinSetCfg.tab.General = Général\r
-FreeformFinSetCfg.tab.ttip.General = Propriétés générales\r
-FreeformFinSetCfg.tab.Shape = Forme\r
-FreeformFinSetCfg.tab.ttip.Finshape = Forme de l'aileron\r
-FreeformFinSetCfg.lbl.Numberoffins = Nombre d'ailerons:\r
-FreeformFinSetCfg.lbl.Finrotation = Rotation des ailerons:\r
-FreeformFinSetCfg.lbl.Fincant = Inclinaison de l'aileron:\r
-FreeformFinSetCfg.lbl.ttip.Fincant = angle d'inclinaison des ailerons par rapport au corps de la fusée.\r
-FreeformFinSetCfg.lbl.Posrelativeto = Position par rapport à:\r
-FreeformFinSetCfg.lbl.plus = plus\r
-FreeformFinSetCfg.lbl.FincrossSection = Coupe de l'aileron:\r
-FreeformFinSetCfg.lbl.Thickness = Epaisseur:\r
-! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle\r
-FreeformFinSetCfg.lbl.doubleClick1 = Double-click\r
-FreeformFinSetCfg.lbl.doubleClick2 = pour éditer\r
-FreeformFinSetCfg.lbl.clickDrag = Cliquer+déplacer: Ajouter et déplacer des points\r
-FreeformFinSetCfg.lbl.ctrlClick = Ctrl+cliquer: Enlever un point\r
-\r
-\r
-!InnerTubeConfig\r
-InnerTubeCfg.tab.Motor = Moteur\r
-InnerTubeCfg.tab.ttip.Motor = Configuration du porte moteur\r
-InnerTubeCfg.tab.Cluster = Cluster\r
-InnerTubeCfg.tab.ttip.Cluster = Configuration du cluster\r
-InnerTubeCfg.tab.Radialpos = Position circulaire\r
-InnerTubeCfg.tab.ttip.Radialpos = Position circulaire\r
-InnerTubeCfg.lbl.Selectclustercfg = Choisir la configuration du cluster:\r
-InnerTubeCfg.lbl.TubeSep = Séparation du tube:\r
-InnerTubeCfg.lbl.ttip.TubeSep = La Séparation des tubes, 1.0 = chacun se touche\r
-InnerTubeCfg.lbl.Rotation = Rotation:\r
-InnerTubeCfg.lbl.ttip.Rotation = Angle de rotation du cluster\r
-InnerTubeCfg.lbl.Rotangle = Angle de rotation de la configuration du cluster\r
-InnerTubeCfg.but.Splitcluster = Séparer le cluster\r
-InnerTubeCfg.lbl.longA1 = <html>séparer le cluster en pièces distinctes.<br>\r
-InnerTubeCfg.lbl.longA2 = Cela duplique également tous les composants rattacher à ce tube interne.\r
-InnerTubeCfg.but.Resetsettings = Réinitialiser les réglages\r
-InnerTubeCfg.but.ttip.Resetsettings = Réinitialiser la séparation et la rotation aux valeurs par défauts\r
-\r
-! LaunchLugConfig\r
-LaunchLugCfg.lbl.Length = Longueur:\r
-LaunchLugCfg.lbl.Outerdiam = Diamètre externe:\r
-LaunchLugCfg.lbl.Innerdiam = Diamètre interne:\r
-LaunchLugCfg.lbl.Thickness = Epaisseur:\r
-LaunchLugCfg.lbl.Radialpos = Position circulaire:\r
-LaunchLugCfg.lbl.Posrelativeto = Position relative à:\r
-LaunchLugCfg.lbl.plus = plus\r
-LaunchLugCfg.tab.General = Général\r
-LaunchLugCfg.tab.Generalprop = Propriétés Générales\r
-\r
-! MassComponentConfig\r
-MassComponentCfg.lbl.Mass = Masse\r
-MassComponentCfg.lbl.Length = Longueur\r
-MassComponentCfg.lbl.Diameter = Diamètre\r
-MassComponentCfg.lbl.PosRelativeto = Position relative à:\r
-MassComponentCfg.lbl.plus = plus\r
-MassComponentCfg.tab.General = Général\r
-MassComponentCfg.tab.ttip.General = Propriétés Générales\r
-MassComponentCfg.tab.Radialpos = Position sur le périmètre\r
-MassComponentCfg.tab.ttip.Radialpos = Configuration de la position sur le périmètre\r
-MassComponentCfg.lbl.Radialdistance = Rayon:\r
-MassComponentCfg.lbl.Radialdirection = Azimut:\r
-MassComponentCfg.but.Reset = Réinitialiser\r
-\r
-! MotorConfig\r
-MotorCfg.checkbox.compmotormount = Cette pièce est un porte moteur\r
-MotorCfg.lbl.Motorcfg = Configuration du moteur:\r
-MotorCfg.but.New = Nouveau\r
-MotorCfg.lbl.Currentmotor = Moteur actuel:\r
-MotorCfg.lbl.Motoroverhang = Surplomb du moteur:\r
-MotorCfg.lbl.Ignitionat = Allumage à:\r
-MotorCfg.lbl.plus = plus\r
-MotorCfg.lbl.seconds = secondes\r
-MotorCfg.lbl.longA1 = Le projet actuel n'a qu'un étage.\r
-MotorCfg.lbl.longA2 = Des étages peuvent-être ajoutés en cliquant \"Nouvel étage\".\r
-MotorCfg.lbl.longB1 = Le projet actuel a\r
-MotorCfg.lbl.longB2 = étage(s).\r
-MotorCfg.but.Selectmotor = Choisir le moteur\r
-MotorCfg.but.Removemotor = Enlever le moteur\r
-MotorCfg.lbl.motorLabel = Aucun\r
-\r
-! NoseConeConfig\r
-NoseConeCfg.lbl.Noseconeshape = Forme du cône de la fusée:\r
-NoseConeCfg.lbl.Shapeparam = Paramètre de la forme:\r
-NoseConeCfg.lbl.Noseconelength = Longueur du cône de la fusée:\r
-NoseConeCfg.lbl.Basediam = Diamètre de la base:\r
-NoseConeCfg.checkbox.Automatic = Automatique\r
-NoseConeCfg.lbl.Wallthickness = Epaisseur de la paroi:\r
-NoseConeCfg.checkbox.Filled = Aspérités bouchées\r
-NoseConeCfg.tab.General = Général\r
-NoseConeCfg.tab.ttip.General = Propriétés générales\r
-NoseConeCfg.tab.Shoulder = Accotement\r
-NoseConeCfg.tab.ttip.Shoulder = Propriétés de l'accotement\r
-\r
-! ParachuteConfig\r
-ParachuteCfg.lbl.Canopy = Canopée:\r
-ParachuteCfg.lbl.Diameter = Diamètre:\r
-ParachuteCfg.lbl.Material = Matériau:\r
-ParachuteCfg.combo.MaterialModel = La nature du matériau affecte le poids de la pièce.\r
-ParachuteCfg.lbl.longA1 = <html>Coefficient de traînée C<sub>D</sub>:\r
-ParachuteCfg.lbl.longB1 = <html>Le coefficient de traînée dépend de la surface totale du parachute.<br>\r
-ParachuteCfg.lbl.longB2 = Un plus grand coefficient de trainée produit une descente plus lente. \r
-ParachuteCfg.lbl.longB3 = Une valeur standard pour le parachute est 0.8.\r
-ParachuteCfg.but.Reset = Réinitialiser\r
-ParachuteCfg.lbl.Shroudlines = Suspentes:\r
-ParachuteCfg.lbl.Numberoflines = Nombre de suspentes:\r
-ParachuteCfg.lbl.Linelength = Longueur des suspentes:\r
-ParachuteCfg.lbl.Material = Matériau:\r
-ParachuteCfg.lbl.Posrelativeto = Position relative à:\r
-ParachuteCfg.lbl.plus = plus\r
-ParachuteCfg.lbl.Packedlength = Longueur plié:\r
-ParachuteCfg.lbl.Packeddiam = Diamètre plié:\r
-ParachuteCfg.lbl.Deploysat = Déploiement à:\r
-ParachuteCfg.lbl.seconds = secondes\r
-ParachuteCfg.lbl.Altitude = Altitude:\r
-ParachuteCfg.tab.General = Général\r
-ParachuteCfg.tab.ttip.General = Propriétés générales\r
-ParachuteCfg.tab.Radialpos = Position sur le périmètre\r
-ParachuteCfg.tab.ttip.Radialpos = Configuration de la position radial\r
-ParachuteCfg.lbl.Radialdistance = Rayon:\r
