From: kruland2607 Date: Wed, 11 Jan 2012 03:26:17 +0000 (+0000) Subject: Move l10n/ in to resources/. X-Git-Tag: upstream/12.03~1^2~137 X-Git-Url: https://git.gag.com/?a=commitdiff_plain;h=a707b6ac1dc37d0892496b0132ad49f3b7328786;p=debian%2Fopenrocket Move l10n/ in to resources/. git-svn-id: https://openrocket.svn.sourceforge.net/svnroot/openrocket/trunk@334 180e2498-e6e9-4542-8430-84ac67f01cd8 --- diff --git a/core/l10n/messages.properties b/core/l10n/messages.properties deleted file mode 100644 index 3a51de44..00000000 --- a/core/l10n/messages.properties +++ /dev/null @@ -1,1546 +0,0 @@ - -# -# 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 = This operation cannot be undone. -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 = 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 = If connected to the Internet, you can simply click Send bug report. -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 = You can report a bug in OpenRocket by filling in and submitting the form below.
You can also report bugs and include attachments on the project web site. -bugreport.reportDialog.txt2 = Please include a short description about what you were doing when the exception occurred. -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 = Motor mounts: -edtmotorconfdlg.title.Editmotorconf = Edit motor configurations -edtmotorconfdlg.selectcomp = Select which components function as motor mounts: -edtmotorconfdlg.lbl.Motorconfig = Motor configurations: -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 = The standard deviation of the windspeed.
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 = The turbulence intensity is the standard deviation divided by the average windspeed.
-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 = Select to use the International Standard Atmosphere model.
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 = The launch site latitude affects the gravitational pull of Earth.
Positive values are on the Northern hemisphere, negative values on the Southern hemisphere. - -simedtdlg.lbl.Longitude = Longitude: -simedtdlg.lbl.ttip.Longitude = Required for weather prediction and elevation models. - -simedtdlg.lbl.Altitude = Altitude: -simedtdlg.lbl.ttip.Altitude = The launch altitude above mean sea level.
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 = Direction of the launch rod relative to the wind.
-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 = The Extended Barrowman method calculates aerodynamic forces according
to the Barrowman equations extended to accommodate more components. -simedtdlg.lbl.ExtBarrowman = Extended Barrowman -simedtdlg.lbl.Simmethod = Simulation method: -simedtdlg.lbl.ttip.Simmethod1 = The six degree-of-freedom simulator allows the rocket total freedom during flight.
-simedtdlg.lbl.ttip.Simmethod2 = Integration is performed using a 4th 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 = The time between simulation steps.
A smaller time step results in a more accurate but slower simulation.
-simedtdlg.lbl.ttip.Timestep2 = The 4th 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 = Simulation listeners 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 = Perform geodetic computations assuming a spherical Earth.
This is sufficiently accurate for almost all purposes. -GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid -GeodeticComputationStrategy.wgs84.desc = Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.
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 = This operation cannot be undone. -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 = The string used to separate the fields in the exported file.
-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 = Pressure CD -componentanalysisdlg.dragTableModel.Col.Base = Base CD -componentanalysisdlg.dragTableModel.Col.friction = Friction CD -componentanalysisdlg.dragTableModel.Col.total = Total CD -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 = Total Cl -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 = An engine block stops the motor from moving forwards in the motor mount tube.

In order to add a motor, create a body tube or inner tube and mark it as a motor mount in the Motor 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 = The component finish affects the aerodynamic drag of the component.
-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 = The overridden mass does not include motors.
-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 = Split the cluster into separate components.
-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 = Drag coefficient CD: -ParachuteCfg.lbl.longB1 = The drag coefficient relative to the total area of the parachute.
-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 = Drag coefficient CD: -StreamerCfg.lbl.longB1 = The drag coefficient relative to the total area of the streamer.
-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 = Store all simulated data.
-StorageOptChooser.lbl.longA2 = This can result in very large files! -StorageOptChooser.rdbut.Every = Every -StorageOptChooser.lbl.longB1 = Store plottable values approximately this far apart.
-StorageOptChooser.lbl.longB2 = Larger values result in smaller files. -StorageOptChooser.lbl.seconds = seconds -StorageOptChooser.rdbut.Onlyprimfig = Only primary figures -StorageOptChooser.lbl.longC1 = Store only the values shown in the summary table.
-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 tangent ogive, which has a smooth transition to the body tube, values less than 1 produce secant ogives. -Shape.Ogive.desc2 = An ogive transition has a profile that is a segment of a circle. The shape parameter value 1 produces a tangent ogive, which has a smooth transition to the body tube at the aft end, values less than 1 produce secant ogives. -Shape.Ellipsoid = Ellipsoid -Shape.Ellipsoid.desc1 = An ellipsoidal nose cone has a profile of a half-ellipse with major axes of lengths 2×Length and Diameter. -Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×Length and Diameter. 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 Radius × (x / Length)k where k is the shape parameter. For k=0.5 this is a \u00BD-power or parabolic nose cone, for k=0.75 a \u00BE-power, and for k=1 a conical nose cone. -Shape.Powerseries.desc2 = A power series transition has a profile of Radius × (x / Length)k where k is the shape parameter. For k=0.5 the transition is \u00BD-power or parabolic, for k=0.75 a \u00BE-power, and for k=1 conical. -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 full parabola which is tangent to the body tube, 0.75 produces a 3/4 parabola, 0.5 procudes a 1/2 parabola and 0 produces a conical 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 full parabola which is tangent to the body tube at the aft end, 0.75 produces a 3/4 parabola, 0.5 procudes a 1/2 parabola and 0 produces a conical transition. -Shape.Haackseries = Haack series -Shape.Haackseries.desc1 = The Haack series nose cones are designed to minimize drag. The shape parameter 0 produces an LD-Haack or Von Karman nose cone, which minimizes drag for fixed length and diameter, while a value of 0.333 produces an LV-Haack nose cone, which minimizes drag for fixed length and volume. -Shape.Haackseries.desc2 = The Haack series nose cones 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 LD-Haack or Von Karman shape, while a value of 0.333 produces an LV-Haack 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! - - diff --git a/core/l10n/messages_de.properties b/core/l10n/messages_de.properties deleted file mode 100644 index 0b972fc1..00000000 --- a/core/l10n/messages_de.properties +++ /dev/null @@ -1,1528 +0,0 @@ - -# -# German base translation file -# -# 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_de.properties - -! RocketActions -RocketActions.checkbox.Donotaskmeagain = Nicht wieder fragen -RocketActions.lbl.Youcanchangedefop = Die Standardaktion kann in den Einstellungen geändert werden. -RocketActions.showConfirmDialog.lbl1 = Simulationen löschen? -RocketActions.showConfirmDialog.lbl2 = Diese Aktion kann nicht rückgängig gemacht werden. -RocketActions.showConfirmDialog.title = Simulationen löschen -RocketActions.DelCompAct.Delete = Löschen -RocketActions.DelCompAct.ttip.Delete = Die ausgewählte Komponente löschen. -RocketActions.DelSimuAct.Delete = Löschen -RocketActions.DelSimuAct.ttip.Delete = Die ausgewählte Simulation löschen. -RocketActions.DelAct.Delete = Löschen -RocketActions.DelAct.ttip.Delete = Die ausgewählte Komponente oder Simulation löschen. -RocketActions.CutAction.Cut = Ausschneiden -RocketActions.CutAction.ttip.Cut = Diese Komponente oder Simulation ausschneiden und aus dem Design entfernen -RocketActions.CopyAct.Copy = Kopieren -RocketActions.CopyAct.ttip.Copy = Komponente (und Subkomponenten) in die Zwischenablage kopieren. -RocketActions.PasteAct.Paste = Einfügen -RocketActions.PasteAct.ttip.Paste = Fügt die Komponente oder Simulation aus der Zwischenablage in das Design ein. -RocketActions.EditAct.Edit = Bearbeiten -RocketActions.EditAct.ttip.Edit = Die ausgewählte Komponente bearbeiten. -RocketActions.NewStageAct.Newstage = Neue Stufe -RocketActions.NewStageAct.ttip.Newstage = Fügt eine neue Stufe in das Raketendesign ein. -RocketActions.ActBoosterstage = Booster-Stufe -RocketActions.MoveUpAct.Moveup = Nach oben verschieben -RocketActions.MoveUpAct.ttip.Moveup = Verschiebt diese Komponente nach oben. -RocketActions.MoveDownAct.Movedown = Nach unten verschieben -RocketActions.MoveDownAct.ttip.Movedown = Verschiebt diese Komponente nach unten. - -! RocketPanel -RocketPanel.FigTypeAct.Sideview = Seitenansicht -RocketPanel.FigTypeAct.ttip.Sideview = Seitenansicht -RocketPanel.FigTypeAct.Backview = Rückansicht -RocketPanel.FigTypeAct.ttip.Backview = Vorderansicht -RocketPanel.lbl.Motorcfg = Motorkonfiguration -RocketPanel.lbl.infoMessage = Zum Auswählen klicken   Shift+Klick andere auswählen    Doppelklick zum Bearbeiten    Klicken+Ziehen zum Verschieben - - -! BasicFrame -BasicFrame.SimpleFileFilter1 = Alle Raketendesigns (*.ork; *.rkt) -BasicFrame.SimpleFileFilter2 = OpenRocket Designs (*.ork) -BasicFrame.SimpleFileFilter3 = RockSim Designs (*.rkt) -BasicFrame.tab.Rocketdesign = Raketendesign -BasicFrame.tab.Flightsim = Flugsimulation -BasicFrame.title.Addnewcomp = Neue Komponente hinzufügen -BasicFrame.dlg.lbl1 = Design ' -BasicFrame.dlg.lbl2 = ' ist nicht gespeichert. -BasicFrame.dlg.lbl3 = Möchten Sie es speichern? -BasicFrame.dlg.title = Design nicht gespeichert -BasicFrame.StageName.Sustainer = Hauptstufe -BasicFrame.WarningDialog.txt1 = Die folgenden Probleme würden beim Öffnen festgestellt -BasicFrame.WarningDialog.txt2 = Einige Designeigenschaften wurde eventuell nicht korrekt geladen. -BasicFrame.WarningDialog.title = Warnungen während des Öffnens der Datei - - -! 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 -button.ok = OK -button.cancel = Abbrechen -button.close = Schließen - -! Common labels used in buttons of dialog windows -dlg.but.ok = OK -dlg.but.cancel = Abbrechen -dlg.but.close = Schließen - - -! 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 = Ins Deutsche übersetzt von: -AboutDialog.lbl.translator = Stefan Lobas (ERIG e.V.) -AboutDialog.lbl.translatorWebsite = http://www.er-ig.de/ -AboutDialog.lbl.translatorIcon = ERIG_Logo-small.png - - -! Print dialog -PrintDialog.title = Drucken oder exportieren -PrintDialog.but.previewAndPrint = Vorschau & Drucken -PrintDialog.checkbox.showByStage = In Stufen anzeigen -PrintDialog.lbl.selectElements = Elemente auswählen, die berücksichtigt werden sollen: -printdlg.but.saveaspdf = Als PDF speichern -printdlg.but.preview = Vorschau -printdlg.but.settings = Einstellungen -PrintDialog.error.preview.title = Vorschau kann nicht geöffnet werden -PrintDialog.error.preview.desc1 = PDF-Vorschau kann nicht geöffnet werden -PrintDialog.error.preview.desc2 = Bitte "Als PDF speichern" benutzen. - - -!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 = Fehlerbericht -bugreport.dlg.but.Sendbugreport = Fehlerbericht senden -bugreport.dlg.but.Sendbugreport.Ttip = Automatische einen Fehlerbericht an die OpenRocket-Entwickler senden. -bugreport.dlg.successmsg1 = Fehlerbericht erfolgreich gesendet. -bugreport.dlg.successmsg2 = Danke für die Hilfe, OpenRocket noch besser zu machen! -bugreport.dlg.successmsg3 = Fehlerbericht gesendet -bugreport.dlg.connectedInternet = Wenn Sie mit dem Internet verbunden sind, können Sie einfach auf Fehlerbericht senden klicken. -bugreport.dlg.otherwise = Sonst senden Sie den den folgenden Text an diese Adresse: -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! -bugreport.dlg.failedmsg1 = OpenRocket konnte den Fehlerbericht nicht versenden: -bugreport.dlg.failedmsg2 = Bitte senden Sie den Bericht manuell an -bugreport.dlg.failedmsg3 = Fehler beim Versenden des Berichts -bugreport.reportDialog.txt = Sie können eine Fehler in OpenRocket mitteilen, indem Sie das unten stehende Formular ausfüllen und abschicken.
Sie können Fehler mit angehängten Dateien auch auf der Projekt-Website mitteilen. -bugreport.reportDialog.txt2 = Bitte beschreiben Sie kurz, was Sie getan haben, als der Fehler auftrat. -bugreport.dlg.provideDescription = Please provide a description of the bug first. -bugreport.dlg.provideDescription.title = Bug description missing - - -! Debug log dialog -debuglogdlg.but.clear = Löschen -debuglogdlg.OpenRocketdebuglog = OpenRocket Fehler-Log -debuglogdlg.Displayloglines = Zeige Log-Zeilen: -debuglogdlg.Follow = Folgen -debuglogdlg.col.Time = Zeit -debuglogdlg.col.Level = Level -debuglogdlg.col.Location = Ort -debuglogdlg.col.Message = Nachricht -debuglogdlg.lbl.Loglinenbr = Log-Zeilennummer -debuglogdlg.lbl.Time = Zeit: -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 = Motor entfernen -edtmotorconfdlg.but.Selectmotor = Motor auswählen -edtmotorconfdlg.but.Removeconfiguration = Konfiguration entfernen -edtmotorconfdlg.but.Newconfiguration = Neue Konfiguration -edtmotorconfdlg.lbl.Motormounts = Motorhalterungen: -edtmotorconfdlg.title.Editmotorconf = Motorkonfiguration bearbeiten -edtmotorconfdlg.selectcomp = Auswählen, welche Komponenten Motorhalterungen sind: -edtmotorconfdlg.lbl.Motorconfig = Motorkonfigurationen: -edtmotorconfdlg.lbl.Configname = Name der Konfiguration: -edtmotorconfdlg.lbl.Leavenamedefault = Leer lassen für Standardwert. - -! Example design dialog -exdesigndlg.but.open = Öffnen -exdesigndlg.lbl.Selectexample = Beispieldesigns zum Öffnen auswählen: -exdesigndlg.lbl.Openexampledesign = Beispieldesign öffnen -exdesigndlg.lbl.Exampledesignsnotfound = Beispieldesigns konnten nicht gefunden werden. -exdesigndlg.lbl.Examplesnotfound = Beispieldesign konnten nicht gefunden werden - - -! Material edit panel -matedtpan.but.new = Neu -matedtpan.but.edit = Bearbeiten -matedtpan.but.delete = Löschen -matedtpan.but.revertall = Alle löschen -matedtpan.col.Material = Material -matedtpan.col.Type = Typ -matedtpan.col.Density = Dichte -matedtpan.col.but.ttip.New = Neues Material hinzufügen -matedtpan.title.Addcustmaterial = Benutzerdefiniertes Material hinzufügen -matedtpan.but.ttip.edit = Bestehendes Material bearbeiten -matedtpan.title.Editmaterial = Material bearbeiten -matedtpan.title2.Editmaterial = Die mitgelieferten Materialien können nicht verändert werden. -matedtpan.but.ttip.delete = Benutzerdefiniertes Material löschen -matedtpan.but.ttip.revertall = Alle benutzerdefinierten Materialien löschen -matedtpan.title.Deletealluser-defined = Alle benutzerdefinierten Materialien löschen? -matedtpan.title.Revertall = Alle löschen? -matedtpan.lbl.edtmaterials = Das Bearbeiten der Materialien beeinflusst keine bereits existierenden Raketendesigns. - -!MaterialModel -MaterialModel.title.Material = Material -MaterialModel.title.Defcustmat = Benutzerdefiniertes Material definieren - - -! Preference dialog -pref.dlg.but.add = Hinzufügen -pref.dlg.but.reset = Zurücksetzen -pref.dlg.but.checknow = Jetzt überprüfen -pref.dlg.but.defaultmetric = Metrisches System -pref.dlg.but.defaultimperial = Imperialistisches System -pref.dlg.title.Preferences = Einstellungen -pref.dlg.tab.Units = Einheiten -pref.dlg.tab.Defaultunits = Standardeinheiten -pref.dlg.tab.Materials = Materialien -pref.dlg.tab.Custommaterials = Benutzerdefinierte Materialien -pref.dlg.tab.Options = Optionen -pref.dlg.tab.Miscellaneousoptions = Weiter Optionen -pref.dlg.lbl.Positiontoinsert = Position, um neue Komponenten einzufügen: -pref.dlg.lbl.Confirmdeletion = Löschen von Simulationen bestätigen -pref.dlg.lbl.User-definedthrust = Benutzerdefinierte Schubkurven: -pref.dlg.Allthrustcurvefiles = Alle Schubkurvendateien (*.eng; *.rrse; *.zzip; Verzeichnisse) -pref.dlg.RASPfiles = RASP Schubkurven (*.eng) -pref.dlg.RockSimfiles = RockSim Schubkurven(*.rse) -pref.dlg.ZIParchives = ZIP-Archiv (*.zip) -pref.dlg.checkbox.Checkupdates = Beim Starten auf neue Version prüfen -pref.dlg.ttip.Checkupdatesnow = Jetzt auf neue Version prüfen -pref.dlg.lbl.Selectprefunits = Wählen Sie Ihre bevorzugten Einheiten aus: -pref.dlg.lbl.Rocketdimensions = Raketendimensionen: -pref.dlg.lbl.Linedensity = Liniendichte: -pref.dlg.lbl.Motordimensions = Motordimensionen: -pref.dlg.lbl.Surfacedensity = Oberflächendichte: -pref.dlg.lbl.Distance = Entfernung: -pref.dlg.lbl.Bulkdensity = Bulk density:: -pref.dlg.lbl.Velocity = Geschwindigkeit -pref.dlg.lbl.Surfaceroughness = Oberflächenrauhheit: -pref.dlg.lbl.Acceleration = Beschleunigung: -pref.dlg.lbl.Area = Fläche -pref.dlg.lbl.Mass = Masse: -pref.dlg.lbl.Angle = Winkel: -pref.dlg.lbl.Force = Kraft: -pref.dlg.lbl.Rollrate = Roll-Rate: -pref.dlg.lbl.Totalimpulse = Gesamtimpuls: -pref.dlg.lbl.Temperature = Temperatur: -pref.dlg.lbl.Momentofinertia = Trägheitsmoment: -pref.dlg.lbl.Pressure = Druck: -pref.dlg.lbl.Stability = Stabilität: -pref.dlg.lbl.FlightTime = Flight time: -pref.dlg.lbl.effect1 = Die Änderungen werden wirksam, wenn Sie das nächste Mal ein Fenster öffnen. -pref.dlg.lbl.Checkingupdates = Prüfe, ob Aktualisierungen verfügbar sind... -pref.dlg.lbl.msg1 = Ein Fehler trat bei der Kommunikation mit dem Server auf. -pref.dlg.lbl.msg2 = Es konnten keine Informationen über Programmaktualisierungen empfangen werden. -pref.dlg.lbl.msg3 = Sie benutzen die neueste Version von OpenRocket. -pref.dlg.lbl.msg4 = Keine Aktualisierungen verfügbar. -pref.dlg.PrefChoiseSelector1 = Immer fragen -pref.dlg.PrefChoiseSelector2 = in der Mitte einfügen -pref.dlg.PrefChoiseSelector3 = an das Ende anhängen -pref.dlg.PrefBooleanSelector1 = Löschen -pref.dlg.PrefBooleanSelector2 = Bestätigen -pref.dlg.Add = Hinzufügen -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. - -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 = Simulation starten -simedtdlg.but.resettodefault = Auf Standardeinstellungen zurücksetzen -simedtdlg.but.add = Hinzufügen -simedtdlg.but.remove = Entfernen -simedtdlg.title.Editsim = Simulation bearbeiten -simedtdlg.lbl.Simname = Name der Simulation: -simedtdlg.tab.Launchcond = Startbedingungen -simedtdlg.tab.Simopt = Simulationsoptionen -simedtdlg.tab.Plotdata = Daten plotten -simedtdlg.tab.Exportdata = Daten exportieren -simedtdlg.lbl.Motorcfg = Motorkonfiguration: -simedtdlg.lbl.ttip.Motorcfg = Motorkonfiguration auswählen -simedtdlg.combo.ttip.motorconf = Die Motorkonfiguration auswählen. -simedtdlg.lbl.Wind = Wind -simedtdlg.lbl.Averwindspeed = Durchschnittliche Windgeschwindigkeit: -simedtdlg.lbl.ttip.Averwindspeed = Die durchschnittliche Windgeschwindigkeit relativ zum Boden. -simedtdlg.lbl.Stddeviation = Standardabweichung -simedtdlg.lbl.ttip.Stddeviation = Die Standardabweichung der Windgeschwindigkeit.
Die Windgeschwindigkeit liegt im Durchschnitt zu 95% der Zeit in der doppelten Standardabweichung. -simedtdlg.lbl.Turbulenceintensity = Intensität der Turbulenz: -simedtdlg.lbl.ttip.Turbulenceintensity1 = Die Intensität der Turbulenz ist die Standardabweichung geteilt durch durch die durchschnittliche Windgeschwindigkeit.
-simedtdlg.lbl.ttip.Turbulenceintensity2 = Typischer Wertebereich von -simedtdlg.lbl.ttip.Turbulenceintensity3 = bis -simedtdlg.border.Atmoscond = Atmosphärische Bedingungen -simedtdlg.checkbox.InterStdAtmosphere = Internationale Standardatmosphäre benutzen -simedtdlg.checkbox.ttip.InterStdAtmosphere1 = Auswählen, um das Modell der Internationalen Standardatmosphäre zu verwenden.
In diesem Modell gilt eine Temperatur von -simedtdlg.checkbox.ttip.InterStdAtmosphere2 = und ein Luftdruck von -simedtdlg.checkbox.ttip.InterStdAtmosphere3 = auf Meeresniveau. -simedtdlg.lbl.Temperature = Temperatur: -simedtdlg.lbl.ttip.Temperature = Die Temperatur am Startplatz. -simedtdlg.lbl.Pressure = Luftdruck: -simedtdlg.lbl.ttip.Pressure = Der Luftdruck am Startplatz. -simedtdlg.lbl.Launchsite = Startplatz -simedtdlg.lbl.Latitude = Breitengrad: -simedtdlg.lbl.ttip.Latitude = Der Breitengrad des Startplatzes beeinflusst die wirksame Gravitationskraft.
Positive Werte liegen auf der Nordhalbkugel, negative Werte auf der Südhalbkugel. - -simedtdlg.lbl.Longitude = Longitude: -simedtdlg.lbl.ttip.Longitude = Required for weather prediction and elevation models. - -simedtdlg.lbl.Altitude = Höhe: -simedtdlg.lbl.ttip.Altitude = Die Höhe des Startplatzes über Meeresniveau.
Die Höhe des Startplatzes beeinflusst die Position der Rakete im atmosphärischen Modell. -simedtdlg.border.Launchrod = Startrampe -simedtdlg.lbl.Length = Länge: -simedtdlg.lbl.ttip.Length = Die Länge der Startrampe -simedtdlg.lbl.Angle = Winkel: -simedtdlg.lbl.ttip.Angle = Der Winkel der Startrampe aus der Vertikalen. -simedtdlg.lbl.Direction = Richtung: -simedtdlg.lbl.ttip.Direction1 = Richtung der Startrampe relativ zur Windrichtung
-simedtdlg.lbl.ttip.Direction2 = = gegen den Wind. -simedtdlg.lbl.ttip.Direction3 = = mit dem Wind -simedtdlg.border.Simopt = Simulationsoptionen -simedtdlg.lbl.Calcmethod = Berechnungsmethode -simedtdlg.lbl.ttip.Calcmethod = Die erweiterte Methode nach Barrowman berechnet die aerodynamischen Kräfte
nach den Gleichungen von Barrowman, die um weitere Faktoren erweitert wurden. -simedtdlg.lbl.ExtBarrowman = Barrowman (erweitert) -simedtdlg.lbl.Simmethod = Simulationsmethode: -simedtdlg.lbl.ttip.Simmethod1 = Der Sechs-Freiheitsgradsimulator erlaubt der Rakete völlige Bewegungsfreiheit während des Fluges.
-simedtdlg.lbl.ttip.Simmethod2 = Das Integrieren wird nach dem numerischen Runge-Kutta-Verfahren 4. Ordnung durchgeführt. -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 = Zeitschritt: -simedtdlg.lbl.ttip.Timestep1 = Die Zeit zwischen den Simulationsschritten.
Kleinere Schritte ergeben genauere Ergebnisse, die Simulationen dauern aber länger.
-simedtdlg.lbl.ttip.Timestep2 = Die Berechnung der Simulation mit dem Verfahren 4. Ordnung liefert gute Ergebnisse mit Zeitschritten von -simedtdlg.but.ttip.resettodefault = Zeitschritte zurücksetzen auf den Standardwert ( -simedtdlg.border.Simlist = Simulationsempfänger -simedtdlg.txt.longA1 = Simulationsempfänger sind ein fortgeschrittenes Feature, dass es benutzerdefinierten Programmen erlaubt, die Simulationsdaten zu empfangen und mit der Simulation zu interagieren. -simedtdlg.txt.longA2 = Mehr Information zum Schreiben von Simualtionsempfängern sind in der OpenRocket technical documentation zu finden. -simedtdlg.lbl.Curlist = Aktuelle Simulationsempfänger: -simedtdlg.lbl.Addsimlist = Simulationsempfänger hinzufügen -simedtdlg.lbl.Noflightdata = Keine Flugdaten verfügbar. -simedtdlg.lbl.runsimfirst = Bitte erst die Simulation ausführen. -simedtdlg.chart.Simflight = Simulierter Flug -simedtdlg.dlg.Simres = Ergebnisse der Simulation -simedtdlg.IntensityDesc.None = Keine -simedtdlg.IntensityDesc.Verylow = Sehr niedrig -simedtdlg.IntensityDesc.Low = Niedrig -simedtdlg.IntensityDesc.Medium = Mittel -simedtdlg.IntensityDesc.High = Hoch -simedtdlg.IntensityDesc.Veryhigh = Sehr hoch -simedtdlg.IntensityDesc.Extreme = Extrem - -GeodeticComputationStrategy.none.name = None -GeodeticComputationStrategy.none.desc = Perform no geodetic computations. -GeodeticComputationStrategy.spherical.name = Spherical approximation -GeodeticComputationStrategy.spherical.desc = Perform geodetic computations assuming a spherical Earth.
This is sufficiently accurate for almost all purposes. -GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid -GeodeticComputationStrategy.wgs84.desc = Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.
Slower and unnecessary in most cases. - - - - -! Simulation Panel -simpanel.but.newsimulation = Neue Simulation -simpanel.but.editsimulation = Simulation bearbeiten -simpanel.but.runsimulations = Simulation ausführen -simpanel.but.deletesimulations = Simulation löschen -simpanel.but.plotexport = Plotten / exportieren -simpanel.but.ttip.newsimulation = Neue Simulation hinzufügen -simpanel.but.ttip.editsim = Ausgewählte Simulation bearbeiten -simpanel.but.ttip.runsimu = Neuberechnen der ausgewählten Simulationen -simpanel.but.ttip.deletesim = Ausgewählte Simulationen löschen -simpanel.checkbox.donotask = Nicht wieder fragen -simpanel.lbl.defpref = Die Standardaktion kann in den Einstellungen geändert werden. -simpanel.dlg.lbl.DeleteSim1 = Die ausgewählten Simulationen löschen? -simpanel.dlg.lbl.DeleteSim2 = Diese Aktion kann nicht rückgängig gemacht werden. -simpanel.dlg.lbl.DeleteSim3 = Simulationen löschen -simpanel.col.Name = Name der Simulation: -simpanel.col.Motors = Motoren -simpanel.col.Apogee = Apogäum -simpanel.col.Maxvelocity = max. Geschwindigkeit -simpanel.col.Maxacceleration = max. Beschleunigung -simpanel.col.Timetoapogee = Zeit bis zum Apogäum -simpanel.col.Flighttime = Flugzeit -simpanel.col.Groundhitvelocity = Landegeschwindigkeit - -! SimulationRunDialog -SimuRunDlg.title.RunSim = Simuliere... -SimuRunDlg.lbl.Running = Arbeite... -SimuRunDlg.lbl.Simutime = Simulationsdauer: -SimuRunDlg.lbl.Altitude = Höhe: -SimuRunDlg.lbl.Velocity = Geschwindigkeit: -SimuRunDlg.msg.Unabletosim = Simulieren nicht möglich: -SimuRunDlg.msg.errorOccurred = Während der Simulation trat ein Fehler auf: -SimuRunDlg.msg.AnException1 = Während der Simulation trat eine Ausnahme auf: -SimuRunDlg.msg.AnException2 = Bitte berichten Sie diesen Fehler mit den unten stehenden Details. -SimuRunDlg.msg.AssertionError1 = Während der Simulation trat ein Berechnungsfehler auf: -SimuRunDlg.msg.AssertionError2 = Bitte berichten Sie diesen Fehler mit den unten stehenden Details. -SimuRunDlg.msg.unknownerror1 = Während der Simulation trat ein unbekannter Fehler auf: -SimuRunDlg.msg.unknownerror2 = Das Programm könnte instabil sein, speichern Sie Ihr Design und starten Sie OpenRocket neu! - - - -! SimulationExportPanel -SimExpPan.desc = Komma getrennte Werte (*.csv) -SimExpPan.border.Vartoexport = zu exportierende Variablen -SimExpPan.but.Selectall = Alle auswählen -SimExpPan.but.Selectnone = Keine auswählen -SimExpPan.border.Fieldsep = Feldtrennung -SimExpPan.lbl.Fieldsepstr = Trennzeichen -SimExpPan.lbl.longA1 = Das Trennzeichen wird benutzt, um die Felder in der exportierten Datei voneinander zu trennen.