-ParachuteCfg.lbl.Radialdirection = Azimut:\r
-ParachuteCfg.but.Reset = Réinitialiser\r
-ParachuteCfg.lbl.plusdelay = Retard\r
-\r
-! ShockCordConfig \r
-ShockCordCfg.lbl.Shockcordlength = Longueur du cordon amortisseur\r
-ShockCordCfg.lbl.Shockcordmaterial = Matériau du cordon amortisseur:\r
-ShockCordCfg.lbl.Posrelativeto = Position relative à:\r
-ShockCordCfg.lbl.plus = plus\r
-ShockCordCfg.lbl.Packedlength = Longueur emballé:\r
-ShockCordCfg.lbl.Packeddiam = Diamètre emballé:\r
-ShockCordCfg.tab.General = Général\r
-ShockCordCfg.tab.ttip.General = Propriétés générales\r
-\r
-!SleeveConfig\r
-SleeveCfg.tab.Outerdiam = Diamètre externe:\r
-SleeveCfg.tab.Innerdiam = Diamètre interne:\r
-SleeveCfg.tab.Wallthickness = Epaisseur des parois:\r
-SleeveCfg.tab.Length = Longueur:\r
-SleeveCfg.tab.General = Général\r
-SleeveCfg.tab.Generalproperties = Propriétés générales\r
-\r
-! StreamerConfig\r
-StreamerCfg.lbl.Striplength = Longueur de la bande:\r
-StreamerCfg.lbl.Stripwidth = Largeur de la bande:\r
-StreamerCfg.lbl.Striparea = Surface de la bande:\r
-StreamerCfg.lbl.Aspectratio = Proportions:\r
-StreamerCfg.lbl.Material = Matériau:\r
-StreamerCfg.combo.ttip.MaterialModel = La nature du matériau affecte le poids de la pièce.\r
-StreamerCfg.lbl.longA1 = <html>Coefficient de traînée C<sub>D</sub>:\r
-StreamerCfg.lbl.longB1 = <html>Le coefficient de trainée dépend de la surface totale de la banderole.<br>\r
-StreamerCfg.lbl.longB2 = Un plus grand coefficient de trainée produit une descente plus lente.\r
-StreamerCfg.lbl.Automatic = Automatique\r
-StreamerCfg.lbl.longC1 = le coefficient de trainée dépend de la surface totale de la banderole.\r
-StreamerCfg.lbl.Posrelativeto = Position relative à:\r
-StreamerCfg.lbl.plus = plus\r
-StreamerCfg.lbl.Packedlength = Longueur emballé:\r
-StreamerCfg.lbl.Packeddiam = Diamètre emballé:\r
-StreamerCfg.lbl.Deploysat = Déploiement à:\r
-StreamerCfg.lbl.seconds = secondes\r
-StreamerCfg.lbl.Altitude = Altitude:\r
-StreamerCfg.tab.General = Général\r
-StreamerCfg.tab.ttip.General = Propriétés générales\r
-StreamerCfg.tab.Radialpos = Position sur le périmètre\r
-StreamerCfg.tab.ttip.Radialpos = Configuration de la position sur le périmètre\r
-StreamerCfg.lbl.Radialdistance = Rayon:\r
-StreamerCfg.lbl.Radialdirection = Azimut:\r
-StreamerCfg.but.Reset = Réinitialiser\r
-StreamerCfg.lbl.plusdelay = Retard\r
-\r
-! ThicknessRingComponentConfig\r
-ThicknessRingCompCfg.tab.Outerdiam = Diamètre externe:\r
-ThicknessRingCompCfg.tab.Innerdiam = Diamètre interne:\r
-ThicknessRingCompCfg.tab.Wallthickness = Epaisseur de la paroi:\r
-ThicknessRingCompCfg.tab.Length = Longueur:\r
-ThicknessRingCompCfg.tab.General = Général\r
-ThicknessRingCompCfg.tab.Generalprop = Propriétés générales\r
-\r
-! TransitionConfig\r
-TransitionCfg.lbl.Transitionshape = Forme de la transition:\r
-TransitionCfg.checkbox.Clipped = Emboitée\r
-TransitionCfg.lbl.Shapeparam = Paramètre de la forme:\r
-TransitionCfg.lbl.Transitionlength = Longueur de la transition:\r
-TransitionCfg.lbl.Forediam = Diamètre avant:\r
-TransitionCfg.checkbox.Automatic = Automatique\r
-TransitionCfg.lbl.Aftdiam = Diamètre arrière:\r
-TransitionCfg.lbl.Wallthickness = Epaisseur de la paroi:\r
-TransitionCfg.checkbox.Filled = Aspérités bouchées\r
-TransitionCfg.tab.General = Général\r
-TransitionCfg.tab.Generalproperties = Propriétés Générales\r
-TransitionCfg.tab.Shoulder = Accotement\r
-TransitionCfg.tab.Shoulderproperties = Propriétés de l'accotement \r
-\r
-! TrapezoidFinSetConfig\r
-TrapezoidFinSetCfg.lbl.Nbroffins = Nombre d'ailerons:\r
-TrapezoidFinSetCfg.lbl.ttip.Nbroffins = Le nombre d'ailerons composant le jeu.\r
-TrapezoidFinSetCfg.lbl.Finrotation = Rotation de l'aileron:\r
-TrapezoidFinSetCfg.lbl.ttip.Finrotation = Angle du premier aileron dans le jeu.\r
-TrapezoidFinSetCfg.lbl.Fincant = Inclinaison de l'aileron:\r
-TrapezoidFinSetCfg.lbl.ttip.Fincant = Angle d'inclinaison des ailerons par rapport au tube du corps de la fusée.\r
-TrapezoidFinSetCfg.lbl.Rootchord = Longueur de la base de l'aileron:\r
-TrapezoidFinSetCfg.lbl.Tipchord = Longueur du bout de l'aileron:\r
-TrapezoidFinSetCfg.lbl.Height = Hauteur:\r
-TrapezoidFinSetCfg.lbl.Sweeplength = Longueur du bord d'attaque:\r
-TrapezoidFinSetCfg.lbl.Sweepangle = Angle du bord d'attaque:\r
-TrapezoidFinSetCfg.lbl.FincrossSection = Coupe de l'aileron:\r
-TrapezoidFinSetCfg.lbl.Thickness = Epaisseur:\r
-TrapezoidFinSetCfg.lbl.Posrelativeto = Position relative à:\r
-TrapezoidFinSetCfg.lbl.plus = plus\r
-TrapezoidFinSetCfg.tab.General = Général\r
-TrapezoidFinSetCfg.tab.Generalproperties = Propriétés générales\r
-\r
-!MotorConfigurationModel\r
-MotorCfgModel.Editcfg = Modifier les configurations\r
-\r
-! StorageOptionChooser\r
-StorageOptChooser.lbl.Simdatatostore = Données simulées à stocker:\r
-StorageOptChooser.rdbut.Allsimdata = Toutes les données des simulations\r
-StorageOptChooser.lbl.longA1 = <html>Enregistrer toutes les données des simulations.<br>\r
-StorageOptChooser.lbl.longA2 = Cela peut entraîner de très gros fichiers!\r
-StorageOptChooser.rdbut.Every = Every\r
-StorageOptChooser.lbl.longB1 = <html>Store plottable values approximately this far apart.<br>\r
-StorageOptChooser.lbl.longB2 = Des valeurs plus grandes produisent des fichiers plus petits.\r
-StorageOptChooser.lbl.seconds = secondes\r
-StorageOptChooser.rdbut.Onlyprimfig = Seuls les chiffres primaires\r
-StorageOptChooser.lbl.longC1 = <html>Stocker seulement les valeurs montrées dans le tableau récapitulatif.<br>\r
-StorageOptChooser.lbl.longC2 = Cela produira des fichiers plus petit.\r
-StorageOptChooser.checkbox.Compfile = Compresse le fichier\r
-StorageOptChooser.lbl.UsingComp = Utiliser la compression réduit significativement la taille du fichier.\r
-StorageOptChooser.lbl.longD1 = Une estimation sur la taille qu'aurait le fichier résultant avec les options actuelles.\r
-StorageOptChooser.ttip.Saveopt = Options de sauvegarde\r
-StorageOptChooser.lbl.Estfilesize = Taille estimée du fichier:\r