-SimExpPan.lbl.longA2 = Für eine CSV-Datei (Comma Separated Values) ein ',' benutzen. -SimExpPan.checkbox.Includesimudesc = Simulationsbeschreibung einfügen -SimExpPan.checkbox.ttip.Includesimudesc = Fügt einen Kommentar mit einer Simulationsbeschreibung am Anfang der Datei ein. -SimExpPan.border.Comments = Kommentare -SimExpPan.checkbox.Includefielddesc = Feldbeschreibungen einfügen -SimExpPan.checkbox.ttip.Includefielddesc = Fügt eine Kommentarzeile mit der Beschreibung der exportierten Variablen ein. -SimExpPan.checkbox.Incflightevents = Flugereignisse einfügen -SimExpPan.checkbox.ttip.Incflightevents = Fügt eine Kommentarzeile für jedes Flugereignis ein. -SimExpPan.lbl.Commentchar = Kommentarzeichen: -SimExpPan.lbl.ttip.Commentchar = Zeichen, das einen Kommentar in der exportierten Datei kennzeichnet. -SimExpPan.but.Exporttofile = In Datei exportieren... -SimExpPan.Fileexists.desc1 = File \"",Datei \«" -SimExpPan.Fileexists.desc2 = \" existiert bereits. Überschreiben?" -SimExpPan.Fileexists.title = Datei existiert bereits -SimExpPan.ExportingVar.desc1 = Exportiere Variable 1 aus -SimExpPan.ExportingVar.desc2 = Exportiere -SimExpPan.ExportingVar.desc3 = Variablen aus -SimExpPan.Col.Variable = Variable -SimExpPan.Col.Unit = Einheit - - -CsvOptionPanel.separator.space = SPACE -CsvOptionPanel.separator.tab = TAB - - - -! MotorPlot -MotorPlot.title.Motorplot = Motorkurve -MotorPlot.but.Select = Auswahl -MotorPlot.Chart.Motorthrustcurve = Motorschubkurve -MotorPlot.Chart.Time = Zeit / s -MotorPlot.Chart.Thrust = Schub / N -MotorPlot.txt.Designation = Bezeichnung: -MotorPlot.txt.Manufacturer = Hersteller -MotorPlot.txt.Type = Typ: -MotorPlot.txt.Delays = Verzögerungen: -MotorPlot.txt.Comment = Kommentare:\n - - - -! Simulation plot panel -simplotpanel.lbl.Presetplotconf = Plotparameter setzen -simplotpanel.lbl.Xaxistype = X-Achse: -simplotpanel.lbl.Unit = Einheit: -simplotpanel.lbl.Yaxistypes = Y-Achse: -simplotpanel.lbl.Flightevents = Flugereignisse: -simplotpanel.but.All = Alle auswählen -simplotpanel.but.None = Keine -simplotpanel.but.NewYaxisplottype = Neuer Y-Achsenplot-Typ -simplotpanel.but.Plotflight = Flug plotten -simplotpanel.lbl.Axis = Achsen: -simplotpanel.but.ttip.Removethisplot = Diesen Plot löschen -simplotpanel.Desc = Die Daten werden in zeitlicher Reihenfolge geplottet, auch wenn der X-Achsen-Typ nicht Zeit ist. -simplotpanel.OptionPane.lbl1 = Es sind maximal 15 Plots erlaubt. -simplotpanel.OptionPane.lbl2 = Plot konnte nicht hinzugefügt werden -simplotpanel.AUTO_NAME = Auto -simplotpanel.LEFT_NAME = Links -simplotpanel.RIGHT_NAME = Rechts -simplotpanel.CUSTOM = Benutzerdefiniert - -! Component add buttons -compaddbuttons.Bodycompandfinsets = Körperteile und Leitwerke -compaddbuttons.Nosecone = Spitze -compaddbuttons.Bodytube = Körperrohr -compaddbuttons.Transition = Übergang -compaddbuttons.Trapezoidal = Trapeziod -compaddbuttons.Elliptical = Elliptisch -compaddbuttons.Freeform = Freiform -compaddbuttons.Launchlug = Leit-\nröhrchen -compaddbuttons.Innercomponent = Innenteile -compaddbuttons.Innertube = Innenrohr -compaddbuttons.Coupler = Koppler -compaddbuttons.Centeringring = Zentrier-\nring -compaddbuttons.Bulkhead = Schott -compaddbuttons.Engineblock = Motor-\nblock -compaddbuttons.Massobjects = Massenobjekte -compaddbuttons.Parachute = Fallschirm -compaddbuttons.Streamer = Strömer -compaddbuttons.Shockcord = Gummiband -compaddbuttons.Masscomponent = Massen-\nobjekt -compaddbuttons.Donotaskmeagain = Nicht wieder fragen -compaddbuttons.Selectcomppos = Komponentenposition auswählen -compaddbuttons.lbl.Youcanchange = Die Standardaktion kann in den Einstellungen geändert werden. -compaddbuttons.lbl.insertcomp = Die Komponente nach der aktuellen Komponente oder als letzte Komponente einfügen? -compaddbuttons.askPosition.Inserthere = Hier einfügen -compaddbuttons.askPosition.Addtotheend = Zum Ende hinzufügen -compaddbuttons.askPosition.Cancel = Abbrechen - -! Component Analysis Dialog -componentanalysisdlg.componentanalysis = Component analysis -componentanalysisdlg.lbl.winddir = Windrichtung -componentanalysisdlg.TitledBorder.warnings = Warnungen: -componentanalysisdlg.ToggleBut.worst = Worst -componentanalysisdlg.lbl.angleofattack = Angriffswinkel: -componentanalysisdlg.lbl.machnumber = Machzahl: -componentanalysisdlg.lbl.rollrate = Rollrate: -componentanalysisdlg.lbl.activestages = Aktive Stufen: -componentanalysisdlg.lbl.motorconf = Motorkonfiguration: -componentanalysisdlg.TabStability.Col = Komponente -componentanalysisdlg.TabStability = Stabilität -componentanalysisdlg.TabStability.ttip = Stabilitätsinformationen -componentanalysisdlg.dragTableModel.Col.Component = Komponente -componentanalysisdlg.dragTableModel.Col.Pressure = Druck CD -componentanalysisdlg.dragTableModel.Col.Base = Base CD -componentanalysisdlg.dragTableModel.Col.friction = Reibung CD -componentanalysisdlg.dragTableModel.Col.total = Gesamt CD -componentanalysisdlg.dragTabchar = Luftwiderstand -componentanalysisdlg.dragTabchar.ttip = Luftwiderstands-Eigenschaften -componentanalysisdlg.rollTableModel.Col.component = Komponente -componentanalysisdlg.rollTableModel.Col.rollforc = Roll forcing coefficient -componentanalysisdlg.rollTableModel.Col.rolldamp = Roll damping coefficient -componentanalysisdlg.rollTableModel.Col.total = Gesamt Cl -componentanalysisdlg.rollTableModel = Rolldynamik -componentanalysisdlg.rollTableModel.ttip = Rolldynamik -componentanalysisdlg.println.closingmethod = Closing method called: -componentanalysisdlg.println.settingnam = SETTING NAN VALUES -componentanalysisdlg.lbl.reflenght = Referenzlänge: -componentanalysisdlg.lbl.refarea = Referenzfläche: -!componentanalysisdlg.But.close =Close -componentanalysisdlg.TabStability.Col.Component = Component - -! Custom Material dialog -custmatdlg.title.Custommaterial = Benutzerdefiniertes Material -custmatdlg.lbl.Materialname = Name des Materials: -custmatdlg.lbl.Materialtype = Materialtyp -custmatdlg.lbl.Materialdensity = Materialdichte: -custmatdlg.checkbox.Addmaterial = Material zur Datenbank hinzufügen - - -! Ring Component Config -ringcompcfg.OuterRadius = Äußerer Radius -ringcompcfg.Automatic = Automatisch -ringcompcfg.InnerRadius = Innerer Radius -ringcompcfg.Thickness = Wandstärke -ringcompcfg.Length = Länge -ringcompcfg.Positionrelativeto = Relative Position zu: -ringcompcfg.plus = plus -ringcompcfg.PositionValue = Positionswert -ringcompcfg.Radialdistance = Radialer Abstand: -ringcompcfg.Distancefrom = Abstand von der Raketenmittellinie -ringcompcfg.Radialdirection = Radiale Richtung -ringcompcfg.radialdirectionfrom = Die radiale Richtung von der Raketenmittellinie -ringcompcfg.but.Reset = Zurücksetzen -ringcompcfg.but.Resetcomponant = Komponente auf die Raketenmittellinie zurücksetzen -ringcompcfg.EngineBlock.desc = Eine Motorhalterung verhindert, dass der Motor sich im Rohr nach vorne bewegt.

Um einen Motor hinzuzufügen, ein Körperrohr oder ein Innenrohr hinzufügen und im Reiter Motor als Motorhalterung markieren. -ringcompcfg.note.desc = Hinweis: Innenrohre beeinflussen die Aerodynamik der Rakete nicht, auch wenn sie außerhalb des Körperohres liegen. - - -! Body Tube Config -BodyTubecfg.lbl.Bodytubelength = Länge des Körperrohres: -BodyTubecfg.lbl.Outerdiameter = Außendurchmesser: -BodyTubecfg.lbl.Innerdiameter = Innendurchmesser: -BodyTubecfg.lbl.Wallthickness = Wandstärke: -BodyTubecfg.tab.General = Allgemein -BodyTubecfg.tab.Generalproperties = Allgemeine Eigenschaften -BodyTubecfg.tab.Motor = Motor -BodyTubecfg.tab.Motormountconf = Motorkonfiguration -BodyTubecfg.checkbox.Automatic = Automatisch -BodyTubecfg.checkbox.Filled = Gefüllt - -! FinSetConfig -FinSetConfig.tab.Fintabs = Leitwerke -FinSetConfig.tab.Through-the-wall = Durchsteckbare Leitwerke -FinSetConfig.but.Converttofreeform = In Freiform konvertieren -FinSetConfig.but.Converttofreeform.ttip = Konvertiert diese Leitwerke in eine Freiform -FinSetConfig.Convertfinset = Leitwerke konvertieren -FinSetConfig.but.Splitfins = Geteilte Leitwerke -FinSetConfig.but.Splitfins.ttip = Teilt den Leitwerkssatz in getrennte Leitwerke -FinSetConfig.lbl.Through-the-wall = Durchsteckbare Leitwerke: -FinSetConfig.lbl.Tablength = Länge: -FinSetConfig.ttip.Tablength = Länge des Leitwerks. -FinSetConfig.lbl.Tabheight = Höhe: -FinSetConfig.ttip.Tabheight = Spannweite des Leitwerks. -FinSetConfig.lbl.Tabposition = Position: -FinSetConfig.ttip.Tabposition = Position des Leitwerks. -FinSetConfig.lbl.relativeto = relativ zu - -! MotorDatabaseLoadingDialog -MotorDbLoadDlg.title = Lade Motoren -MotorDbLoadDlg.Loadingmotors = Lade Motoren... - -! RocketConfig -RocketCfg.lbl.Designname = Name der Rakete: -RocketCfg.lbl.Designer = Ersteller: -RocketCfg.lbl.Comments = Kommentare: -RocketCfg.lbl.Revisionhistory = Versionsgeschichte: -RocketCfg.lbl.Material = Material: - -! ShockCordConfig -ShockCordCfg.lbl.Shockcordlength = Gummibandlänge - -! RocketComponentConfig -RocketCompCfg.lbl.Componentname = Komponentenname: -RocketCompCfg.ttip.Thecomponentname = Name der Komponente. -RocketCompCfg.tab.Override = Werte überschreiben -RocketCompCfg.tab.MassandCGoverride = Massen- und Schwerpunktsoptionen -RocketCompCfg.tab.Figure = Form -RocketCompCfg.tab.Figstyleopt = Formoptionen -RocketCompCfg.tab.Comment = Kommentar -RocketCompCfg.tab.Specifyacomment = Kommentar zu dieser Komponente -RocketCompCfg.lbl.Mass = Masse: -RocketCompCfg.lbl.Componentmass = Masse der Komponente: -RocketCompCfg.lbl.overriddento = (überschrieben auf -RocketCompCfg.lbl.overriddenby = (überschrieben durch -RocketCompCfg.lbl.Componentmaterial = Material: -RocketCompCfg.lbl.Componentfinish = Oberfläche: -RocketCompCfg.lbl.ttip.componentmaterialaffects = Das Material beeinflusst die Masse der Komponente. -RocketCompCfg.combo.ttip.componentmaterialaffects = Das Material beeinflusst die Masse der Komponente. -RocketCompCfg.lbl.longA1 = Die Oberfläche beeinflusst den aerodynamischen Widerstand der Komponente.
-RocketCompCfg.lbl.longA2 = Der angegebene Wert ist die durchschnittliche Rautiefe der Oberfläche. -RocketCompCfg.but.Setforall = Für alle setzen -RocketCompCfg.but.ttip.Setforall = Diese Oberflächen für alle Komponenten der Rakete setzen. -RocketCompCfg.lbl.Overridemassorcenter = Überschreiben von Masse oder Schwerpunkts von -RocketCompCfg.checkbox.Overridemass = Masse überschreiben: -RocketCompCfg.checkbox.Overridecenterofgrav = Schwerpunkt überschreiben: -RocketCompCfg.checkbox.OverridemassandCG = Masse und Schwerpunkt für alle Unterkomponenten überschreiben -RocketCompCfg.lbl.longB1 = Die überschriebene Masse enthält keine Motoren.
-RocketCompCfg.lbl.longB2 = Die Messung des Schwerpunktes beginnt am Ende von -RocketCompCfg.lbl.Commentsonthe = Kommentare zu -RocketCompCfg.lbl.Figurestyle = Form: -RocketCompCfg.lbl.Componentcolor = Farbe: -RocketCompCfg.lbl.Choosecolor = Farbe auswählen -RocketCompCfg.checkbox.Usedefaultcolor = Standardfarbe verwenden -RocketCompCfg.lbl.Complinestyle = Linienstil: -RocketCompCfg.but.Saveasdefstyle = Als Standardstil speichern -RocketCompCfg.lbl.Diameter = Durchmesser: -RocketCompCfg.lbl.Length = Länge: -RocketCompCfg.lbl.Thickness = Wandstärke: -RocketCompCfg.checkbox.Endcapped = Verschlossenes Ende -RocketCompCfg.ttip.Endcapped = Gibt an, ob das Ende der Schulter geschlossen ist. -RocketCompCfg.title.Noseconeshoulder = Spitzenschulter -RocketCompCfg.title.Aftshoulder = Schulter hinten -RocketCompCfg.border.Foreshoulder = Schulter vorn -!RocketCompCfg.lbl.Length = Length: - -! BulkheadConfig -BulkheadCfg.tab.Radius = Radius: -BulkheadCfg.tab.Thickness = Wandstärke: -BulkheadCfg.tab.General = Allgemein -BulkheadCfg.tab.Generalproperties = Allgemeine Eigenschaften - -!CenteringRingConfig -CenteringRingCfg.tab.Outerdiam = Außendurchmesser: -CenteringRingCfg.tab.Innerdiam = Innendurchmesser: -CenteringRingCfg.tab.Thickness = Wandstärke: -CenteringRingCfg.tab.General = Allgemein -CenteringRingCfg.tab.Generalproperties = Allgemeine Eigenschaften - -!ComponentConfigDialog -ComponentCfgDlg.configuration = Konfiguration -ComponentCfgDlg.configuration1 = -ComponentCfgDlg.Modify = Verändern - -!EllipticalFinSetConfig -EllipticalFinSetCfg.Nbroffins = Anzahl der Leitwerke -EllipticalFinSetCfg.Rotation = Rotation: -EllipticalFinSetCfg.Fincant = Neigung: -EllipticalFinSetCfg.Rootchord = Blatttiefe: -EllipticalFinSetCfg.Height = Höhe: -EllipticalFinSetCfg.Positionrelativeto = Position relativ zu: -EllipticalFinSetCfg.plus = plus -EllipticalFinSetCfg.FincrossSection = Querschnitt: -EllipticalFinSetCfg.Thickness = Wandstärke: -EllipticalFinSetCfg.General = Allgemein -EllipticalFinSetCfg.Generalproperties = Allgemeine Eigenschaften -EllipticalFinSetCfg.ttip.Fincant = Der Winkel, in dem die Leitwerke zum Körperrohr geneigt sind. - -!FreeformFinSetConfig -FreeformFinSetCfg.tab.General = Allgemein -FreeformFinSetCfg.tab.ttip.General = Allgemeine Eigenschaften -FreeformFinSetCfg.tab.Shape = Form -FreeformFinSetCfg.tab.ttip.Finshape = Leitwerksform -FreeformFinSetCfg.lbl.Numberoffins = Anzahl der Leitwerke -FreeformFinSetCfg.lbl.Finrotation = Rotation: -FreeformFinSetCfg.lbl.Fincant = Neigung: -FreeformFinSetCfg.lbl.ttip.Fincant = Der Winkel, in dem die Leitwerke zum Körperrohr geneigt sind. -FreeformFinSetCfg.lbl.Posrelativeto = Position relativ zu: -FreeformFinSetCfg.lbl.plus = plus -FreeformFinSetCfg.lbl.FincrossSection = Querschnitt: -FreeformFinSetCfg.lbl.Thickness = Wandstärke: -! 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 = Motorkonfiguration -InnerTubeCfg.tab.Cluster = Cluster -InnerTubeCfg.tab.ttip.Cluster = Cluster-Konfiguration -InnerTubeCfg.tab.Radialpos = Radiale Position -InnerTubeCfg.tab.ttip.Radialpos = Radiale Position -InnerTubeCfg.lbl.Selectclustercfg = Cluster-Konfiguration auswählen: -InnerTubeCfg.lbl.TubeSep = Rohrtrennung -InnerTubeCfg.lbl.ttip.TubeSep = Die Trennung der Rohre, 1.0 = die Rohre berühren sich -InnerTubeCfg.lbl.Rotation = Rotation: -InnerTubeCfg.lbl.ttip.Rotation = Rotationswinkel der Cluster-Konfiguration -InnerTubeCfg.lbl.Rotangle = Rotationswinkel der Cluster-Konfiguration -InnerTubeCfg.but.Splitcluster = Cluster aufteilen -InnerTubeCfg.lbl.longA1 = Den Cluster in einzelne Komponenten aufteilen.
-InnerTubeCfg.lbl.longA2 = Die dupliziert alle Komponenten innerhalb dieses Innenrohrs. -InnerTubeCfg.but.Resetsettings = Einstellungen zurücksetzen -InnerTubeCfg.but.ttip.Resetsettings = Setzt die Aufteilung und Rotation auf die Standardwerte zurück - -! LaunchLugConfig -LaunchLugCfg.lbl.Length = Länge: -LaunchLugCfg.lbl.Outerdiam = Außendurchmesser: -LaunchLugCfg.lbl.Innerdiam = Innendurchmesser: -LaunchLugCfg.lbl.Thickness = Wandstärke: -LaunchLugCfg.lbl.Radialpos = Radiale Position: -LaunchLugCfg.lbl.Posrelativeto = Position relativ zu: -LaunchLugCfg.lbl.plus = plus -LaunchLugCfg.tab.General = Allgemein -LaunchLugCfg.tab.Generalprop = Allgemeine Eigenschaften - -! MassComponentConfig -MassComponentCfg.lbl.Mass = Masse -MassComponentCfg.lbl.Length = Länge -MassComponentCfg.lbl.Diameter = Durchmesser -MassComponentCfg.lbl.PosRelativeto = Position relativ zu: -MassComponentCfg.lbl.plus = plus -MassComponentCfg.tab.General = Allgemein -MassComponentCfg.tab.ttip.General = Allgemeine Eigenschaften -MassComponentCfg.tab.Radialpos = Radiale Position -MassComponentCfg.tab.ttip.Radialpos = Konfiguration der radialen Position -MassComponentCfg.lbl.Radialdistance = Radialer Abstand: -MassComponentCfg.lbl.Radialdirection = radiale Richtung: -MassComponentCfg.but.Reset = Zurücksetzen - -! MotorConfig -MotorCfg.checkbox.compmotormount = Diese Komponente ist eine Motorhalterung -MotorCfg.lbl.Motorcfg = Motorkonfiguration -MotorCfg.but.New = Neu -MotorCfg.lbl.Currentmotor = Aktueller Motor: -MotorCfg.lbl.Motoroverhang = Motorüberstand: -MotorCfg.lbl.Ignitionat = Zündung bei: -MotorCfg.lbl.plus = plus -MotorCfg.lbl.seconds = Sekunden -MotorCfg.lbl.longA1 = Das aktuelle Design hat im Moment nur eine Stufe. -MotorCfg.lbl.longA2 = Stufen können durch Klicken auf \«Neue Stufe\« hinzugefügt werden. -MotorCfg.lbl.longB1 = Das aktuelle Design hat im Moment nur eine Stufe. -MotorCfg.lbl.longB2 = Stufen. -MotorCfg.but.Selectmotor = Motor auswählen -MotorCfg.but.Removemotor = Motor entfernen -MotorCfg.lbl.motorLabel = Keiner - -! NoseConeConfig -NoseConeCfg.lbl.Noseconeshape = Spitzenform: -NoseConeCfg.lbl.Shapeparam = Formparameter: -NoseConeCfg.lbl.Noseconelength = Spitzenlänge: -NoseConeCfg.lbl.Basediam = Basisdurchmesser: -NoseConeCfg.checkbox.Automatic = Automatisch -NoseConeCfg.lbl.Wallthickness = Wandstärke: -NoseConeCfg.checkbox.Filled = gefüllt -NoseConeCfg.tab.General = Allgemein -NoseConeCfg.tab.ttip.General = Allgemeine Eigenschaften -NoseConeCfg.tab.Shoulder = Schulter -NoseConeCfg.tab.ttip.Shoulder = Schultereigenschaften - -! ParachuteConfig -ParachuteCfg.lbl.Canopy = Fallschirmkappe: -ParachuteCfg.lbl.Diameter = Durchmesser: -ParachuteCfg.lbl.Material = Material: -ParachuteCfg.combo.MaterialModel = Das Material beeinflusst die Masse der Komponente. -ParachuteCfg.lbl.longA1 = Luftwiderstandskoeffizient CD: -ParachuteCfg.lbl.longB1 = Der Luftwiderstandsbeiwert relativ zur Gesamtfläche des Fallschirms.