-StorageOptChooser.lbl.Saveopt = Options de sauvegarde\r
-\r
-! ThrustCurveMotorSelectionPanel\r
-TCMotorSelPan.lbl.Selrocketmotor = Choisir le moteur fusée:\r
-TCMotorSelPan.checkbox.hideSimilar = Cacher les courbes de poussées similaires\r
-TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Montrer tous les moteurs\r
-TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Montrer les moteurs avec un diamètre inferieur au porte moteur\r
-TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Montrer les moteurs avec un diamètre égale au porte moteur\r
-TCMotorSelPan.lbl.Motormountdia = Diamètre du tube porte moteur:\r
-TCMotorSelPan.lbl.Search = Rechercher:\r
-TCMotorSelPan.lbl.Selectthrustcurve = Choisir la courbe de poussée:\r
-TCMotorSelPan.lbl.Ejectionchargedelay = Retard de la charge d'éjection:\r
-TCMotorSelPan.equalsIgnoreCase.None = Aucun\r
-TCMotorSelPan.lbl.NumberofsecondsorNone = (Nombre de secondes ou \"Aucun\")\r
-TCMotorSelPan.lbl.Totalimpulse = Impulsion totale:\r
-TCMotorSelPan.lbl.Avgthrust = Poussée moyenne:\r
-TCMotorSelPan.lbl.Maxthrust = Poussée Max.:\r
-TCMotorSelPan.lbl.Burntime = Temps de combustion:\r
-TCMotorSelPan.lbl.Launchmass = Masse au lancement:\r
-TCMotorSelPan.lbl.Emptymass = Masse à vide:\r
-TCMotorSelPan.lbl.Datapoints = Points de données:\r
-TCMotorSelPan.lbl.Digest = Assimilation:\r
-TCMotorSelPan.title.Thrustcurve = Courbe de poussée:\r
-TCMotorSelPan.title.Thrust = Poussée\r
-TCMotorSelPan.delayBox.None = Aucun\r
-\r
-\r
-! PlotDialog\r
-PlotDialog.title.Flightdataplot = Tracé du vol\r
-PlotDialog.Chart.Simulatedflight = Simulation du vol\r
-PlotDialog.CheckBox.Showdatapoints = Afficher un point pour chaque valeur\r
-PlotDialog.lbl.Chart = Cliquer+déplacer en bas +droite pour agrandir, haut+gauche pour rétrécir\r
-\r
-\r
-! "main" prefix is used for the main application dialog\r
-\r
-# FIXME: Rename the description keys \r
-\r
-main.menu.file = Fichier\r
-main.menu.file.desc = File-handling related tasks\r
-main.menu.file.new = Nouveau\r
-main.menu.file.new.desc = Crée un nouveau projet fusée\r
-main.menu.file.open = Ouvrir...\r
-BasicFrame.item.Openrocketdesign = Ouvre un projet fusée\r
-main.menu.file.openExample = Ouvrir un exemple...\r
-BasicFrame.item.Openexamplerocketdesign = Ouvre un exemple de projet fusée\r
-main.menu.file.save = Sauvegarder\r
-BasicFrame.item.SavecurRocketdesign = Sauvegarde le projet fusée en cours\r
-main.menu.file.saveAs = Sauvegarder sous...\r
-BasicFrame.item.SavecurRocketdesnewfile = Sauvegarde le projet fusée en cour dans un nouveau fichier\r
-main.menu.file.print = Imprimer/Exporter en PDF...\r
-main.menu.file.print.desc = Imprimer ou sauvegarde en PDF la liste des pièces et les gabaries des ailerons\r
-main.menu.file.close = Fermer\r
-BasicFrame.item.Closedesign = Ferme le projet fusée en cour\r
-main.menu.file.quit = Quitter\r
-BasicFrame.item.Quitprogram = Quitte le programme\r
-\r
-main.menu.edit = Modifier\r
-BasicFrame.menu.Rocketedt = Modification de la fusée\r
-main.menu.edit.undo = Annuler modification\r
-main.menu.edit.undo.desc = Annuler l'opération précédente\r
-main.menu.edit.redo = Refaire modification\r
-main.menu.edit.redo.desc = Refaire l'opération precedente qui avait été défaite\r
-main.menu.edit.cut = Couper\r
-main.menu.edit.copy = Copier\r
-main.menu.edit.paste = Coller\r
-main.menu.edit.delete = Effacer\r
-main.menu.edit.resize = Redimensionner...\r
-main.menu.edit.resize.desc = Redimensionner certaines parties de la fusée\r
-main.menu.edit.preferences = Préférences\r
-main.menu.edit.preferences.desc = Configure les préférences de l'application\r
-\r
-main.menu.analyze = Analyse\r
-main.menu.analyze.desc = Analyses de la fusée\r
-main.menu.analyze.componentAnalysis = Analyse des Pièces\r
-main.menu.analyze.componentAnalysis.desc = Analyse séparé des pices de la fusée\r
-main.menu.analyze.optimization = Optimisation de la fusée\r
-main.menu.analyze.optimization.desc = Optimisation generale de la fusée\r
-\r
-main.menu.help = Aide\r
-main.menu.help.desc = Information à propos d'OpenRocket\r
-main.menu.help.license = Licence\r
-main.menu.help.license.desc = Information sur la license d'OpenRocket\r
-main.menu.help.bugReport = Rapport d'erreurs\r
-main.menu.help.bugReport.desc = Information pour pouvoir sgnaler les bugs dans OpenRocket\r
-main.menu.help.debugLog = Debug log\r
-main.menu.help.debugLog.desc = Visualiser le fichier log d'OpenRocket\r
-main.menu.help.about = A propos\r
-main.menu.help.about.desc = Détails du Copyright d'OpenRocket\r
-\r
-main.menu.debug = Debug\r
-main.menu.debug.whatisthismenu = Quel est ce menu?\r
-main.menu.debug.createtestrocket = Créer une fusée test\r
-\r
-! database\r
-! Translate here all material database\r
-!\r
-\r
-! Material database\r
-! BULK_MATERIAL\r
-Databases.materials.Acrylic = Acrylique\r
-Databases.materials.Balsa = Balsa\r
-Databases.materials.Birch = Bouleau\r
-Databases.materials.Cardboard = Carton\r
-Databases.materials.Carbonfiber = Fibre de carbone\r
-Databases.materials.Cork = Liège\r
-Databases.materials.DepronXPS = Depron (XPS)\r
-Databases.materials.Fiberglass = Fibre de verre\r
-Databases.materials.Kraftphenolic = Kraft phénolique\r
-Databases.materials.Maple = Érable\r
-Databases.materials.Paperoffice = Papier (bureau)\r
-Databases.materials.Pine = Pin\r
-Databases.materials.Plywoodbirch = Contre-plaqué (bouleau)\r
-Databases.materials.PolycarbonateLexan = Polycarbonate (Lexan)\r
-Databases.materials.Polystyrene = Polystyrène\r
-Databases.materials.PVC = PVC\r
-Databases.materials.Spruce = Sapin\r
-Databases.materials.StyrofoamgenericEPS = Polystyrène (générique EPS)\r
-Databases.materials.StyrofoamBluefoamXPS = \"Mousse Bleue\" de polystyrène (XPS)\r
-Databases.materials.Quantumtubing = Tube Quantum\r
-Databases.materials.BlueTube = Blue tube\r
-!SURFACE_MATERIAL\r
-Databases.materials.Ripstopnylon = Ripstop nylon\r
-Databases.materials.Mylar = Mylar\r
-Databases.materials.Polyethylenethin = Polyéthylène (fin)\r