-ParachuteCfg.lbl.longB2 = Ein größerer Luftwiderstand führt zu einer kleineren Sinkrate. -ParachuteCfg.lbl.longB3 = Ein typischer Wert für Fallschirme ist 0,8. -ParachuteCfg.but.Reset = Zurücksetzen -ParachuteCfg.lbl.Shroudlines = Fangleinen: -ParachuteCfg.lbl.Numberoflines = Anzahl der Leinen: -ParachuteCfg.lbl.Linelength = Länge der Leinen: -ParachuteCfg.lbl.Material = Material: -ParachuteCfg.lbl.Posrelativeto = Position relativ zu: -ParachuteCfg.lbl.plus = plus -ParachuteCfg.lbl.Packedlength = gepackte Länge: -ParachuteCfg.lbl.Packeddiam = gepackter Durchmesser: -ParachuteCfg.lbl.Deploysat = Auswurf bei -ParachuteCfg.lbl.seconds = Sekunden -ParachuteCfg.lbl.Altitude = Höhe: -ParachuteCfg.tab.General = Allgemein -ParachuteCfg.tab.ttip.General = Allgemeine Eigenschaften -ParachuteCfg.tab.Radialpos = Radiale Position -ParachuteCfg.tab.ttip.Radialpos = Konfiguration der radialen Position -ParachuteCfg.lbl.Radialdistance = Radialer Abstand: -ParachuteCfg.lbl.Radialdirection = radiale Richtung: -ParachuteCfg.but.Reset = Zurücksetzen -ParachuteCfg.lbl.plusdelay = plus - -! ShockCordConfig -ShockCordCfg.lbl.Shockcordlength = Länge des Gummibands -ShockCordCfg.lbl.Shockcordmaterial = Material des Gummibands: -ShockCordCfg.lbl.Posrelativeto = Position relativ zu: -ShockCordCfg.lbl.plus = plus -ShockCordCfg.lbl.Packedlength = gepackte Länge: -ShockCordCfg.lbl.Packeddiam = gepackter Durchmesser: -ShockCordCfg.tab.General = Allgemein -ShockCordCfg.tab.ttip.General = Allgemeine Eigenschaften - -!SleeveConfig -SleeveCfg.tab.Outerdiam = Außendurchmesser: -SleeveCfg.tab.Innerdiam = Innendurchmesser: -SleeveCfg.tab.Wallthickness = Wandstärke: -SleeveCfg.tab.Length = Länge: -SleeveCfg.tab.General = Allgemein -SleeveCfg.tab.Generalproperties = Allgemeine Eigenschaften - -! StreamerConfig -StreamerCfg.lbl.Striplength = Länge des Strömers: -StreamerCfg.lbl.Stripwidth = Breite des Strömers: -StreamerCfg.lbl.Striparea = Fläche des Strömers: -StreamerCfg.lbl.Aspectratio = Seitenverhältnis: -StreamerCfg.lbl.Material = Material: -StreamerCfg.combo.ttip.MaterialModel = Das Material beeinflusst die Masse der Komponente. -StreamerCfg.lbl.longA1 = Widerstandskoeffizient CD: -StreamerCfg.lbl.longB1 = Der Widerstandskoeffizient des Strömers hängt von der Gesamtfläche ab.
-StreamerCfg.lbl.longB2 = Ein größerer Luftwiderstandskoeffizient führt zu einer kleineren Sinkrate. -StreamerCfg.lbl.Automatic = Automatisch -StreamerCfg.lbl.longC1 = Der Luftwiderstandskoeffizient hängt von der Fläche des Strömers ab. -StreamerCfg.lbl.Posrelativeto = Position relativ zu: -StreamerCfg.lbl.plus = plus -StreamerCfg.lbl.Packedlength = gepackte Länge: -StreamerCfg.lbl.Packeddiam = gepackter Durchmesser: -StreamerCfg.lbl.Deploysat = Auswurf bei -StreamerCfg.lbl.seconds = Sekunden -StreamerCfg.lbl.Altitude = Höhe: -StreamerCfg.tab.General = Allgemein -StreamerCfg.tab.ttip.General = Allgemeine Eigenschaften -StreamerCfg.tab.Radialpos = Radiale Position -StreamerCfg.tab.ttip.Radialpos = Konfiguration der radialen Position -StreamerCfg.lbl.Radialdistance = Radialer Abstand: -StreamerCfg.lbl.Radialdirection = radiale Richtung: -StreamerCfg.but.Reset = Zurücksetzen -StreamerCfg.lbl.plusdelay = plus - -! ThicknessRingComponentConfig -ThicknessRingCompCfg.tab.Outerdiam = Außendurchmesser: -ThicknessRingCompCfg.tab.Innerdiam = Innendurchmesser: -ThicknessRingCompCfg.tab.Wallthickness = Wandstärke: -ThicknessRingCompCfg.tab.Length = Länge: -ThicknessRingCompCfg.tab.General = Allgemein -ThicknessRingCompCfg.tab.Generalprop = Allgemeine Eigenschaften - -! TransitionConfig -TransitionCfg.lbl.Transitionshape = Form des Übergangs -TransitionCfg.checkbox.Clipped = geklemmt -TransitionCfg.lbl.Shapeparam = Formparameter: -TransitionCfg.lbl.Transitionlength = Länge des Übergangs: -TransitionCfg.lbl.Forediam = Vorderer Durchmesser -TransitionCfg.checkbox.Automatic = Automatisch -TransitionCfg.lbl.Aftdiam = Hinterer Durchmesser -TransitionCfg.lbl.Wallthickness = Wandstärke: -TransitionCfg.checkbox.Filled = gefüllt -TransitionCfg.tab.General = Allgemein -TransitionCfg.tab.Generalproperties = Allgemeine Eigenschaften -TransitionCfg.tab.Shoulder = Schulter -TransitionCfg.tab.Shoulderproperties = Schultereigenschaften - -! TrapezoidFinSetConfig -TrapezoidFinSetCfg.lbl.Nbroffins = Anzahl der Leitwerke -TrapezoidFinSetCfg.lbl.ttip.Nbroffins = Anzahl der Leitwerke in diesem Satz -TrapezoidFinSetCfg.lbl.Finrotation = Rotation der Leitwerke -TrapezoidFinSetCfg.lbl.ttip.Finrotation = Winkel des ersten Leitwerks in diesem Satz -TrapezoidFinSetCfg.lbl.Fincant = Neigung: -TrapezoidFinSetCfg.lbl.ttip.Fincant = Der Winkel, in dem die Leitwerke zum Körperrohr geneigt sind. -TrapezoidFinSetCfg.lbl.Rootchord = Blatttiefe: -TrapezoidFinSetCfg.lbl.Tipchord = Blatttiefe (Spitze) -TrapezoidFinSetCfg.lbl.Height = Höhe: -TrapezoidFinSetCfg.lbl.Sweeplength = Blattbreite: -TrapezoidFinSetCfg.lbl.Sweepangle = Pfeilungswinkel -TrapezoidFinSetCfg.lbl.FincrossSection = Leitwerksquerschnitt -TrapezoidFinSetCfg.lbl.Thickness = Wandstärke: -TrapezoidFinSetCfg.lbl.Posrelativeto = Position relativ zu: -TrapezoidFinSetCfg.lbl.plus = plus -TrapezoidFinSetCfg.tab.General = Allgemein -TrapezoidFinSetCfg.tab.Generalproperties = Allgemeine Eigenschaften - -!MotorConfigurationModel -MotorCfgModel.Editcfg = Konfiguration bearbeiten - -! StorageOptionChooser -StorageOptChooser.lbl.Simdatatostore = Zu speichernde Simulationsdaten: -StorageOptChooser.rdbut.Allsimdata = Alle Simulationsdaten -StorageOptChooser.lbl.longA1 = Speichert alle Simulationsdaten.
-StorageOptChooser.lbl.longA2 = Dies kann sehr große Dateien erzeugen! -StorageOptChooser.rdbut.Every = Alle Simulationsdaten -StorageOptChooser.lbl.longB1 = Speicher plotbare Daten in etwa diesem Abstand.
-StorageOptChooser.lbl.longB2 = Größere Werte erzeugen kleinere Dateien. -StorageOptChooser.lbl.seconds = Sekunden -StorageOptChooser.rdbut.Onlyprimfig = Nur die wichtigsten Werte -StorageOptChooser.lbl.longC1 = Speichert nur die Werte, die in der Zusammenfassung stehen.
-StorageOptChooser.lbl.longC2 = Dies ergibt die kleinsten Dateien -StorageOptChooser.checkbox.Compfile = Datei komprimieren -StorageOptChooser.lbl.UsingComp = Kompression der Datei verringert die Größe signifikant. -StorageOptChooser.lbl.longD1 = Eine Schätzung der Dateigröße mit den gegebenen Optionen. -StorageOptChooser.ttip.Saveopt = Speicheroptionen -StorageOptChooser.lbl.Estfilesize = Voraussichtliche Dateigröße: -StorageOptChooser.lbl.Saveopt = Speicheroptionen - -! ThrustCurveMotorSelectionPanel -TCMotorSelPan.lbl.Selrocketmotor = Raketenmotor auswählen: -TCMotorSelPan.checkbox.hideSimilar = Ähnliche Schubkurven verbergen -TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Alle Motoren anzeigen -TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Motoren anzeigen, deren Durchmesser kleiner als der der Motorhalterung ist -TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Motoren anzeigen, deren Durchmesser gleich der der Motorhalterung ist -TCMotorSelPan.lbl.Motormountdia = Durchmesser der Motorhalterung -TCMotorSelPan.lbl.Search = Suchen: -TCMotorSelPan.lbl.Selectthrustcurve = Schubkurve auswählen: -TCMotorSelPan.lbl.Ejectionchargedelay = Verzögerung der Ausstoßladung: -TCMotorSelPan.equalsIgnoreCase.None = keine -TCMotorSelPan.lbl.NumberofsecondsorNone = (Anzahl der Sekunden oder \«keine\«) -TCMotorSelPan.lbl.Totalimpulse = Gesamtimpuls: -TCMotorSelPan.lbl.Avgthrust = Durchschn. Schub: -TCMotorSelPan.lbl.Maxthrust = max. Schub -TCMotorSelPan.lbl.Burntime = Brenndauer: -TCMotorSelPan.lbl.Launchmass = Startmasse: -TCMotorSelPan.lbl.Emptymass = Leermasse: -TCMotorSelPan.lbl.Datapoints = Datenpunkte: -TCMotorSelPan.lbl.Digest = Übersicht: -TCMotorSelPan.title.Thrustcurve = Schubkurve: -TCMotorSelPan.title.Thrust = Schub: -TCMotorSelPan.delayBox.None = keine - - -! PlotDialog -PlotDialog.title.Flightdataplot = Flugdatenplot -PlotDialog.Chart.Simulatedflight = Simulierter Flug -PlotDialog.CheckBox.Showdatapoints = Datenpunkte anzeigen -PlotDialog.lbl.Chart = Klicken+ziehen: runter+rechts um hinein zu zoomen, hoch+links um heraus zu zoomen - - -! "main" prefix is used for the main application dialog - -# FIXME: Rename the description keys - -main.menu.file = Datei -main.menu.file.desc = File-handling related tasks -main.menu.file.new = Neu -main.menu.file.new.desc = Create a new rocket design -main.menu.file.open = Öffnen.. -BasicFrame.item.Openrocketdesign = Raketendesign öffnen -main.menu.file.openExample = Beispiel öffnen.. -BasicFrame.item.Openexamplerocketdesign = Beispieldesign öffnen -main.menu.file.save = Speichern -BasicFrame.item.SavecurRocketdesign = Aktuelles Raketendesign speichern -main.menu.file.saveAs = Speichern unter... -BasicFrame.item.SavecurRocketdesnewfile = Aktuelles Raketendesign in eine neue Datei speichern -main.menu.file.print = Drucken / als PDF exportieren... -BasicFrame.item.Printpart = Komponentenliste und Leitwerkschablone drucken -main.menu.file.close = Schließen -BasicFrame.item.Closedesign = Aktuelles Raketendesign schließen -main.menu.file.quit = Beenden -BasicFrame.item.Quitprogram = Programm beenden - -main.menu.edit = Bearbeiten -BasicFrame.menu.Rocketedt = Rakete bearbeiten -main.menu.edit.undo = Rückgängig -main.menu.edit.undo.desc = Undo the previous operation -main.menu.edit.redo = Wiederholen -main.menu.edit.redo.desc = Redo the previously undone operation -main.menu.edit.cut = Ausschneiden -main.menu.edit.copy = Kopieren -main.menu.edit.paste = Einfügen -main.menu.edit.delete = Löschen -main.menu.edit.resize = Scale... -main.menu.edit.resize.desc = Scale parts of the rocket design -main.menu.edit.preferences = Einstellungen -main.menu.edit.preferences.desc = Setup the application preferences - -main.menu.analyze = Analysieren -main.menu.analyze.desc = Rocket analysis -main.menu.analyze.componentAnalysis = Komponente analysieren -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 = Hilfe -main.menu.help.desc = Information about OpenRocket -main.menu.help.license = Lizenz -main.menu.help.license.desc = OpenRocket license information -main.menu.help.bugReport = Fehlerbericht -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 = Über -main.menu.help.about.desc = Copyright details about OpenRocket - -main.menu.debug = Debug -main.menu.debug.whatisthismenu = Was macht diese Menü? -main.menu.debug.createtestrocket = Eine Testrakete erstellen - -! database -! Translate here all material database -! - -! Material database -! BULK_MATERIAL -Databases.materials.Acrylic = Acryl -Databases.materials.Balsa = Balsa -Databases.materials.Birch = Birke -Databases.materials.Cardboard = Karton -Databases.materials.Carbonfiber = Kohlefaser -Databases.materials.Cork = Kork -Databases.materials.DepronXPS = Depron (XPS) -Databases.materials.Fiberglass = Glasfaser -Databases.materials.Kraftphenolic = Pertinax -Databases.materials.Maple = Ahorn -Databases.materials.Paperoffice = Papier (Büro) -Databases.materials.Pine = Kiefer -Databases.materials.Plywoodbirch = Sperrholz (Birke) -Databases.materials.PolycarbonateLexan = Polycarbonat (Lexan) -Databases.materials.Polystyrene = Polystyrène -Databases.materials.PVC = PVC -Databases.materials.Spruce = Fichte -Databases.materials.StyrofoamgenericEPS = Styropor (EPS) -Databases.materials.StyrofoamBluefoamXPS = Styrodur (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 = Polyethylen (dünn) -Databases.materials.Polyethyleneheavy = Polyethylen (schwer) -Databases.materials.Silk = Seide -Databases.materials.Paperoffice = Papier (Büro) -Databases.materials.Cellophane = Zellophan -Databases.materials.Crepepaper = Krepppapier -! LINE_MATERIAL -Databases.materials.Threadheavy-duty = Faden (stark) -Databases.materials.Elasticcordround2mm = Elastikband (rund, 2mm, 1/16 in) -Databases.materials.Elasticcordflat6mm = Elastikband (flach, 6mm, 1/4 in) -Databases.materials.Elasticcordflat12mm = Elastikband (flach, 12mm, 1/2 in) -Databases.materials.Elasticcordflat19mm = Elastikband (flach, 19mm, 3/4 in) -Databases.materials.Elasticcordflat25mm = Elastikband (flach, 25mm, 1 in) -Databases.materials.Braidednylon2mm = Nylonflachband (2 mm, 1/16 in) -Databases.materials.Braidednylon3mm = Nylonflachband (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 = Rau -ExternalComponent.Unfinished = unbehandelt -ExternalComponent.Regularpaint = normale Farbe -ExternalComponent.Smoothpaint = glatte Farbe -ExternalComponent.Polished = poliert - -! LineStyle -LineStyle.Solid = durchgehend -LineStyle.Dashed = gestrichelt -LineStyle.Dotted = gepunktet -LineStyle.Dash-dotted = Strich-Punkt -LineStyle.Defaultstyle = Standardstil - -! Shape -Shape.Conical = Konisch -Shape.Conical.desc1 = Eine konische Spitze hat ein dreieckiges Profil -Shape.Conical.desc2 = Ein konischer Übergang hat gerade Kanten -Shape.Ogive = Ogive -Shape.Ogive.desc1 = Eine ogive Spitze hat das Profil eines Kreissegments. Der Formparamter 1 erzeugt eine tangentiale Ogive, die einen weichen Übergang zum Körperrohr hat, Werte kleiner 1 erzeugen eine sekante Ogive. -Shape.Ogive.desc2 = Eine ogive Spitze hat das Profil eines Kreissegments. Der Formparamter 1 erzeugt eine tangentiale Ogive, die einen weichen Übergang zum Körperrohr am hinteren Ende hat, Werte kleiner 1 erzeugen eine sekante Ogive. -Shape.Ellipsoid = Ellipsoid -Shape.Ellipsoid.desc1 = Eine ellipsoide Spitze hat ein Profil einer Halbellipse mit der einer Hauptachsenlänge von 2×Länge und Durchmesser -Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×Length and Diameter. 