-Databases.materials.Polyethyleneheavy = Polyéthylène (lourd)\r
-Databases.materials.Silk = Soie\r
-Databases.materials.Paperoffice = Papier (bureau)\r
-Databases.materials.Cellophane = Cellophane\r
-Databases.materials.Crepepaper = Papier crépon\r
-! LINE_MATERIAL\r
-Databases.materials.Threadheavy-duty = Fil(résistant)\r
-Databases.materials.Elasticcordround2mm = Corde Elastique (ronde 2mm, 1/16 in)\r
-Databases.materials.Elasticcordflat6mm = Corde Elastique (plate 6mm, 1/4 in)\r
-Databases.materials.Elasticcordflat12mm = Corde Elastique (plate 12mm, 1/2 in)\r
-Databases.materials.Elasticcordflat19mm = Corde Elastique (plate 19mm, 3/4 in)\r
-Databases.materials.Elasticcordflat25mm = Corde Elastique (plate 25mm, 1 in)\r
-Databases.materials.Braidednylon2mm = Nylon tressé (2 mm, 1/16 in)\r
-Databases.materials.Braidednylon3mm = Nylon tressé (3 mm, 1/8 in)\r
-Databases.materials.Tubularnylon11mm = Nylon tubulaire (11 mm, 7/16 in)\r
-Databases.materials.Tubularnylon14mm = Nylon tubulaire (14 mm, 9/16 in)\r
-Databases.materials.Tubularnylon25mm = Nylon tubulaire (25 mm, 1 in)\r
-\r
-! ExternalComponent\r
-ExternalComponent.Rough = Rugueuse\r
-ExternalComponent.Unfinished = Non peinte\r
-ExternalComponent.Regularpaint = Peinture classique\r
-ExternalComponent.Smoothpaint = Fine couche\r
-ExternalComponent.Polished = Polie\r
-\r
-! LineStyle\r
-LineStyle.Solid = Ligne pleine\r
-LineStyle.Dashed = Tiret\r
-LineStyle.Dotted = Ligne pointillée\r
-LineStyle.Dash-dotted = Ligne Pointillée et Tiret\r
-LineStyle.Defaultstyle = Style par défaut\r
-\r
-! Shape\r
-Shape.Conical = Conique\r
-Shape.Conical.desc1 = Un cône conique a un profil triangulaire.\r
-Shape.Conical.desc2 = Une transition conique a des côtés droits.\r
-Shape.Ogive = Ogive\r
-Shape.Ogive.desc1 = Un cône ogival a un profil qui est un segment de cercle. La valeur du paramètre de forme 1 produit une <b>ogive tangente</b>, qui a une transition en douceur vers le tube de la fusée, des valeurs inférieures à 1 produisent des <b>ogives sécantes</b>.\r
-Shape.Ogive.desc2 = Une transition en ogive a un profil qui est un segment de cercle. La valeur du paramètre de forme 1 produit une <b>ogive tangente</b>, qui a une transition en douceur vers le tube de la fusée à l'extrémité arrière, des valeurs inférieures à 1 produisent des <b>ogives sécantes</b>.\r
-Shape.Ellipsoid = Ellipsoïde\r
-Shape.Ellipsoid.desc1 = Un cône ellipsoïdal a un profil d'une demi ellipse dont les axes principaux sont de longueurs 2×<i>la longueur</i> et <i>diamètre</i>.\r
-Shape.Ellipsoid.desc2 = Une transition ellipsoïdale a un profil d'une demi ellipse dont les axes principaux sont de longueurs 2×<i>longueur</i> et <i>diamètre</i>. Si la transition n'est pas coupée alors le profil est étendu au centre par le rayon correspondant. \r
-Shape.Powerseries = Série Haute puissance\r
-Shape.Powerseries.desc1 = Un cône de puissance a un profil de <i>Rayon</i> × (<i>x</i> / <i>Longueur</i>)<sup><i>k</i></sup> ou <i>k</i> est le paramètre de la forme. Pour <i>k</i>=0,5 c'est une <b>\u00BD-puissance</b> ou une ogive <b>parabolique</b>, pour <i>k</i>=0,75 une <b>\u00BE-puissance</b>, et pour <i>k</i>=1 un cône <b>conique</b>.\r
-Shape.Powerseries.desc2 = Une transition de la série haute puissance a un profile de <i>Rayon</i> × (<i>x</i> / <i>Longueur</i>)<sup><i>k</i></sup> ou <i>k</i> est le paramètre de la forme. Pour <i>k</i>=0,5 la transition est <b>\u00BD-puissance</b> ou <b>parabolique</b>, pour <i>k</i>=0,75 une <b>\u00BE-puissance</b>, et pour <i>k</i>=1 <b>conique</b>.\r
-Shape.Parabolicseries = Série parabolique\r
-Shape.Parabolicseries.desc1 = Un cône parabolique a un profil d'une parabole. Le paramètre de forme définit le segment de la parabole à utiliser. Le paramètre 1 produit une <b>parabole pleine</b> qui est tangent au tube de la fusée, 0,75 produit un <b>3/4 de parabole</b>, 0,5 produit une <b>1/2 parabole</b> et 0 produit un cône <b>conique</b>.\r
-Shape.Parabolicseries.desc2 = Une transition de type parabolique a un profile en forme de parabole. Le paramètre de forme définit le segment de la parabole à utiliser. Le paramètre 1,0 produit une <b>parabole pleine</b> qui est tangent au tube de la fusée à l'extrémité arrière, 0,75 produit une <b>3/4 parabole</b>, 0,5 produit une <b>1/2 parabole</b> et 0 produit une transition <b>conique</b>.\r
-Shape.Haackseries = Série Haack\r
-Shape.Haackseries.desc1 = Les cônes du type Haack sont conçus pour minimiser la trainée. Le paramètre de forme égale à 0 produit une <b>LD-Haack</b> ou un cône <b>Von Karman</b>, ce qui a pour effet de minimiser la trainée pour une longueur et un diamètre fixe, tandis qu'une valeur de 0,333 produit un cône <b>LV-Haack</b>, ce qui minimise la trainée pour une longueur et un volume fixe.\r
-Shape.Haackseries.desc2 = Les <i>cônes</i> du type Haack sont conçus pour minimiser la trainée. Ces formes de transition sont leurs équivalents, mais ne produisent pas nécessairement des valeurs optimales. Le paramètre 0 produit une forme <b>LD-Haack</b> ou <b>Von Karman</b>, tandis qu'une valeur de 0,333 produit une forme <b>LV-Haack</b>. \r
-\r
-\r
-! RocketComponent\r
-RocketComponent.Position.TOP = Haut de la pièce parent\r
-RocketComponent.Position.MIDDLE = Milieu de la pièce parent(porteuse)\r
-RocketComponent.Position.BOTTOM = Bas de la pièce parent\r
-RocketComponent.Position.AFTER = Après la pièce parent\r
-RocketComponent.Position.ABSOLUTE = Pointe de l'ogive\r
-\r
-! LaunchLug\r
-LaunchLug.Launchlug = Tube de guidage\r
-! NoseCone\r
-NoseCone.NoseCone = Ogive\r
-! Transition\r
-Transition.Transition = Transition\r
-!Stage\r
-Stage.Stage = Etage\r
-! BodyTube\r
-BodyTube.BodyTube = Tube du corps\r
-! TubeCoupler\r
-TubeCoupler.TubeCoupler = Coupleur de tube\r
-!InnerTube\r
-InnerTube.InnerTube = Tube interne\r
-! TrapezoidFinSet\r
-TrapezoidFinSet.TrapezoidFinSet = Ailerons Trapézoïdaux\r
-! FreeformFinSet\r
-FreeformFinSet.FreeformFinSet = Ailerons personnalisés\r