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 Radius × (x / Length)k where k is the shape parameter. For k=0.5 this is a \u00BD-power or parabolic nose cone, for k=0.75 a \u00BE-power, and for k=1 a conical nose cone. -Shape.Powerseries.desc2 = A power series transition has a profile of Radius × (x / Length)k where k is the shape parameter. For k=0.5 the transition is \u00BD-power or parabolic, for k=0.75 a \u00BE-power, and for k=1 conical. -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 full parabola which is tangent to the body tube, 0.75 produces a 3/4 parabola, 0.5 procudes a 1/2 parabola and 0 produces a conical 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 full parabola which is tangent to the body tube at the aft end, 0.75 produces a 3/4 parabola, 0.5 procudes a 1/2 parabola and 0 produces a conical transition. -Shape.Haackseries = Haack series -Shape.Haackseries.desc1 = The Haack series nose cones are designed to minimize drag. The shape parameter 0 produces an LD-Haack or Von Karman nose cone, which minimizes drag for fixed length and diameter, while a value of 0.333 produces an LV-Haack nose cone, which minimizes drag for fixed length and volume. -Shape.Haackseries.desc2 = The Haack series nose cones 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 LD-Haack or Von Karman shape, while a value of 0.333 produces an LV-Haack shape. - - -! RocketComponent -RocketComponent.Position.TOP = oberes Ende der übergeordneten Komponente -RocketComponent.Position.MIDDLE = Mitte der übergeordneten Komponente -RocketComponent.Position.BOTTOM = unteres Ende der übergeordneten Komponente -RocketComponent.Position.AFTER = nach der übergeordneten Komponente -RocketComponent.Position.ABSOLUTE = zur Spitze - -! LaunchLug -LaunchLug.Launchlug = Leitröhrchen -! NoseCone -NoseCone.NoseCone = Spitze -! Transition -Transition.Transition = Übergang -!Stage -Stage.Stage = Stufe -! BodyTube -BodyTube.BodyTube = Körperrohr -! TubeCoupler -TubeCoupler.TubeCoupler = Koppler -!InnerTube -InnerTube.InnerTube = Innenrohr -! TrapezoidFinSet -TrapezoidFinSet.TrapezoidFinSet = Trapezoide Leitwerke -! FreeformFinSet -FreeformFinSet.FreeformFinSet = Frei geformte Leitwerke -!MassComponent -MassComponent.MassComponent = Masse -! Parachute -Parachute.Parachute = Fallschirm -! ShockCord -ShockCord.ShockCord = Gummiband -! Bulkhead -Bulkhead.Bulkhead = Schott - -!Rocket -Rocket.motorCount.Nomotor = [Keine Motoren] -Rocket.compname.Rocket = Rakete - -!MotorMount -MotorMount.IgnitionEvent.AUTOMATIC = Automatisch (Start oder Ausstoßladung) -MotorMount.IgnitionEvent.LAUNCH = Start -MotorMount.IgnitionEvent.EJECTION_CHARGE = Erste Ausstoßladung der vorherigen Stufe -MotorMount.IgnitionEvent.BURNOUT = Erster Brennschluss der vorherigen Stufe -MotorMount.IgnitionEvent.NEVER = Nie - -!ComponentIcons -ComponentIcons.Nosecone = Spitze -ComponentIcons.Bodytube = Körperrohr -ComponentIcons.Transition = Übergang -ComponentIcons.Trapezoidalfinset = Trapezoide Leitwerke -ComponentIcons.Ellipticalfinset = Elliptische Leitwerke -ComponentIcons.Freeformfinset = Frei geformte Leitwerke -ComponentIcons.Launchlug = Leitröhrchen -ComponentIcons.Innertube = Innenrohr -ComponentIcons.Tubecoupler = Koppler -ComponentIcons.Centeringring = Zentrierring -ComponentIcons.Bulkhead = Schott -ComponentIcons.Engineblock = Motorhalterung -ComponentIcons.Parachute = Fallschirm -ComponentIcons.Streamer = Strömer -ComponentIcons.Shockcord = Gummiband -ComponentIcons.Masscomponent = Masse -ComponentIcons.disabled = (deaktiviert) - -! StageAction -StageAction.Stage = Stufe - -! RecoveryDevice -RecoveryDevice.DeployEvent.LAUNCH = Start (plus NN Sekunden) -RecoveryDevice.DeployEvent.EJECTION = Erste Ausstoßladung dieser Stufe -RecoveryDevice.DeployEvent.APOGEE = Apogäum -RecoveryDevice.DeployEvent.ALTITUDE = Spezifische Höhe während der Landephase -RecoveryDevice.DeployEvent.NEVER = Nie - -! FlightEvent -FlightEvent.Type.LAUNCH = Start -FlightEvent.Type.IGNITION = Motorzündung -FlightEvent.Type.LIFTOFF = Abheben -FlightEvent.Type.LAUNCHROD = Verlassen der Startrampe -FlightEvent.Type.BURNOUT = Motorbrennschluss -FlightEvent.Type.EJECTION_CHARGE = Ausstoßladung -FlightEvent.Type.STAGE_SEPARATION = Stufentrennung -FlightEvent.Type.APOGEE = Apogäum -FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Auslösung des Bergungssystems -FlightEvent.Type.GROUND_HIT = Landung -FlightEvent.Type.SIMULATION_END = Ende der Simulation -FlightEvent.Type.ALTITUDE = Höhenänderung - -! ThrustCurveMotorColumns -TCurveMotorCol.MANUFACTURER = Hersteller -TCurveMotorCol.DESIGNATION = Bezeichnung -TCurveMotorCol.TYPE = Typ -TCurveMotorCol.DIAMETER = Durchmesser -TCurveMotorCol.LENGTH = Länge - -! RocketInfo -RocketInfo.lengthLine.Length = Länge -RocketInfo.lengthLine.maxdiameter = , max. Durchmesser -RocketInfo.massText1 = Masse mit Motoren -RocketInfo.massText2 = Masse ohne Motoren -RocketInfo.at = bei M= -RocketInfo.cgText = CG: -RocketInfo.cpText = CP: -RocketInfo.stabText = Stabilität: -RocketInfo.Warning = Warnung: -RocketInfo.Calculating = Berechne... -RocketInfo.Apogee = Apogäum: -RocketInfo.Maxvelocity = max. Geschwindigkeit: -RocketInfo.Maxacceleration = max. Beschleunigung: -RocketInfo.apogeeValue = N/A -RocketInfo.Mach = (Mach -RocketInfo.velocityValue = N/A -RocketInfo.accelerationValue = N/A - -! FinSet -FinSet.CrossSection.SQUARE = Quadrat -FinSet.CrossSection.ROUNDED = Abgerundet -FinSet.CrossSection.AIRFOIL = Tragfläche -FinSet.TabRelativePosition.FRONT = Root chord leading edge -FinSet.TabRelativePosition.CENTER = Root chord midpoint -FinSet.TabRelativePosition.END = Root chord trailing edge - -! FlightDataType -FlightDataType.TYPE_TIME = Zeit -FlightDataType.TYPE_ALTITUDE = Höhe -FlightDataType.TYPE_VELOCITY_Z = Vertikalgeschwindigkeit -FlightDataType.TYPE_ACCELERATION_Z = Vertikalbeschleunigung -FlightDataType.TYPE_VELOCITY_TOTAL = Gesamtgeschwindigkeit -FlightDataType.TYPE_ACCELERATION_TOTAL = Gesamtbeschleunigung -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 = Angriffswinkel -FlightDataType.TYPE_ROLL_RATE = Rollrate -FlightDataType.TYPE_PITCH_RATE = Nickrate -FlightDataType.TYPE_YAW_RATE = Gierrate -FlightDataType.TYPE_MASS = Masse -FlightDataType.TYPE_LONGITUDINAL_INERTIA = Longitudinal moment of inertia -FlightDataType.TYPE_ROTATIONAL_INERTIA = Rotational moment of inertia -FlightDataType.TYPE_CP_LOCATION = Position vom CP -FlightDataType.TYPE_CG_LOCATION = Position vom CG -FlightDataType.TYPE_STABILITY = Stabilität in Kalibern -FlightDataType.TYPE_MACH_NUMBER = Machzahl -FlightDataType.TYPE_REYNOLDS_NUMBER = Reynoldszahl -FlightDataType.TYPE_THRUST_FORCE = Schub -FlightDataType.TYPE_DRAG_FORCE = Luftwiderstandskraft -FlightDataType.TYPE_DRAG_COEFF = Luftwiderstandskoeffizient -FlightDataType.TYPE_AXIAL_DRAG_COEFF = Axial drag coefficient -FlightDataType.TYPE_FRICTION_DRAG_COEFF = Reibungskoeffizient -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 = Referenzlänge -FlightDataType.TYPE_REFERENCE_AREA = Referenzfläche -FlightDataType.TYPE_ORIENTATION_THETA = Vertical orientation (zenith) -FlightDataType.TYPE_ORIENTATION_PHI = Lateral orientation (azimuth) -FlightDataType.TYPE_WIND_VELOCITY = Windgeschwindigkeit -FlightDataType.TYPE_AIR_TEMPERATURE = Lufttemperatur -FlightDataType.TYPE_AIR_PRESSURE = Luftdruck -FlightDataType.TYPE_SPEED_OF_SOUND = Schallgeschwindigkeit -FlightDataType.TYPE_TIME_STEP = Simulationsintervall -FlightDataType.TYPE_COMPUTATION_TIME = Berechnnungszeit -FlightDataType.TYPE_LATITUDE = Latitude -FlightDataType.TYPE_LONGITUDE = Longitude -FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration - -! PlotConfiguration -PlotConfiguration.Verticalmotion = Vertikale Bewegung über Zeit -PlotConfiguration.Totalmotion = Gesamte Bewegung über Zeit -PlotConfiguration.Flightside = Flight side profile -PlotConfiguration.Stability = Stabilität über Zeit -PlotConfiguration.Dragcoef = Drag coefficients vs. Mach number -PlotConfiguration.Rollcharacteristics = Roll characteristics -PlotConfiguration.Angleofattack = Angle of attack and orientation vs. time -PlotConfiguration.Simulationtime = Simulationszeitschritt und Berechnungszeit - -! Warning -Warning.LargeAOA.str1 = Large angle of attack encountered. -Warning.LargeAOA.str2 = Large angle of attack encountered ( -Warning.DISCONTINUITY = Unstetigkeit im Raketendurchmesser -Warning.THICK_FIN = Dicke Leitwerke können nicht präzise modelliert werden. -Warning.JAGGED_EDGED_FIN = Gezackte Ecken in Leitwerken können unpräzise Ergebnisse liefern. -Warning.LISTENERS_AFFECTED = Simulationsempfänger haben die Simulation beeinflusst. -Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Bergungssystem wurde ausgelöst während der Motor noch gebrannt hat. -Warning.FILE_INVALID_PARAMETER = Ignoriere ungültigen Parameter. - - -! 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.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! diff --git a/core/l10n/messages_es.properties b/core/l10n/messages_es.properties deleted file mode 100644 index 1fa041df..00000000 --- a/core/l10n/messages_es.properties +++ /dev/null @@ -1,1534 +0,0 @@ -# -# 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 = Esta operación no puede deshacerse. -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 = 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 = Si está conectado a Internet, haga Clik en Enviar informe de errores. -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 = Puede realizar un informe de errores escribiendo en el formulario de abajo y enviarlo.
También puede informar de los errores adjuntando el archivo de su proyecto por email. -bugreport.reportDialog.txt2 = Por favor incluya una breve descripción de lo que estaba haciendo cuando ocurrió el error. -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 = Porta motor: -edtmotorconfdlg.title.Editmotorconf = Mostrar las configuraciones de motor -edtmotorconfdlg.selectcomp = Seleccionar qué componentes tienen la función de porta motor: -edtmotorconfdlg.lbl.Motorconfig = Configuraciones del motor: -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 = Desviación estándar de la velocidad del viento.
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 = La intensidad de la turbulencia es la desviación estándar dividida por la velocidad media del viento.
-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 = Seleccionar para usar el modelo de la International Standard Atmosphere.
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 = La latitud del lugar de lanzamiento afecta la atracción terrestre.
Los valores positivos se dan en el hemisferio Norte, los negativos en el hemisferio Sur. - -simedtdlg.lbl.Longitude = Longitud: -simedtdlg.lbl.ttip.Longitude = Requerido para modelos de elevación y predicción meteorológica. - -simedtdlg.lbl.Altitude = Altitud: -simedtdlg.lbl.ttip.Altitude = Los valores por encima del nivel del mar
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 = Dirección de la varilla de lanzamiento relativa al viento.
-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 = El método Barrowman extendido considera las fuerzas aerodinámicas
que actúan sobre cuerpos cilíndricos en cohetes que vuelan con un
ángulo de ataque (AOA) superior a 10 grados. -simedtdlg.lbl.ExtBarrowman = Barrowman Extendido -simedtdlg.lbl.Simmethod = Método de simulación: -simedtdlg.lbl.ttip.Simmethod1 = El simulador de seis-grados-de-libertad permite al cohete una total libertad durante el vuelo.
-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 = Tiempo entre etapas de simulación.
Un tiempo mas corto de etapa origina una simulación mas exacta pero mas lenta.
-simedtdlg.lbl.ttip.Timestep2 = Con 4th 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 = Extensiones del simulador 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 = Al incluir las computaciones geodésicas se considera una Tierra esférica.
Este aspecto es bastante preciso en la mayoría de los proyectos. -GeodeticComputationStrategy.wgs84.name = Elipsoidal WGS84 -GeodeticComputationStrategy.wgs84.desc = Incluye las computaciones geodésicas sobre la referencia elipsoidal WGS84 utilizando el método de Vicenty.
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 = Esta operación no puede deshacerse. -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 = Caracter para separar campos en el documento exportado.
-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 = Presión CD -componentanalysisdlg.dragTableModel.Col.Base = Base CD -componentanalysisdlg.dragTableModel.Col.friction = Rozamiento CD -componentanalysisdlg.dragTableModel.Col.total = Total CD -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 = Total Cl -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 = Un retén de motor impide que el motor se desplace hacia delante, por dentro del tubo porta motor.

Para añadir un motor, cree un Cuerpo tubular o Tubo interior y desígnelo como porta motor en el casillero Motor. -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 = El acabado del componente afecta a su coeficiente de rozamiento.
-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 = En la masa especificada no se incluye la de los motores.
-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 = Separar los tubos del cluster para convertirlos en componentes internos independientes.
-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 = Coeficiente de arrastre CD: -ParachuteCfg.lbl.longB1 = Coeficiente de rozamiento relativo al área total del paracaídas.
-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 = Coeficiente de rozamiento CD: -StreamerCfg.lbl.longB1 = Coeficiente de rozamiento relativo al área total de la banderola.
-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 = Almacenar todos los datos simulados.
-StorageOptChooser.lbl.longA2 = puede generar archivos muy grandes -StorageOptChooser.rdbut.Every = Cada -StorageOptChooser.lbl.longB1 = Almacenar los valores de impresión de este apartado.
-StorageOptChooser.lbl.longB2 = Genera valores grandes en archivos más pequeños. -StorageOptChooser.lbl.seconds = Segundos -StorageOptChooser.rdbut.Onlyprimfig = Sólo figuras principales -StorageOptChooser.lbl.longC1 = Almacenar sólo los valores en la tabla resumen.
-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 Ojiva tangente, mientras que un valor inferior a 1 produce una Ojiva secante con un perfil más afilado. -Shape.Ogive.desc2 = Transición con perfil de arco de circunferencia. Un valor de forma igual a 1 produce una Transición tangente, mientras que un valor inferior a 1 produce una Transición secante con un perfil más afilado. -Shape.Ellipsoid = Elíptica -Shape.Ellipsoid.desc1 = Ojiva con perfil de media elipse. Por defecto, una elipse de longitud igual al triple de su diámetro. -Shape.Ellipsoid.desc2 = Transición con perfil de media elipse. Por defecto, una elipse de longitud igual al triple de su diámetro. -Shape.Powerseries = Serie potencial -Shape.Powerseries.desc1 = Ojiva cuyo perfil es una curva obtenida a partir de una función potencial f(x)k. Un valor de forma k=0.5 produce una ojiva con perfil de parábola, para k=0.75 se produce una ojiva con perfil potencial, y para k=1 se produce una ojiva con perfil recto u Ojiva cónica. -Shape.Powerseries.desc2 = Transición cuyo perfil es una curva obtenida a partir de una función potencial de Radio  =; (x / L)k donde k es el parámetro de forma. Para k=0.5 la transición es \u00BD-potencial o parabólica, para k=0.75 a \u00BE-potencia, y para k=1 cónica. -Shape.Parabolicseries = Serie parabólica -Shape.Parabolicseries.desc1 = Ojiva con perfil de arco de parábola. Un valor de forma igual a 1 produce una Ojiva tangente, un valor igual a 0.75 produce una parábola de 3/4, un valor igual a 0.5 produce una parábola de 1/2, y un valor igual a 0 produce un perfil recto u Ojiva cónica. -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 parábola de 3/4, un valor de 0.5 produce una parábola de 1/2, 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 Ojiva LD Haack u Ojiva Von Karman que minimiza el arrastre aerodinámico para una determinada longitud y diámetro de la base, mientras que un valor igual a 0.333 produce una Ojiva LV-Haack 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 LD-Haack o Von Karman, mientras que un valor de 0.333 produce una forma LV-Haack. - - -! 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! - diff --git a/core/l10n/messages_fr.properties b/core/l10n/messages_fr.properties deleted file mode 100644 index c095ee74..00000000 --- a/core/l10n/messages_fr.properties +++ /dev/null @@ -1,1524 +0,0 @@ - -# -# French base translation file -# Translated by Tripoli France -# 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_fr.properties - -! RocketActions -RocketActions.checkbox.Donotaskmeagain = Ne plus me demander -RocketActions.lbl.Youcanchangedefop = Vous pouvez changer le mode opératoire par defaut dans les préferences. -RocketActions.showConfirmDialog.lbl1 = Supprimer les simulations sélectionnées? -RocketActions.showConfirmDialog.lbl2 = Cette opération n'est pas réversible. -RocketActions.showConfirmDialog.title = Effacer les simulations -RocketActions.DelCompAct.Delete = Effacer -RocketActions.DelCompAct.ttip.Delete = Effacer la pièce sélectionnée. -RocketActions.DelSimuAct.Delete = Effacer -RocketActions.DelSimuAct.ttip.Delete = Effacer la simulation sélectionnée. -RocketActions.DelAct.Delete = Effacer -RocketActions.DelAct.ttip.Delete = Effacer la pièce ou la simulation sélectionnée. -RocketActions.CutAction.Cut = Couper -RocketActions.CutAction.ttip.Cut = Couper cette pièce ou simulation, l'ajouter au presse papier et l'enlever du projet -RocketActions.CopyAct.Copy = Copier -RocketActions.CopyAct.ttip.Copy = Copier les pièces (et les pièces liées) dans le presse papier. -RocketActions.PasteAct.Paste = Coller -RocketActions.PasteAct.ttip.Paste = Coller la pièce ou simulation présente dans le presse papier dans le projet. -RocketActions.EditAct.Edit = Modifier -RocketActions.EditAct.ttip.Edit = Modifier la pièce sélectionnée. -RocketActions.NewStageAct.Newstage = Nouvel étage -RocketActions.NewStageAct.ttip.Newstage = Ajouter un nouvel étage au projet. -RocketActions.ActBoosterstage = Etage Booster -RocketActions.MoveUpAct.Moveup = Monter -RocketActions.MoveUpAct.ttip.Moveup = Monter la pièce. -RocketActions.MoveDownAct.Movedown = Descendre -RocketActions.MoveDownAct.ttip.Movedown = Descendre la pièce. - -! RocketPanel -RocketPanel.FigTypeAct.Sideview = Vue de coté -RocketPanel.FigTypeAct.ttip.Sideview = Vue de coté -RocketPanel.FigTypeAct.Backview = Vue arrière -RocketPanel.FigTypeAct.ttip.Backview = Vue arrière -RocketPanel.lbl.Motorcfg = Configuration Moteur: -RocketPanel.lbl.infoMessage = Cliquer pour sélectionner    Shift+cliquer pour sélectionner plusieurs    Double-cliquer pour modifier    Click+déplacer pour déplacer - - -! BasicFrame -BasicFrame.SimpleFileFilter1 = Tous les fichiers fusée (*.ork; *.rkt) -BasicFrame.SimpleFileFilter2 = Fichiers OpenRocket (*.ork) -BasicFrame.SimpleFileFilter3 = Fichiers RockSim (*.rkt) -BasicFrame.tab.Rocketdesign = Projet fusée -BasicFrame.tab.Flightsim = Simulations de vol -BasicFrame.title.Addnewcomp = Ajouter une nouvelle pièce -BasicFrame.dlg.lbl1 = Le projet ' -BasicFrame.dlg.lbl2 = ' N'a pas été sauvegardé. -BasicFrame.dlg.lbl3 = Voulez vous le sauvegarder? -BasicFrame.dlg.title = Projet non sauvegardé -BasicFrame.StageName.Sustainer = Sustainer -BasicFrame.WarningDialog.txt1 = Les problèmes suivant sont survenus lors de l'ouverture de -BasicFrame.WarningDialog.txt2 = Certains éléments du projet n'ont peut être pas été chargé correctement. -BasicFrame.WarningDialog.title = Avertissement lors de l'ouverture du fichier - -! General error messages used in multiple contexts -error.fileExists.title = Le fichier existe déjà -error.fileExists.desc = Le fichier '{filename}' existe déjà. Voulez vous l'ecraser? - -error.writing.title = Erreur d'éciture du fichier -error.writing.desc = Une erreur est survenue lors de l'écriture dans le fichier: - -! Labels used in buttons of dialog windows -button.ok = OK -button.cancel = Annuler -button.close = Fermer - -! Common labels used in buttons of dialog windows -dlg.but.ok = Accepter -dlg.but.cancel = Annuler -dlg.but.close = Fermer - - -! General file type names -filetypes.pdf = fichier PDF - - -! 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 = Traduit en français par: -AboutDialog.lbl.translator = Tripoli France -AboutDialog.lbl.translatorWebsite = http://tripoli.france.free.fr/ -AboutDialog.lbl.translatorIcon = logoTripoliFrance.png - -! Print dialog -PrintDialog.title = Imprimer ou exporter -PrintDialog.but.previewAndPrint = Pré-visualiser et imprimer -PrintDialog.checkbox.showByStage = Montrer par étage -PrintDialog.lbl.selectElements = Choisir les éléments à inclure: -printdlg.but.saveaspdf = Sauvegarder en PDF -printdlg.but.preview = Prévisualisation -printdlg.but.settings = Configuration -PrintDialog.error.preview.title = Impossible d'ouvrir la prévisualisation -PrintDialog.error.preview.desc1 = Impossible d'ouvrir la prévisualisation PDF. -PrintDialog.error.preview.desc2 = S'il vous plait utilisez l'option "Sauvegarder en PDF" à la place. - - -!PrintSettingsDialog -PrintSettingsDialog.title = Configuration impression -PrintSettingsDialog.lbl.Templatefillcolor = Couleur de remplissage du modèle: -PrintSettingsDialog.lbl.Templatebordercolor = Couleur des bords du modèle: -PrintSettingsDialog.lbl.Papersize = Dimensions du papier: -PrintSettingsDialog.lbl.Paperorientation = Orientation du papier: -PrintSettingsDialog.but.Reset = Réinitialiser -PrintSettingsDialog.but.Close = Fermer - - -! Bug Report dialog -bugreport.dlg.title = Rapport d'erreurs -bugreport.dlg.but.Sendbugreport = Envoyer un rapport d'erreurs -bugreport.dlg.but.Sendbugreport.Ttip = Envoyer automatiquement un rapport d'erreurs aux développeurs d'OpenRocket -bugreport.dlg.successmsg1 = Rapport d'erreurs envoyé avec succès. -bugreport.dlg.successmsg2 = Merci d'avoir contribué à l'amélioration d'OpenRocket! -bugreport.dlg.successmsg3 = Rapport d'erreurs envoyé -bugreport.dlg.connectedInternet = Si vous êtes connecté sur Internet, vous pouvez tout simplement cliquer sur Envoyer un rapport d'erreurs. -bugreport.dlg.otherwise = Sinon envoyez le texte ci-dessous à l'adresse: -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. -bugreport.dlg.failedmsg1 = OpenRocket n'a pas réussi à envoyer le rapport d'erreur: -bugreport.dlg.failedmsg2 = S'il vous plait envoyez le rapport manuellement à -bugreport.dlg.failedmsg3 = Erreur d'envoi du rapport -bugreport.reportDialog.txt = Vous pouvez signaler une erreur avec OpenRocket en remplissant et en envoyant le message ci-dessous.
Vous pouvez également signaler des erreurs et inclure des pièces jointes sur le site web du projet. -bugreport.reportDialog.txt2 = S'il vous plait ajoutez une courte description de ce que vous faisiez lorsque l'erreur s'est produite. -bugreport.dlg.provideDescription = S'il vous plait veuillez fournir d'abord une description du bug. -bugreport.dlg.provideDescription.title = La description du bug est absente - - -! Debug log dialog -debuglogdlg.but.clear = Effacer -debuglogdlg.OpenRocketdebuglog = Fichier debug d'OpenRocket -debuglogdlg.Displayloglines = Afficher les numéros des lignes: -debuglogdlg.Follow = Suivre -debuglogdlg.col.Time = Heure -debuglogdlg.col.Level = Niveau -debuglogdlg.col.Location = Emplacement -debuglogdlg.col.Message = Message -debuglogdlg.lbl.Loglinenbr = Numéro de la ligne: -debuglogdlg.lbl.Time = Heure: -debuglogdlg.lbl.Level = Niveau: -debuglogdlg.lbl.Location = Emplacement: -debuglogdlg.lbl.Logmessage = Texte du message: -debuglogdlg.lbl.Stacktrace = Stack trace: - - -! Edit Motor configuration dialog -edtmotorconfdlg.but.removemotor = Enlever le moteur -edtmotorconfdlg.but.Selectmotor = Choisir le moteur -edtmotorconfdlg.but.Removeconfiguration = Supprimer la configuration -edtmotorconfdlg.but.Newconfiguration = Nouvelle configuration -edtmotorconfdlg.lbl.Motormounts = Portes moteur: -edtmotorconfdlg.title.Editmotorconf = Changer la configuration moteur -edtmotorconfdlg.selectcomp = Choisir les pièces utilisées par le porte moteur: -edtmotorconfdlg.lbl.Motorconfig = Configurations moteur: -edtmotorconfdlg.lbl.Configname = Nom de la configuration: -edtmotorconfdlg.lbl.Leavenamedefault = Laisser le champ vide par défaut. - -! Example design dialog -exdesigndlg.but.open = Ouvrir -exdesigndlg.lbl.Selectexample = Choisir l'exemple de projet à ouvrir: -exdesigndlg.lbl.Openexampledesign = Ouvrir un exemple de projet -exdesigndlg.lbl.Exampledesignsnotfound = Impossible de trouver les exemples de projets. -exdesigndlg.lbl.Examplesnotfound = Exemples non trouvés - - -! Material edit panel -matedtpan.but.new = Nouveau -matedtpan.but.edit = Editer -matedtpan.but.delete = Effacer -matedtpan.but.revertall = Revenir aux valeurs précédentes -matedtpan.col.Material = Matériaux -matedtpan.col.Type = Type -matedtpan.col.Density = Densité -matedtpan.col.but.ttip.New = Ajouter un nouveau matériau -matedtpan.title.Addcustmaterial = Ajouter un matériau personnalisé -matedtpan.but.ttip.edit = Modifier un matériau existant -matedtpan.title.Editmaterial = Modifier un matériau -matedtpan.title2.Editmaterial = Les matériaux prédéfinis ne peuvent pas être modifiés. -matedtpan.but.ttip.delete = Supprimer un matériau personnalisé -matedtpan.but.ttip.revertall = Supprimer tous les matériaux personnalisés -matedtpan.title.Deletealluser-defined = Effacer tous les matériaux personalisés? -matedtpan.title.Revertall = Revenir aux valeurs précédentes? -matedtpan.lbl.edtmaterials = Modifier les matériaux n'affectera pas les projets fusée existants. - -!MaterialModel -MaterialModel.title.Material = Matériau -MaterialModel.title.Defcustmat = Définir un matériau personnalisé - - -! Preference dialog -pref.dlg.but.add = Ajouter -pref.dlg.but.reset = Réinitialiser -pref.dlg.but.checknow = Vérifier maintenant -pref.dlg.but.defaultmetric = Système métrique -pref.dlg.but.defaultimperial = Système impérial -pref.dlg.title.Preferences = Préférences -pref.dlg.tab.Units = Unités -pref.dlg.tab.Defaultunits = Unités par défaut -pref.dlg.tab.Materials = Matériaux -pref.dlg.tab.Custommaterials = Matériaux personnalisés -pref.dlg.tab.Options = Options -pref.dlg.tab.Miscellaneousoptions = Autres options -pref.dlg.lbl.Positiontoinsert = Position pour insérer des composants internes: -pref.dlg.lbl.Confirmdeletion = Confirmer l'effacement des simulations: -pref.dlg.lbl.User-definedthrust = Courbes de poussée personnalisées: -pref.dlg.Allthrustcurvefiles = Tous les fichiers de courbes de poussée (*.eng; *.rse; *.zip; répertoires) -pref.dlg.RASPfiles = Fichiers moteur RASP (*.eng) -pref.dlg.RockSimfiles = Fichiers moteur RockSim (*.rse) -pref.dlg.ZIParchives = Archives ZIP (*.zip) -pref.dlg.checkbox.Checkupdates = Rechercher les mises à jour au démarrage -pref.dlg.ttip.Checkupdatesnow = Recherchez les mises à jour maintenant -pref.dlg.lbl.Selectprefunits = Choisissez vos unités favorites: -pref.dlg.lbl.Rocketdimensions = Dimensions de la fusée: -pref.dlg.lbl.Linedensity = Epaisseur des lignes: -pref.dlg.lbl.Motordimensions = Dimensions du moteur: -pref.dlg.lbl.Surfacedensity = Densité de la Surface: -pref.dlg.lbl.Distance = Distance: -pref.dlg.lbl.Bulkdensity = Densité apparente: -pref.dlg.lbl.Velocity = Vitesse: -pref.dlg.lbl.Surfaceroughness = Rugosité de la Surface: -pref.dlg.lbl.Acceleration = Accélération: -pref.dlg.lbl.Area = Surface: -pref.dlg.lbl.Mass = Masse: -pref.dlg.lbl.Angle = Angle: -pref.dlg.lbl.Force = Force: -pref.dlg.lbl.Rollrate = Taux de roulis: -pref.dlg.lbl.Totalimpulse = Impulsion totale: -pref.dlg.lbl.Temperature = Température: -pref.dlg.lbl.Momentofinertia = Moment d'inertie: -pref.dlg.lbl.Pressure = Pression: -pref.dlg.lbl.Stability = Stabilité: -pref.dlg.lbl.FlightTime = Durée du vol: -pref.dlg.lbl.effect1 = Les changements prendront effet la prochaine fois que vous ouvrirez une fenêtre. -pref.dlg.lbl.Checkingupdates = Recherche des mises à jour... -pref.dlg.lbl.msg1 = Une erreur est survenue durant la communication avec le serveur. -pref.dlg.lbl.msg2 = Incapable de récupérer les informations de mise à jour -pref.dlg.lbl.msg3 = Vous utilisez la dernière version d'OpenRocket. -pref.dlg.lbl.msg4 = Pas de mises à jour disponible -pref.dlg.PrefChoiseSelector1 = Toujours demander -pref.dlg.PrefChoiseSelector2 = Insérer au milieu -pref.dlg.PrefChoiseSelector3 = Ajouter à la fin -pref.dlg.PrefBooleanSelector1 = Supprimer -pref.dlg.PrefBooleanSelector2 = Confirmer -pref.dlg.Add = Ajouter -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. - -PreferencesDialog.lbl.language = Langue du programme: -PreferencesDialog.languages.default = Valeur système par défaut -PreferencesDialog.lbl.languageEffect = La langue sera changée après avoir redémarré OpenRocket. - -! Simulation edit dialog -simedtdlg.but.runsimulation = Lancer la simulation -simedtdlg.but.resettodefault = Restaurer les paramètres par défaut -simedtdlg.but.add = Ajouter -simedtdlg.but.remove = Enlever -simedtdlg.title.Editsim = Modifier la simulation -simedtdlg.lbl.Simname = Nom de la simulation: -simedtdlg.tab.Launchcond = Conditions de lancement -simedtdlg.tab.Simopt = Options de simulation -simedtdlg.tab.Plotdata = Tracer les données -simedtdlg.tab.Exportdata = Exporter les données -simedtdlg.lbl.Motorcfg = Configuration moteur: -simedtdlg.lbl.ttip.Motorcfg = Choisir la configuration moteur à utiliser. -simedtdlg.combo.ttip.motorconf = Choisir la configuration moteur à utiliser. -simedtdlg.lbl.Wind = Vent -simedtdlg.lbl.Averwindspeed = Vitesse moyenne du vent: -simedtdlg.lbl.ttip.Averwindspeed = Vitesse moyenne du vent par rapport au sol. -simedtdlg.lbl.Stddeviation = Dérive standard: -simedtdlg.lbl.ttip.Stddeviation = La dérive standard de la vitesse du vent.
La vitesse du vent est le double de l'écart-type de la moyenne dans 95% des cas. -simedtdlg.lbl.Turbulenceintensity = Intensité de la turbulence: -simedtdlg.lbl.ttip.Turbulenceintensity1 = L'intensité de la turbulence résulte de la division de la dérive par la vitesse moyenne de vent.