-!MassComponent\r
-MassComponent.MassComponent = Poids\r
-! Parachute\r
-Parachute.Parachute = Parachute\r
-! ShockCord\r
-ShockCord.ShockCord = Cordon amortisseur\r
-! Bulkhead\r
-Bulkhead.Bulkhead = Cloison\r
-\r
-!Rocket\r
-Rocket.motorCount.Nomotor = [aucun moteurs]\r
-Rocket.compname.Rocket = Fusée\r
-\r
-!MotorMount\r
-MotorMount.IgnitionEvent.AUTOMATIC = Automatique (lancement ou charge d'éjection)\r
-MotorMount.IgnitionEvent.LAUNCH = Lancement\r
-MotorMount.IgnitionEvent.EJECTION_CHARGE = Première charge d'éjection ou étage précédent\r
-MotorMount.IgnitionEvent.BURNOUT = Première combustion totale de l'étage précédent\r
-MotorMount.IgnitionEvent.NEVER = Jamais\r
-\r
-!ComponentIcons \r
-ComponentIcons.Nosecone = Ogive\r
-ComponentIcons.Bodytube = Tube\r
-ComponentIcons.Transition = Transition\r
-ComponentIcons.Trapezoidalfinset = Jeu d'ailerons de forme trapézoïdale\r
-ComponentIcons.Ellipticalfinset = Jeu d'ailerons de forme elliptique \r
-ComponentIcons.Freeformfinset = Jeu d'ailerons de forme personnalisé\r
-ComponentIcons.Launchlug = Tube de guidage\r
-ComponentIcons.Innertube = Tube interne\r
-ComponentIcons.Tubecoupler = Coupleur de tube\r
-ComponentIcons.Centeringring = Anneau de centrage\r
-ComponentIcons.Bulkhead = Cloison\r
-ComponentIcons.Engineblock = Bague de retension moteur\r
-ComponentIcons.Parachute = Parachute\r
-ComponentIcons.Streamer = Banderolle\r
-ComponentIcons.Shockcord = Cordon amortisseur\r
-ComponentIcons.Masscomponent = Piéce Masse\r
-ComponentIcons.disabled = (désactivé)\r
-\r
-! StageAction\r
-StageAction.Stage = Etage\r
-\r
-! RecoveryDevice\r
-RecoveryDevice.DeployEvent.LAUNCH = Lancement(plus NN secondes)\r
-RecoveryDevice.DeployEvent.EJECTION = Première charge d'éjection de cet étage\r
-RecoveryDevice.DeployEvent.APOGEE = Apogée\r
-RecoveryDevice.DeployEvent.ALTITUDE = Altitude spécifiée durant la descente\r
-RecoveryDevice.DeployEvent.NEVER = Jamais\r
-\r
-! FlightEvent\r
-FlightEvent.Type.LAUNCH = Lancement\r
-FlightEvent.Type.IGNITION = Allumage du moteur\r
-FlightEvent.Type.LIFTOFF = Décollage\r
-FlightEvent.Type.LAUNCHROD = Dégagement de rampe de lancement\r
-FlightEvent.Type.BURNOUT = Fin de combustion du moteur\r
-FlightEvent.Type.EJECTION_CHARGE = Charge d'éjection\r
-FlightEvent.Type.STAGE_SEPARATION = Séparation d'étage\r
-FlightEvent.Type.APOGEE = Apogée\r
-FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Déploiement du dispositif de récupération\r
-FlightEvent.Type.GROUND_HIT = Atterrissage\r
-FlightEvent.Type.SIMULATION_END = Fin de la simulation\r
-FlightEvent.Type.ALTITUDE = Changement d'altitude\r
-\r
-! ThrustCurveMotorColumns\r
-TCurveMotorCol.MANUFACTURER = Fabricant\r
-TCurveMotorCol.DESIGNATION = Désignation\r
-TCurveMotorCol.TYPE = Type\r
-TCurveMotorCol.DIAMETER = Diamètre\r
-TCurveMotorCol.LENGTH = Longueur\r
-\r
-! RocketInfo\r
-RocketInfo.lengthLine.Length = Longueur\r
-RocketInfo.lengthLine.maxdiameter = , diamètre max.\r
-RocketInfo.massText1 = Masse avec moteurs \r
-RocketInfo.massText2 = Masse sans moteurs\r
-RocketInfo.at = à M=\r
-RocketInfo.cgText = CG:\r
-RocketInfo.cpText = CP:\r
-RocketInfo.stabText = Stabilité:\r
-RocketInfo.Warning = Avertissement:\r
-RocketInfo.Calculating = Calcul en cours...\r
-RocketInfo.Apogee = Apogée:\r
-RocketInfo.Maxvelocity = Vitesse Max.:\r
-RocketInfo.Maxacceleration = Accélération Max.:\r
-RocketInfo.apogeeValue = N/A\r
-RocketInfo.Mach = (Mach\r
-RocketInfo.velocityValue = N/A\r
-RocketInfo.accelerationValue = N/A\r
-\r
-! FinSet\r
-FinSet.CrossSection.SQUARE = Carré\r
-FinSet.CrossSection.ROUNDED = Arondie\r
-FinSet.CrossSection.AIRFOIL = Airfoil\r
-FinSet.TabRelativePosition.FRONT = Emplanture avant\r
-FinSet.TabRelativePosition.CENTER = Emplanture centrale\r
-FinSet.TabRelativePosition.END = Emplanture arrière\r
-\r
-! FlightDataType\r
-FlightDataType.TYPE_TIME = Temps\r
-FlightDataType.TYPE_ALTITUDE = Altitude\r
-FlightDataType.TYPE_VELOCITY_Z = Vitesse verticale\r
-FlightDataType.TYPE_ACCELERATION_Z = Accélération verticale\r
-FlightDataType.TYPE_VELOCITY_TOTAL = Vitesse totale\r
-FlightDataType.TYPE_ACCELERATION_TOTAL = Accélération totale\r
-FlightDataType.TYPE_POSITION_X = Position contre le vent\r
-FlightDataType.TYPE_POSITION_Y = Position parallèle au vent\r
-FlightDataType.TYPE_POSITION_XY = Distance latérale\r
-FlightDataType.TYPE_POSITION_DIRECTION = Direction latérale\r
-FlightDataType.TYPE_VELOCITY_XY = Vitesse latérale\r
-FlightDataType.TYPE_ACCELERATION_XY = Accélération latérale\r
-FlightDataType.TYPE_AOA = Angle d'attaque\r
-FlightDataType.TYPE_ROLL_RATE = Taux de roulis\r
-FlightDataType.TYPE_PITCH_RATE = Taux de tangage\r
-FlightDataType.TYPE_YAW_RATE = Taux d'embardée\r
-FlightDataType.TYPE_MASS = Masse\r
-FlightDataType.TYPE_LONGITUDINAL_INERTIA = Moment d'inertie longitudinale\r
-FlightDataType.TYPE_ROTATIONAL_INERTIA = Moment d'inertie rotatif\r
-FlightDataType.TYPE_CP_LOCATION = Emplacement du CP\r
-FlightDataType.TYPE_CG_LOCATION = Emplacement du CG\r
-FlightDataType.TYPE_STABILITY = Calibres marge de stabilité\r
-FlightDataType.TYPE_MACH_NUMBER = Mach number\r
-FlightDataType.TYPE_REYNOLDS_NUMBER = Nombre de Reynolds\r
-FlightDataType.TYPE_THRUST_FORCE = Poussée\r
-FlightDataType.TYPE_DRAG_FORCE = Force de traînée\r
-FlightDataType.TYPE_DRAG_COEFF = Coefficient de traînée\r
-FlightDataType.TYPE_AXIAL_DRAG_COEFF = Coefficient de trainée axiale\r
-FlightDataType.TYPE_FRICTION_DRAG_COEFF = Coefficient de traînée de friction\r
-FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Coefficient de traînée de pression\r
-FlightDataType.TYPE_BASE_DRAG_COEFF = Coefficient de traînée de base\r
-FlightDataType.TYPE_NORMAL_FORCE_COEFF = Coefficient de force normale\r
-FlightDataType.TYPE_PITCH_MOMENT_COEFF = Coefficient de moment de tangage\r
-FlightDataType.TYPE_YAW_MOMENT_COEFF = Coefficient de moment d'embardée \r
-FlightDataType.TYPE_SIDE_FORCE_COEFF = Coefficient de force latérale \r
-FlightDataType.TYPE_ROLL_MOMENT_COEFF = Coefficient de moment de roulis \r