-simedtdlg.lbl.ttip.Turbulenceintensity2 = Les valeurs typiques vont de -simedtdlg.lbl.ttip.Turbulenceintensity3 = à -simedtdlg.border.Atmoscond = Conditions atmosphériques -simedtdlg.checkbox.InterStdAtmosphere = Utiliser les paramètres de l'Atmosphère Standard -simedtdlg.checkbox.ttip.InterStdAtmosphere1 = Sélectionner pour utiliser les paramètres de l'Atmosphère Standard.
Ce modèle à une température de -simedtdlg.checkbox.ttip.InterStdAtmosphere2 = et une pression de -simedtdlg.checkbox.ttip.InterStdAtmosphere3 = au niveau de la mer. -simedtdlg.lbl.Temperature = Température: -simedtdlg.lbl.ttip.Temperature = Température du site de lancement. -simedtdlg.lbl.Pressure = Pression: -simedtdlg.lbl.ttip.Pressure = Pression atmosphérique du site de lancement. -simedtdlg.lbl.Launchsite = Site de lancement -simedtdlg.lbl.Latitude = Latitude: -simedtdlg.lbl.ttip.Latitude = La latitude du site de lancement affecte l'attraction gravitationnelle de la Terre.
> Les valeurs positives sont dans l'hémisphère Nord, les valeurs négatives sur l'hémisphère Sud. - -simedtdlg.lbl.Longitude = Longitude: -simedtdlg.lbl.ttip.Longitude = Nécessaire pour les prédictions du temps and elevation models. - -simedtdlg.lbl.Altitude = Altitude: -simedtdlg.lbl.ttip.Altitude = Altitude du site de lancement par rapport au niveau de la mer.
Cela affecte la position de la fusée dans le modèle atmosphérique. -simedtdlg.border.Launchrod = Rampe de lancement -simedtdlg.lbl.Length = Longueur: -simedtdlg.lbl.ttip.Length = Longueur de la rampe. -simedtdlg.lbl.Angle = Angle: -simedtdlg.lbl.ttip.Angle = Angle de la rampe de lancement par rapport à la verticale. -simedtdlg.lbl.Direction = Direction: -simedtdlg.lbl.ttip.Direction1 = Direction de la rampe de lance par rapport au vent.
-simedtdlg.lbl.ttip.Direction2 = = Face au vent, -simedtdlg.lbl.ttip.Direction3 = = vent arrière. -simedtdlg.border.Simopt = Options de simulation -simedtdlg.lbl.Calcmethod = Méthode de calcul: -simedtdlg.lbl.ttip.Calcmethod = La méthode Barrowman étendue calcule les forces aérodynamique selon
les équations de Barrowman étendues pour arranger plus de pièces. -simedtdlg.lbl.ExtBarrowman = Barrowman étendu -simedtdlg.lbl.Simmethod = Méthode de Simulation: -simedtdlg.lbl.ttip.Simmethod1 = Le simulateur de six degrés de liberté permet la liberté totale de fusée en vol.
-simedtdlg.lbl.ttip.Simmethod2 = Integration is performed using a 4th order Runge-Kutta 4 numerical integration. -simedtdlg.lbl.GeodeticMethod = Calculs Geodetic: -simedtdlg.lbl.ttip.GeodeticMethodTip = Relate to the calculation of coordinates on the earth. This also enables coriolis effect computations. -simedtdlg.lbl.Timestep = Réglage du pas de temps: -simedtdlg.lbl.ttip.Timestep1 = Le temps entre les étapes de la simulation.
Avec un pas de temps plus petit la simulation est plus lente mais également plus précise.
-simedtdlg.lbl.ttip.Timestep2 = The 4th order simulation method is quite accurate with a time step of -simedtdlg.but.ttip.resettodefault = Réinitialiser le pas de temps à sa valeur par défaut ( -simedtdlg.border.Simlist = Auditeurs de simulation -simedtdlg.txt.longA1 = Les auditeurs de simulation sont une fonction avancé qui permet à l'utilisateur d'écrire du code pour suivre et interagir avec la simulation. -simedtdlg.txt.longA2 = Pour plus de détails sur les auditeurs de simulation, reférez vous à la documentation technique d'OpenRocket. -simedtdlg.lbl.Curlist = Auditeurs de simulation actuel: -simedtdlg.lbl.Addsimlist = Ajouter un "auditeur de simulation" -simedtdlg.lbl.Noflightdata = Aucune donnée de vol disponible. -simedtdlg.lbl.runsimfirst = S'il vous plait faites tourner la simulation d'abord. -simedtdlg.chart.Simflight = Vol simulé -simedtdlg.dlg.Simres = Résultats de la simulation -simedtdlg.IntensityDesc.None = Aucune -simedtdlg.IntensityDesc.Verylow = Très basse -simedtdlg.IntensityDesc.Low = Basse -simedtdlg.IntensityDesc.Medium = Moyenne -simedtdlg.IntensityDesc.High = Haute -simedtdlg.IntensityDesc.Veryhigh = Très haute -simedtdlg.IntensityDesc.Extreme = Extrême - -GeodeticComputationStrategy.none.name = Aucune -GeodeticComputationStrategy.none.desc = Ne pas faire de calculs geodetic. -GeodeticComputationStrategy.spherical.name = Approximation sphérique -GeodeticComputationStrategy.spherical.desc = Perform geodetic computations assuming a spherical Earth.
This is sufficiently accurate for almost all purposes. -GeodeticComputationStrategy.wgs84.name = ellipsoïde WGS84 -GeodeticComputationStrategy.wgs84.desc = Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.
Slower and unnecessary in most cases. - - - -! Simulation Panel -simpanel.but.newsimulation = Nouvelle simulation -simpanel.but.editsimulation = Modifier la simulation -simpanel.but.runsimulations = Lancer les simulations -simpanel.but.deletesimulations = Effacer les simulations -simpanel.but.plotexport = Tracer / exporter -simpanel.but.ttip.newsimulation = Ajouter une nouvelle simulation -simpanel.but.ttip.editsim = Modifier la simulation sélectionnée -simpanel.but.ttip.runsimu = Recommencer la simulation sélectionnée -simpanel.but.ttip.deletesim = Effacer les simulations sélectionnées -simpanel.checkbox.donotask = Ne plus me demander -simpanel.lbl.defpref = Vous pouvez changer le mode opératoire par défaut dans préférences. -simpanel.dlg.lbl.DeleteSim1 = Effacer les simulations sélectionnées? -simpanel.dlg.lbl.DeleteSim2 = Cette opération n'est pas réversible. -simpanel.dlg.lbl.DeleteSim3 = Effacer les simulations -simpanel.col.Name = Nom -simpanel.col.Motors = Moteurs -simpanel.col.Apogee = Apogée -simpanel.col.Maxvelocity = Vitesse Max. -simpanel.col.Maxacceleration = Accélération Max. -simpanel.col.Timetoapogee = Temps pour atteindre l'apogée -simpanel.col.Flighttime = Temps de vol -simpanel.col.Groundhitvelocity = Vitesse à l'atterrissage - -! SimulationRunDialog -SimuRunDlg.title.RunSim = Simulations en cour... -SimuRunDlg.lbl.Running = En cour ... -SimuRunDlg.lbl.Simutime = Temps de simulation: -SimuRunDlg.lbl.Altitude = Altitude: -SimuRunDlg.lbl.Velocity = Vitesse: -SimuRunDlg.msg.Unabletosim = Simulation impossible: -SimuRunDlg.msg.errorOccurred = Une erreur s'est produite durant la simulation: -SimuRunDlg.msg.AnException1 = Une exception s'est produite lors de la simulation: -SimuRunDlg.msg.AnException2 = S'il vous plaît faites un rapport d'erreurs avec les détails ci-dessous. -SimuRunDlg.msg.AssertionError1 = Une erreur de calcul s'est produite lors de la simulation. -SimuRunDlg.msg.AssertionError2 = S'il vous plaît faites un rapport d'erreurs avec les détails ci-dessous. -SimuRunDlg.msg.unknownerror1 = Une erreur inconnue s'est produite lors de la simulation. -SimuRunDlg.msg.unknownerror2 = Le programme peut être instable, vous devez enregistrer toutes vos créations et redémarrez OpenRocket maintenant! - - - -! SimulationExportPanel -SimExpPan.desc = Fichiers dont les données sont séparées par une virgule (*.csv) -SimExpPan.border.Vartoexport = Variables à exporter -SimExpPan.but.Selectall = Tout sélectionner -SimExpPan.but.Selectnone = Ne rien sélectionner -SimExpPan.border.Fieldsep = Séparateur de champ -SimExpPan.lbl.Fieldsepstr = Séparateur de champ: -SimExpPan.lbl.longA1 = La chaîne utilisée pour séparer les champs dans le fichier exporté.
-SimExpPan.lbl.longA2 = Utiliser ',' pour un fichier (CSV). -SimExpPan.checkbox.Includesimudesc = Inclure la description de la simulation -SimExpPan.checkbox.ttip.Includesimudesc = Inclure un commentaire au début du fichier pour décrire la simulation. -SimExpPan.border.Comments = Commentaires -SimExpPan.checkbox.Includefielddesc = Inclure les descriptions des champs -SimExpPan.checkbox.ttip.Includefielddesc = Inclure une ligne de commentaire avec la description des variables exportées. -SimExpPan.checkbox.Incflightevents = Inclure les événements de vol -SimExpPan.checkbox.ttip.Incflightevents = Inclure une ligne de commentaire pour chaque évènement de vol. -SimExpPan.lbl.Commentchar = Symbole pour les commentaires: -SimExpPan.lbl.ttip.Commentchar = Le symbole utilisé pour une ligne de commentaires. -SimExpPan.but.Exporttofile = Exporter dans un fichier... -SimExpPan.Fileexists.desc1 = Le fichier \" -SimExpPan.Fileexists.desc2 = \" existe déjà. Ecraser? -SimExpPan.Fileexists.title = Le fichier existe -SimExpPan.ExportingVar.desc1 = Exporter 1 variable sur un total de -SimExpPan.ExportingVar.desc2 = Exportation -SimExpPan.ExportingVar.desc3 = variable sur un total de -SimExpPan.Col.Variable = Variable -SimExpPan.Col.Unit = Unité - - -CsvOptionPanel.separator.space = SPACE -CsvOptionPanel.separator.tab = TAB - - - -! MotorPlot -MotorPlot.title.Motorplot = Courbe du moteur -MotorPlot.but.Select = Sélection -MotorPlot.Chart.Motorthrustcurve = Courbe de poussée moteur -MotorPlot.Chart.Time = Temps / s -MotorPlot.Chart.Thrust = Poussée / N -MotorPlot.txt.Designation = Désignation: -MotorPlot.txt.Manufacturer = Manufacturer: -MotorPlot.txt.Type = Type: -MotorPlot.txt.Delays = Retards: -MotorPlot.txt.Comment = Commentaires:\n - - - -! Simulation plot panel -simplotpanel.lbl.Presetplotconf = Prédéfinir les paramètres du tracé: -simplotpanel.lbl.Xaxistype = Axe des X: -simplotpanel.lbl.Unit = Unités: -simplotpanel.lbl.Yaxistypes = Axe des Y: -simplotpanel.lbl.Flightevents = Evénements du vol: -simplotpanel.but.All = Tous -simplotpanel.but.None = Aucun -simplotpanel.but.NewYaxisplottype = Nouveau type de tracé de l'axe Y -simplotpanel.but.Plotflight = Tracer le vol -simplotpanel.lbl.Axis = Axes: -simplotpanel.but.ttip.Removethisplot = Effacer le tracé -simplotpanel.Desc = Les données seront tracées en fonction du temps même si le type d'Axe des abscisses n'est pas le temps. -simplotpanel.OptionPane.lbl1 = Un maximum de 15 tracés est permis. -simplotpanel.OptionPane.lbl2 = Impossible d'ajouter le tracé -simplotpanel.AUTO_NAME = Auto -simplotpanel.LEFT_NAME = Gauche -simplotpanel.RIGHT_NAME = Droite -simplotpanel.CUSTOM = Personnalisé - -! Component add buttons -compaddbuttons.Bodycompandfinsets = Pièces du corps et ailerons -compaddbuttons.Nosecone = Cône -compaddbuttons.Bodytube = Tube du\ncorps -compaddbuttons.Transition = Transition -compaddbuttons.Trapezoidal = Trapézoïdale -compaddbuttons.Elliptical = Elliptique -compaddbuttons.Freeform = Forme libre -compaddbuttons.Launchlug = Tube de\nguidage -compaddbuttons.Innercomponent = Pièces internes -compaddbuttons.Innertube = Tube interne -compaddbuttons.Coupler = Coupleur -compaddbuttons.Centeringring = Anneau de\ncentrage -compaddbuttons.Bulkhead = Cloison -compaddbuttons.Engineblock = Bague de\nrétention\nmoteur -compaddbuttons.Massobjects = Pièces pleines -compaddbuttons.Parachute = Parachute -compaddbuttons.Streamer = Banderole -compaddbuttons.Shockcord = Cordon\namortisseur -compaddbuttons.Masscomponent = Poids -compaddbuttons.Donotaskmeagain = Ne plus me poser la question -compaddbuttons.Selectcomppos = Position de la pièce -compaddbuttons.lbl.Youcanchange = Vous pouvez modifier le fonctionnement par défaut dans les préférences. -compaddbuttons.lbl.insertcomp = Insérez la pièce après l'élément actuel ou en tant que dernier élément? -compaddbuttons.askPosition.Inserthere = Ajouter ici -compaddbuttons.askPosition.Addtotheend = Ajouter à la fin -compaddbuttons.askPosition.Cancel = Annuler - -! Component Analysis Dialog -componentanalysisdlg.componentanalysis = Analyse pièce -componentanalysisdlg.lbl.winddir = Direction du vent: -componentanalysisdlg.TitledBorder.warnings = Avertissements: -componentanalysisdlg.ToggleBut.worst = Pire -componentanalysisdlg.lbl.angleofattack = Angle d'attaque: -componentanalysisdlg.lbl.machnumber = Mach number: -componentanalysisdlg.lbl.rollrate = Taux de roulis: -componentanalysisdlg.lbl.activestages = Etages actifs: -componentanalysisdlg.lbl.motorconf = Configuration moteur: -componentanalysisdlg.TabStability.Col.Component = Pièce -componentanalysisdlg.TabStability = Stabilité -componentanalysisdlg.TabStability.ttip = Information de stabilité -componentanalysisdlg.dragTableModel.Col.Component = Pièce -componentanalysisdlg.dragTableModel.Col.Pressure = Pression CD -componentanalysisdlg.dragTableModel.Col.Base = Base CD -componentanalysisdlg.dragTableModel.Col.friction = Friction CD -componentanalysisdlg.dragTableModel.Col.total = Total CD -componentanalysisdlg.dragTabchar = Caractéristiques de traînée -componentanalysisdlg.dragTabchar.ttip = Caractéristiques de traînée -componentanalysisdlg.rollTableModel.Col.component = Pièce -componentanalysisdlg.rollTableModel.Col.rollforc = Coefficient de forçage de roulis -componentanalysisdlg.rollTableModel.Col.rolldamp = Coefficient amortisseur de roulis -componentanalysisdlg.rollTableModel.Col.total = Total Cl -componentanalysisdlg.rollTableModel = Dynamique du roulis -componentanalysisdlg.rollTableModel.ttip = Dynamique du roulis -componentanalysisdlg.println.closingmethod = Méthode de clôture appelée: -componentanalysisdlg.println.settingnam = SETTING NAN VALUES -componentanalysisdlg.lbl.reflenght = Longueur de référence: -componentanalysisdlg.lbl.refarea = Aire de référence: -!componentanalysisdlg.but.close =Fermer -componentanalysisdlg.TabStability.Col.Component = Pièce - -! Custom Material dialog -custmatdlg.title.Custommaterial = Matériau personnalisé -custmatdlg.lbl.Materialname = Nom du matériau: -custmatdlg.lbl.Materialtype = Type de matériau: -custmatdlg.lbl.Materialdensity = Densité du matériau: -custmatdlg.checkbox.Addmaterial = Ajouter la pièce dans la base de données - - -! Ring Component Config -ringcompcfg.OuterRadius = Diamètre extérieur -ringcompcfg.Automatic = Automatique -ringcompcfg.InnerRadius = Diamètre intérieur -ringcompcfg.Thickness = Epaisseur -ringcompcfg.Length = Longueur -ringcompcfg.Positionrelativeto = Position relative à: -ringcompcfg.plus = plus -!ringcompcfg.PositionValue = PositionValue -ringcompcfg.Radialdistance = Rayon: -ringcompcfg.Distancefrom = Distance de l'axe central de la fusée -ringcompcfg.Radialdirection = Azimut -ringcompcfg.radialdirectionfrom = Sens par rapport à l'axe central de la fusée -ringcompcfg.but.Reset = Réinitialisation -ringcompcfg.but.Resetcomponant = Réinitialiser la pièce à l'axe de la fusée -ringcompcfg.EngineBlock.desc = Un bloc moteur empêche le moteur de se déplacer vers l'avant dans le tube porte moteur.