-FlightDataType.TYPE_ROLL_FORCING_COEFF = Coefficient de forçage de roulis\r
-FlightDataType.TYPE_ROLL_DAMPING_COEFF = Coefficient d'amortissement de roulis\r
-FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Coefficient d'amortissement de tangage\r
-FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Coefficient d'amortissement d'embardée\r
-FlightDataType.TYPE_REFERENCE_LENGTH = Longueur de référence\r
-FlightDataType.TYPE_REFERENCE_AREA = Surface de référence\r
-FlightDataType.TYPE_ORIENTATION_THETA = Orientation verticale (zénith)\r
-FlightDataType.TYPE_ORIENTATION_PHI = Orientation latérale (azimut)\r
-FlightDataType.TYPE_WIND_VELOCITY = Vitesse de vent\r
-FlightDataType.TYPE_AIR_TEMPERATURE = Température de l'air\r
-FlightDataType.TYPE_AIR_PRESSURE = Pression atmosphérique\r
-FlightDataType.TYPE_SPEED_OF_SOUND = Vitesse du son\r
-FlightDataType.TYPE_TIME_STEP = Pas de simulation du temps\r
-FlightDataType.TYPE_COMPUTATION_TIME = Temps de calcul\r
-FlightDataType.TYPE_LATITUDE = Latitude\r
-FlightDataType.TYPE_LONGITUDE = Longitude\r
-FlightDataType.TYPE_CORIOLIS_ACCELERATION = Accélération de Coriolis\r
-\r
-! PlotConfiguration\r
-PlotConfiguration.Verticalmotion = Mouvement vertical par rapport au temps\r
-PlotConfiguration.Totalmotion = Mouvement total par rapport au temps\r
-PlotConfiguration.Flightside = Profil latéral du vol\r
-PlotConfiguration.Stability = Stabilité par rapport au temps\r
-PlotConfiguration.Dragcoef = Coefficients de traînée par rapport au Mach number\r
-PlotConfiguration.Rollcharacteristics = Caractéristiques de roulis\r
-PlotConfiguration.Angleofattack = Angle d'attaque et orientation par rapport au temps\r
-PlotConfiguration.Simulationtime = Pas du temps et temps de calcul\r
-\r
-! Warning\r
-Warning.LargeAOA.str1 = Grand angle d'attaque rencontré.\r
-Warning.LargeAOA.str2 = Grand angle d'attaque rencontré (\r
-Warning.DISCONTINUITY = Discontinuité dans le diamètre du corps de la fusée.\r
-Warning.THICK_FIN = Les ailerons fin ne seront peut être pas modélisés correctement.\r
-Warning.JAGGED_EDGED_FIN = Des ailerons aux bords irréguliers ne seront pas modélisés correctement.\r
-Warning.LISTENERS_AFFECTED = Listeners modified the flight simulation\r
-Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Le dispositif de récupération s'est ouvert alors que la combustion du moteur n'était pas finie.\r
-Warning.FILE_INVALID_PARAMETER = Paramètre invalide rencontré, ignorer.\r
-\r
-\r
-! Scale dialog\r
-ScaleDialog.lbl.scaleRocket = Fusée entière\r
-ScaleDialog.lbl.scaleSubselection = La sélection et tous ses composants \r
-ScaleDialog.lbl.scaleSelection = Seulement les composants sélectionnés\r
-ScaleDialog.title = Redimensionner le projet\r
-ScaleDialog.lbl.scale = Mise à l'échelle:\r
-ScaleDialog.lbl.scale.ttip = Choisir de redimensionner tout le projet ou seulement la pièce choisie\r
-ScaleDialog.lbl.scaling = Echelle à appliquer:\r
-ScaleDialog.lbl.scaling.ttip = Taille résultante,les valeurs au-dessus de 100% agrandissent et les valeurs en-dessous de 100% réduisent le design.\r
-! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"\r
-ScaleDialog.lbl.scaleFrom = Mise à l'échelle de \r
-ScaleDialog.lbl.scaleTo = à\r
-ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and resulting length.\r
-ScaleDialog.checkbox.scaleMass = Update explicit mass values\r
-ScaleDialog.checkbox.scaleMass.ttip = Scale mass component and override mass values by the cube of the scaling factor\r
-ScaleDialog.button.scale = Redimensionner\r
-ScaleDialog.undo.scaleRocket = Redimensionner la fusée\r
-ScaleDialog.undo.scaleComponent = Redimensionner une pièce\r
-ScaleDialog.undo.scaleComponents = Redimensionner les pièces\r
-\r
-!icons\r
-Icons.Undo = Undo\r
-Icons.Redo = Redo\r
-\r
-OpenRocketPrintable.Partsdetail = Détail des pièces\r
-OpenRocketPrintable.Fintemplates = Gabaries des ailerons\r
-OpenRocketPrintable.DesignReport = Rapport de conception\r
-\r
-OpenRocketDocument.Redo = Refaire\r
-OpenRocketDocument.Undo = Défaire\r
-\r
-!EllipticalFinSet\r
-EllipticalFinSet.Ellipticalfinset = Ailerons elliptique\r
-\r
-! Optimization\r
-\r
-! Modifiers\r
-\r
-optimization.modifier.nosecone.length = Longueur du cône\r
-optimization.modifier.nosecone.length.desc = Optimise la longueur du cône.\r
-optimization.modifier.nosecone.diameter = Diamètre du cône\r
-optimization.modifier.nosecone.diameter.desc = Optimise le diamètre du cône.\r
-optimization.modifier.nosecone.thickness = Epaisseur du cône\r
-optimization.modifier.nosecone.thickness.desc = Optimise l'épaisseur des parois du cône.\r
-optimization.modifier.nosecone.shapeparameter = Paramètre de la forme\r
-optimization.modifier.nosecone.shapeparameter.desc = Optimise les paramètres de forme du cône.\r
- \r
-optimization.modifier.transition.length = Longueur de la Transition\r
-optimization.modifier.transition.length.desc = Optimise la longueur de la transition.\r
-optimization.modifier.transition.forediameter = Diamètre avant de la Transition\r
-optimization.modifier.transition.forediameter.desc = Optimise le diamètre avant de la transition.\r
-optimization.modifier.transition.aftdiameter = Diamètre arrière de la transition\r
-optimization.modifier.transition.aftdiameter.desc = Optimise le diamètre arrière de la transition.\r
-optimization.modifier.transition.thickness = Epaisseur de la transition\r
-optimization.modifier.transition.thickness.desc = Optimise l'épaisseur des parois de la transition.\r
-optimization.modifier.transition.shapeparameter = Paramètre de la forme\r
-optimization.modifier.transition.shapeparameter.desc = Optimise le paramètre de la forme.\r
-\r
-optimization.modifier.bodytube.length = Longueur du tube du corps\r
-optimization.modifier.bodytube.length.desc = Optimise la longueur du tube du corps.\r
-optimization.modifier.bodytube.outerDiameter = Diamètre externe du tube du corps\r
-optimization.modifier.bodytube.outerDiameter.desc = Optimise le diamètre externe du tube du corps tout en maintenant l'épaisseur des parois.\r
-optimization.modifier.bodytube.innerDiameter = Diamètre interne du tube du corps\r
-optimization.modifier.bodytube.thickness = Epaisseur du tube du corps\r
-optimization.modifier.bodytube.thickness.desc = Optimise l'épaisseur des parois du tube du corps.\r
-\r
-optimization.modifier.trapezoidfinset.rootChord = Root chord\r
-optimization.modifier.trapezoidfinset.rootChord.desc = Optimize the root chord length of the fin set (length of fin at the rocket body).\r
-optimization.modifier.trapezoidfinset.tipChord = Tip chord\r
-optimization.modifier.trapezoidfinset.tipChord.desc = Optimize the tip chord length of the fin set (length of fin at outer edge).\r
-optimization.modifier.trapezoidfinset.sweep = Sweep\r
-optimization.modifier.trapezoidfinset.sweep.desc = Optimize the sweep of the fin set (distance that the leading edge sweeps backwards).\r
-optimization.modifier.trapezoidfinset.height = Hauteur\r
-optimization.modifier.trapezoidfinset.height.desc = Optimize the height (semi-span) of the fin set.\r
-\r
-optimization.modifier.ellipticalfinset.length = Root chord\r
-optimization.modifier.ellipticalfinset.length.desc = Optimize the root chord length of the fin set.\r
-optimization.modifier.ellipticalfinset.height = Hauteur\r
-optimization.modifier.ellipticalfinset.height.desc = Optimize the height (semi-span) of the fin set.\r
-\r
-optimization.modifier.finset.cant = Cant angle\r
-optimization.modifier.finset.cant.desc = Optimize the cant angle of the fin set.\r
-optimization.modifier.finset.position = Position\r
-optimization.modifier.finset.position.desc = Optimisation de la position du jeux d'ailerons sur le corps de la fusée.\r
-\r
-optimization.modifier.launchlug.length = Longueur\r
-optimization.modifier.launchlug.length.desc = Optimisation de la longueur du tube de guidage.\r
-optimization.modifier.launchlug.outerDiameter = Diamètre externe\r
-optimization.modifier.launchlug.outerDiameter.desc = Optimisation du diamètre externe du tube de guidage.\r
-optimization.modifier.launchlug.thickness = Epaisseur\r
-optimization.modifier.launchlug.thickness.desc = Optimise l'épaisseur de la bague de guide tout en gardant le diamètre extérieur constant.\r
-optimization.modifier.launchlug.position = Position\r
-optimization.modifier.launchlug.position.desc = Optimise la position de la bague de guidage le long du corps de la fusée.\r
-\r
-\r
-optimization.modifier.internalcomponent.position = Position\r
-optimization.modifier.internalcomponent.position.desc = Optimise la position de la pièce par rapport à la pièce parent.\r
-\r
-optimization.modifier.masscomponent.mass = Masse\r
-optimization.modifier.masscomponent.mass.desc = Optimise la masse du composant.\r
-\r
-optimization.modifier.parachute.diameter = Diamètre\r
-optimization.modifier.parachute.diameter.desc = Optimise le diamètre de la coupole du parachute.\r
-optimization.modifier.parachute.coefficient = Coefficient de trainée\r
-optimization.modifier.parachute.coefficient.desc = Optimisation du coefficient de trainée du parachute. Un parachute type à un coefficient de trainée d'environ 0.8.\r
-\r
-optimization.modifier.streamer.length = Longueur\r
-optimization.modifier.streamer.length.desc = Optimisation de la longueur de la banderole (streamer).\r
-optimization.modifier.streamer.width = Largeur\r
-optimization.modifier.streamer.width.desc = Optimisation de la largeur de la banderole (streamer).\r
-optimization.modifier.streamer.aspectRatio = Aspect ratio\r
-optimization.modifier.streamer.aspectRatio.desc = Optimize the aspect ratio of the streamer (length/width). You should NOT select streamer length or width at the same time with the aspect ratio.\r
-optimization.modifier.streamer.coefficient = Coefficient de trainée\r
-optimization.modifier.streamer.coefficient.desc = Optimisation du coéfficient de trainée de la banderole (streamer).\r
-\r
-optimization.modifier.recoverydevice.deployDelay = Retard du déploiement\r
-optimization.modifier.recoverydevice.deployDelay.desc = Optimise le délai du déploiement du système du récupération.\r
-optimization.modifier.recoverydevice.deployAltitude = Altitude du déploiement\r
-optimization.modifier.recoverydevice.deployAltitude.desc = Optimise l'altitude de déploiement du dispositif de récupération.\r
-\r
-optimization.modifier.rocketcomponent.overrideMass = Forcer la masse\r
-optimization.modifier.rocketcomponent.overrideMass.desc = Optimise le forçage de la masse du composant.\r
-optimization.modifier.rocketcomponent.overrideCG = forcer le CG\r
-optimization.modifier.rocketcomponent.overrideCG.desc = Optimise le forçage du centre de gravité du composant.\r
-\r
-optimization.modifier.motormount.overhang = Surplomb du moteur\r
-optimization.modifier.motormount.overhang.desc = Optimise le surplomb du moteur.\r
-optimization.modifier.motormount.delay = Retard de l'allumage moteur\r
-optimization.modifier.motormount.delay.desc = Optimisation du retard d'allumage du moteur.\r
-\r
-\r
-\r
-\r
-! General rocket design optimization dialog\r
-\r
-GeneralOptimizationDialog.title = Optimisation de la fusée\r
-GeneralOptimizationDialog.goal.maximize = Maximiser la valeur\r
-GeneralOptimizationDialog.goal.minimize = Minimiser la valeur\r
-GeneralOptimizationDialog.goal.seek = Cherchez la valeur de\r
-GeneralOptimizationDialog.btn.start = Démarrer l'optimisation\r
-GeneralOptimizationDialog.btn.stop = Terminer l'optimisation\r
-GeneralOptimizationDialog.lbl.paramsToOptimize = Paramètres à optimiser:\r
-GeneralOptimizationDialog.btn.add = Ajouter\r
-GeneralOptimizationDialog.btn.add.ttip = Ajouter le paramètre sélectionné aux paramètres à optimiser\r
-GeneralOptimizationDialog.btn.remove = Enlever\r
-GeneralOptimizationDialog.btn.remove.ttip = Enlever le paramètre sélectionné des paramètres à optimiser\r
-GeneralOptimizationDialog.btn.removeAll = Tout enlever\r
-GeneralOptimizationDialog.btn.removeAll.ttip = Enlever tous les paramètres de l'optimisation\r
-GeneralOptimizationDialog.lbl.availableParams = Paramètres disponible:\r
-GeneralOptimizationDialog.lbl.optimizationOpts = Options pour l'optimisation\r
-GeneralOptimizationDialog.lbl.optimizeSim = Optimiser la simulation:\r
-GeneralOptimizationDialog.lbl.optimizeSim.ttip = Choisir la simulation à optimiser\r
-GeneralOptimizationDialog.lbl.optimizeValue = Valeur optimum\r
-GeneralOptimizationDialog.lbl.optimizeValue.ttip = Choisir quelle valeur à optimiser\r
-GeneralOptimizationDialog.lbl.optimizeGoal = But de l'optimisation:\r
-GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Choisir le but de l'optimisation\r
-GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Valeur personnalisée à rechercher\r
-GeneralOptimizationDialog.lbl.requireStability = Stabilité désirée\r
-GeneralOptimizationDialog.lbl.requireMinStability = Stabilité minimum:\r
-GeneralOptimizationDialog.lbl.requireMinStability.ttip = Exiger une marge de stabilité statique minimale pour le design\r
-GeneralOptimizationDialog.lbl.requireMaxStability = Stabilité maximum:\r
-GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Exiger une marge de stabilité statique maximale pour le design\r
-GeneralOptimizationDialog.status.bestValue = Meilleure valeur:\r
-GeneralOptimizationDialog.status.bestValue.ttip = Meilleure valeur optimum trouvé jusqu'à présent.\r
-GeneralOptimizationDialog.status.stepCount = Step count:\r
-GeneralOptimizationDialog.status.stepCount.ttip = Number of optimization steps that have been performed.\r
-GeneralOptimizationDialog.status.evalCount = Evaluations:\r
-GeneralOptimizationDialog.status.evalCount.ttip = Total number of function evaluations (simulations) that have been performed.\r
-GeneralOptimizationDialog.status.stepSize = Step size:\r
-GeneralOptimizationDialog.status.stepSize.ttip = Current optimization step size (relative to the optimization parameter ranges)\r
-GeneralOptimizationDialog.btn.plotPath = Plot path\r
-GeneralOptimizationDialog.btn.plotPath.ttip = Plot the optimization path (one and two dimensional optimization only)\r
-GeneralOptimizationDialog.btn.save = Save path\r
-GeneralOptimizationDialog.btn.save.ttip = Save the results of the function evaluations (simulations) as a CSV file.\r
-GeneralOptimizationDialog.btn.apply = Appliquer l'optimisation\r
-GeneralOptimizationDialog.btn.apply.ttip = Appliquer les résultats de l'optimisation au design de la fusée\r
-GeneralOptimizationDialog.btn.reset = Re-Réinitialiser\r
-GeneralOptimizationDialog.btn.reset.ttip = Réinitialiser le design de la fusée au design actuel de la fusée\r
-GeneralOptimizationDialog.btn.close = Fermer\r
-GeneralOptimizationDialog.btn.close.ttip = Fermer la fenêtre de dialogue sans modifier la fusée\r
-GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters.\r
-GeneralOptimizationDialog.error.selectParams.title = Choisir les paramètres de l'optimisation\r
-GeneralOptimizationDialog.error.optimizationFailure.text = L'optimisation n'a pas fonctionnée:\r
-GeneralOptimizationDialog.error.optimizationFailure.title = L'optimisation n'a pas réussie\r
-GeneralOptimizationDialog.undoText = Appliquer l'optimisation\r
-GeneralOptimizationDialog.basicSimulationName = Simulation simple\r
-GeneralOptimizationDialog.noSimulationName = Pas de simulation\r
-GeneralOptimizationDialog.table.col.parameter = Paramètre\r
-GeneralOptimizationDialog.table.col.current = Courant\r
-GeneralOptimizationDialog.table.col.min = Minimum\r
-GeneralOptimizationDialog.table.col.max = Maximum\r
-GeneralOptimizationDialog.export.header = Inclure la ligne d'en tête\r
-GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions.\r
-GeneralOptimizationDialog.export.stability = Stabilité\r
-\r
-\r
-! Dialog for plotting optimization results\r
-OptimizationPlotDialog.title = Résultats de l'optimisation\r
-OptimizationPlotDialog.lbl.zoomInstructions = Click et glisser en bas et à droite pour zoomer plus, en haut et à gauche pour zoomer moins\r
-OptimizationPlotDialog.plot1d.title = Résultat de l'optimisation\r
-OptimizationPlotDialog.plot1d.series = Résultat de l'optimisation\r
-OptimizationPlotDialog.plot2d.title = Optimization path\r
-OptimizationPlotDialog.plot2d.path = Chemin pour l'optimisation\r
-OptimizationPlotDialog.plot2d.evals = Evaluations\r
-OptimizationPlotDialog.plot.ttip.stability = Stabilité:\r
-OptimizationPlotDialog.plot.label.optimum = Optimum\r
-\r
-! Optimization parameters\r
-MaximumAltitudeParameter.name = Altitude de l'apogée\r
-MaximumVelocityParameter.name = Vitesse maximum\r
-MaximumAccelerationParameter.name = Accélération maximum\r
-StabilityParameter.name = Stabilité\r
-GroundHitVelocityParameter.name = Vitesse à l'atterrissage\r
-LandingDistanceParameter.name = Distance à l'atterrissage\r
-TotalFlightTimeParameter.name = Durée totale du vol\r
-DeploymentVelocityParameter.name = Vitesse lors de l'ouverture du parachute\r
-\r
-\r
-! Compass directions drawn on a compass rose.\r
-CompassRose.lbl.north = N\r
-CompassRose.lbl.east = E\r
-CompassRose.lbl.south = S\r
-CompassRose.lbl.west = O\r
-\r
-! Compass directions with subdirections. These might not be localized even if the directions on the compass rose are.\r
-CompassSelectionButton.lbl.N = N\r
-CompassSelectionButton.lbl.NE = NE\r
-CompassSelectionButton.lbl.E = E\r
-CompassSelectionButton.lbl.SE = SE\r
-CompassSelectionButton.lbl.S = S\r
-CompassSelectionButton.lbl.SW = SO\r
-CompassSelectionButton.lbl.W = O\r
-CompassSelectionButton.lbl.NW = NO\r
-\r
-\r
-SlideShowDialog.btn.next = Suivant\r
-SlideShowDialog.btn.prev = Précédent\r
-\r
-GuidedTourSelectionDialog.title = Tours d'horizon\r
-GuidedTourSelectionDialog.lbl.selectTour = Choisir un tour d'horizon:\r
-GuidedTourSelectionDialog.lbl.description = Description du tour d'horizon:\r
-GuidedTourSelectionDialog.lbl.length = Nombre de diapositives:\r
-GuidedTourSelectionDialog.btn.start = Commencer le tour d'horizon!\r
projects / debian / openrocket / commitdiff