Pour ajouter un moteur, créer un tube ou un tube interne et marquer le comme porte moteur dans l'onglet Moteur. -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. - - -! Body Tube Config -BodyTubecfg.lbl.Bodytubelength = Longueur du tube: -BodyTubecfg.lbl.Outerdiameter = Diamètre externe: -BodyTubecfg.lbl.Innerdiameter = Diamètre interne: -BodyTubecfg.lbl.Wallthickness = Epaisseur des parois: -BodyTubecfg.tab.General = Général -BodyTubecfg.tab.Generalproperties = Propriétés générales -BodyTubecfg.tab.Motor = Moteur -BodyTubecfg.tab.Motormountconf = Configuration du porte moteur -BodyTubecfg.checkbox.Automatic = Automatique -BodyTubecfg.checkbox.Filled = Aspérités bouchées - -! FinSetConfig -FinSetConfig.tab.Fintabs = Pattes des ailerons -FinSetConfig.tab.Through-the-wall = Ailerons traversant le fuselage -FinSetConfig.but.Converttofreeform = Convertir en forme libre -FinSetConfig.but.Converttofreeform.ttip = Convertir ce jeu d'ailerons en forme libre -FinSetConfig.Convertfinset = Convertir le jeu d'ailerons -FinSetConfig.but.Splitfins = Séparer les ailerons -FinSetConfig.but.Splitfins.ttip = Diviser le jeu d'ailerons en aileron indépendant -FinSetConfig.lbl.Through-the-wall = Ailerons traversant le fuselage: -FinSetConfig.lbl.Tablength = Longueur de la patte: -FinSetConfig.ttip.Tablength = La longueur de la patte de l'aileron. -FinSetConfig.lbl.Tabheight = Hauteur de la patte: -FinSetConfig.ttip.Tabheight = La hauteur de l'envergure de la patte de l'aileron. -FinSetConfig.lbl.Tabposition = Position de la patte: -FinSetConfig.ttip.Tabposition = La position de la patte de l'aileron. -FinSetConfig.lbl.relativeto = relative à - -! MotorDatabaseLoadingDialog -MotorDbLoadDlg.title = Chargement des moteurs -MotorDbLoadDlg.Loadingmotors = Chargement des moteurs... - -! RocketConfig -RocketCfg.lbl.Designname = Nom du projet: -RocketCfg.lbl.Designer = Concepteur: -RocketCfg.lbl.Comments = Commentaires: -RocketCfg.lbl.Revisionhistory = Historique des modifications: -RocketCfg.lbl.Material = Matériaux: - -! ShockCordConfig -ShockCordCfg.lbl.Shockcordlength = Longueur du cordon amortisseur - -! RocketComponentConfig -RocketCompCfg.lbl.Componentname = Nom de la pièce: -RocketCompCfg.ttip.Thecomponentname = Le nom de la pièce. -RocketCompCfg.tab.Override = Forcer la valeur -RocketCompCfg.tab.MassandCGoverride = Forçage de la Masse et du CG -RocketCompCfg.tab.Figure = Forme -RocketCompCfg.tab.Figstyleopt = Options de la forme -RocketCompCfg.tab.Comment = Commentaires -RocketCompCfg.tab.Specifyacomment = Commentaires concernant la pièce -RocketCompCfg.lbl.Mass = Masse: -RocketCompCfg.lbl.Componentmass = Masse de la pièce: -RocketCompCfg.lbl.overriddento = (forcé à -RocketCompCfg.lbl.overriddenby = (forcé par -RocketCompCfg.lbl.Componentmaterial = Matériaux composant la pièce: -RocketCompCfg.lbl.Componentfinish = Finition de la pièce: -RocketCompCfg.lbl.ttip.componentmaterialaffects = Les matériaux utilisés pour la pièce affectent le poids de la pièce. -RocketCompCfg.combo.ttip.componentmaterialaffects = Les matériaux utilisés pour la pièce affectent le poids de la pièce. -RocketCompCfg.lbl.longA1 = La finition de la pièce affecte l'aérodynamisme de la pièce.
-RocketCompCfg.lbl.longA2 = La valeur indiquée est la hauteur moyenne de la rugosité de la surface. -RocketCompCfg.but.Setforall = Appliquer à tous -RocketCompCfg.but.ttip.Setforall = Régler la finition pour tous les composants de la fusée. -RocketCompCfg.lbl.Overridemassorcenter = Forcer la masse ou le centre de gravité du -RocketCompCfg.checkbox.Overridemass = Forcer la masse: -RocketCompCfg.checkbox.Overridecenterofgrav = Forcer le centre de gravité: -RocketCompCfg.checkbox.OverridemassandCG = Forcer la masse et le centre de gravité de tous les sous composants -RocketCompCfg.lbl.longB1 = Le forçage de la masse n'inclus pas le ou les moteurs.
-RocketCompCfg.lbl.longB2 = Le centre de gravité est mesuré à partir de l'extrémité avant de la fusée -RocketCompCfg.lbl.Commentsonthe = Commentaires à propos du -RocketCompCfg.lbl.Figurestyle = Modèle de forme: -RocketCompCfg.lbl.Componentcolor = Couleur de la pièce: -RocketCompCfg.lbl.Choosecolor = Choisir la couleur -RocketCompCfg.checkbox.Usedefaultcolor = Utiliser la couleur par défaut -RocketCompCfg.lbl.Complinestyle = Style de lignes pour les pièces: -RocketCompCfg.but.Saveasdefstyle = Sauver le modèle par défaut -RocketCompCfg.lbl.Diameter = Diamètre: -RocketCompCfg.lbl.Length = Longueur: -RocketCompCfg.lbl.Thickness = Epaisseur: -RocketCompCfg.checkbox.Endcapped = Arrière clos -RocketCompCfg.ttip.Endcapped = Précise si l'arrière du cône est clos. -RocketCompCfg.title.Noseconeshoulder = Accotement du cône -RocketCompCfg.title.Aftshoulder = Accotement arrière -RocketCompCfg.border.Foreshoulder = Accotement avant -!RocketCompCfg.lbl.Length = Length: - -! BulkheadConfig -BulkheadCfg.tab.Radius = Rayon: -BulkheadCfg.tab.Thickness = Epaisseur: -BulkheadCfg.tab.General = Général -BulkheadCfg.tab.Generalproperties = Propriétés générales - -!CenteringRingConfig -CenteringRingCfg.tab.Outerdiam = Diamètre externe: -CenteringRingCfg.tab.Innerdiam = Diamètre interne: -CenteringRingCfg.tab.Thickness = Epaisseur: -CenteringRingCfg.tab.General = Général -CenteringRingCfg.tab.Generalproperties = Propriétés Générales - -!ComponentConfigDialog -ComponentCfgDlg.configuration = -ComponentCfgDlg.configuration1 = configuration -ComponentCfgDlg.Modify = Modifier - -!EllipticalFinSetConfig -EllipticalFinSetCfg.Nbroffins = Nombre d'ailerons: -EllipticalFinSetCfg.Rotation = Rotation: -EllipticalFinSetCfg.Fincant = Inclinaison de l'aileron: -EllipticalFinSetCfg.Rootchord = Emplanture: -EllipticalFinSetCfg.Height = Hauteur: -EllipticalFinSetCfg.Positionrelativeto = Position relative à: -EllipticalFinSetCfg.plus = plus -EllipticalFinSetCfg.FincrossSection = Coupe de l'aileron: -EllipticalFinSetCfg.Thickness = Epaisseur: -EllipticalFinSetCfg.General = Général -EllipticalFinSetCfg.Generalproperties = Propriétés Générales -EllipticalFinSetCfg.ttip.Fincant = Angle d'inclinaison des ailerons par rapport au corps de la fusée - -!FreeformFinSetConfig -FreeformFinSetCfg.tab.General = Général -FreeformFinSetCfg.tab.ttip.General = Propriétés générales -FreeformFinSetCfg.tab.Shape = Forme -FreeformFinSetCfg.tab.ttip.Finshape = Forme de l'aileron -FreeformFinSetCfg.lbl.Numberoffins = Nombre d'ailerons: -FreeformFinSetCfg.lbl.Finrotation = Rotation des ailerons: -FreeformFinSetCfg.lbl.Fincant = Inclinaison de l'aileron: -FreeformFinSetCfg.lbl.ttip.Fincant = angle d'inclinaison des ailerons par rapport au corps de la fusée. -FreeformFinSetCfg.lbl.Posrelativeto = Position par rapport à: -FreeformFinSetCfg.lbl.plus = plus -FreeformFinSetCfg.lbl.FincrossSection = Coupe de l'aileron: -FreeformFinSetCfg.lbl.Thickness = Epaisseur: -! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle -FreeformFinSetCfg.lbl.doubleClick1 = Double-click -FreeformFinSetCfg.lbl.doubleClick2 = pour éditer -FreeformFinSetCfg.lbl.clickDrag = Cliquer+déplacer: Ajouter et déplacer des points -FreeformFinSetCfg.lbl.ctrlClick = Ctrl+cliquer: Enlever un point - - -!InnerTubeConfig -InnerTubeCfg.tab.Motor = Moteur -InnerTubeCfg.tab.ttip.Motor = Configuration du porte moteur -InnerTubeCfg.tab.Cluster = Cluster -InnerTubeCfg.tab.ttip.Cluster = Configuration du cluster -InnerTubeCfg.tab.Radialpos = Position circulaire -InnerTubeCfg.tab.ttip.Radialpos = Position circulaire -InnerTubeCfg.lbl.Selectclustercfg = Choisir la configuration du cluster: -InnerTubeCfg.lbl.TubeSep = Séparation du tube: -InnerTubeCfg.lbl.ttip.TubeSep = La Séparation des tubes, 1.0 = chacun se touche -InnerTubeCfg.lbl.Rotation = Rotation: -InnerTubeCfg.lbl.ttip.Rotation = Angle de rotation du cluster -InnerTubeCfg.lbl.Rotangle = Angle de rotation de la configuration du cluster -InnerTubeCfg.but.Splitcluster = Séparer le cluster -InnerTubeCfg.lbl.longA1 = séparer le cluster en pièces distinctes.
-InnerTubeCfg.lbl.longA2 = Cela duplique également tous les composants rattacher à ce tube interne. -InnerTubeCfg.but.Resetsettings = Réinitialiser les réglages -InnerTubeCfg.but.ttip.Resetsettings = Réinitialiser la séparation et la rotation aux valeurs par défauts - -! LaunchLugConfig -LaunchLugCfg.lbl.Length = Longueur: -LaunchLugCfg.lbl.Outerdiam = Diamètre externe: -LaunchLugCfg.lbl.Innerdiam = Diamètre interne: -LaunchLugCfg.lbl.Thickness = Epaisseur: -LaunchLugCfg.lbl.Radialpos = Position circulaire: -LaunchLugCfg.lbl.Posrelativeto = Position relative à: -LaunchLugCfg.lbl.plus = plus -LaunchLugCfg.tab.General = Général -LaunchLugCfg.tab.Generalprop = Propriétés Générales - -! MassComponentConfig -MassComponentCfg.lbl.Mass = Masse -MassComponentCfg.lbl.Length = Longueur -MassComponentCfg.lbl.Diameter = Diamètre -MassComponentCfg.lbl.PosRelativeto = Position relative à: -MassComponentCfg.lbl.plus = plus -MassComponentCfg.tab.General = Général -MassComponentCfg.tab.ttip.General = Propriétés Générales -MassComponentCfg.tab.Radialpos = Position sur le périmètre -MassComponentCfg.tab.ttip.Radialpos = Configuration de la position sur le périmètre -MassComponentCfg.lbl.Radialdistance = Rayon: -MassComponentCfg.lbl.Radialdirection = Azimut: -MassComponentCfg.but.Reset = Réinitialiser - -! MotorConfig -MotorCfg.checkbox.compmotormount = Cette pièce est un porte moteur -MotorCfg.lbl.Motorcfg = Configuration du moteur: -MotorCfg.but.New = Nouveau -MotorCfg.lbl.Currentmotor = Moteur actuel: -MotorCfg.lbl.Motoroverhang = Surplomb du moteur: -MotorCfg.lbl.Ignitionat = Allumage à: -MotorCfg.lbl.plus = plus -MotorCfg.lbl.seconds = secondes -MotorCfg.lbl.longA1 = Le projet actuel n'a qu'un étage. -MotorCfg.lbl.longA2 = Des étages peuvent-être ajoutés en cliquant \"Nouvel étage\". -MotorCfg.lbl.longB1 = Le projet actuel a -MotorCfg.lbl.longB2 = étage(s). -MotorCfg.but.Selectmotor = Choisir le moteur -MotorCfg.but.Removemotor = Enlever le moteur -MotorCfg.lbl.motorLabel = Aucun - -! NoseConeConfig -NoseConeCfg.lbl.Noseconeshape = Forme du cône de la fusée: -NoseConeCfg.lbl.Shapeparam = Paramètre de la forme: -NoseConeCfg.lbl.Noseconelength = Longueur du cône de la fusée: -NoseConeCfg.lbl.Basediam = Diamètre de la base: -NoseConeCfg.checkbox.Automatic = Automatique -NoseConeCfg.lbl.Wallthickness = Epaisseur de la paroi: -NoseConeCfg.checkbox.Filled = Aspérités bouchées -NoseConeCfg.tab.General = Général -NoseConeCfg.tab.ttip.General = Propriétés générales -NoseConeCfg.tab.Shoulder = Accotement -NoseConeCfg.tab.ttip.Shoulder = Propriétés de l'accotement - -! ParachuteConfig -ParachuteCfg.lbl.Canopy = Canopée: -ParachuteCfg.lbl.Diameter = Diamètre: -ParachuteCfg.lbl.Material = Matériau: -ParachuteCfg.combo.MaterialModel = La nature du matériau affecte le poids de la pièce. -ParachuteCfg.lbl.longA1 = Coefficient de traînée CD: -ParachuteCfg.lbl.longB1 = Le coefficient de traînée dépend de la surface totale du parachute.
-ParachuteCfg.lbl.longB2 = Un plus grand coefficient de trainée produit une descente plus lente. -ParachuteCfg.lbl.longB3 = Une valeur standard pour le parachute est 0.8. -ParachuteCfg.but.Reset = Réinitialiser -ParachuteCfg.lbl.Shroudlines = Suspentes: -ParachuteCfg.lbl.Numberoflines = Nombre de suspentes: -ParachuteCfg.lbl.Linelength = Longueur des suspentes: -ParachuteCfg.lbl.Material = Matériau: -ParachuteCfg.lbl.Posrelativeto = Position relative à: -ParachuteCfg.lbl.plus = plus -ParachuteCfg.lbl.Packedlength = Longueur plié: -ParachuteCfg.lbl.Packeddiam = Diamètre plié: -ParachuteCfg.lbl.Deploysat = Déploiement à: -ParachuteCfg.lbl.seconds = secondes -ParachuteCfg.lbl.Altitude = Altitude: -ParachuteCfg.tab.General = Général -ParachuteCfg.tab.ttip.General = Propriétés générales -ParachuteCfg.tab.Radialpos = Position sur le périmètre -ParachuteCfg.tab.ttip.Radialpos = Configuration de la position radial -ParachuteCfg.lbl.Radialdistance = Rayon: -ParachuteCfg.lbl.Radialdirection = Azimut: -ParachuteCfg.but.Reset = Réinitialiser -ParachuteCfg.lbl.plusdelay = Retard - -! ShockCordConfig -ShockCordCfg.lbl.Shockcordlength = Longueur du cordon amortisseur -ShockCordCfg.lbl.Shockcordmaterial = Matériau du cordon amortisseur: -ShockCordCfg.lbl.Posrelativeto = Position relative à: -ShockCordCfg.lbl.plus = plus -ShockCordCfg.lbl.Packedlength = Longueur emballé: -ShockCordCfg.lbl.Packeddiam = Diamètre emballé: -ShockCordCfg.tab.General = Général -ShockCordCfg.tab.ttip.General = Propriétés générales - -!SleeveConfig -SleeveCfg.tab.Outerdiam = Diamètre externe: -SleeveCfg.tab.Innerdiam = Diamètre interne: -SleeveCfg.tab.Wallthickness = Epaisseur des parois: -SleeveCfg.tab.Length = Longueur: -SleeveCfg.tab.General = Général -SleeveCfg.tab.Generalproperties = Propriétés générales - -! StreamerConfig -StreamerCfg.lbl.Striplength = Longueur de la bande: -StreamerCfg.lbl.Stripwidth = Largeur de la bande: -StreamerCfg.lbl.Striparea = Surface de la bande: -StreamerCfg.lbl.Aspectratio = Proportions: -StreamerCfg.lbl.Material = Matériau: -StreamerCfg.combo.ttip.MaterialModel = La nature du matériau affecte le poids de la pièce. -StreamerCfg.lbl.longA1 = Coefficient de traînée CD: -StreamerCfg.lbl.longB1 = Le coefficient de trainée dépend de la surface totale de la banderole.
-StreamerCfg.lbl.longB2 = Un plus grand coefficient de trainée produit une descente plus lente. -StreamerCfg.lbl.Automatic = Automatique -StreamerCfg.lbl.longC1 = le coefficient de trainée dépend de la surface totale de la banderole. -StreamerCfg.lbl.Posrelativeto = Position relative à: -StreamerCfg.lbl.plus = plus -StreamerCfg.lbl.Packedlength = Longueur emballé: -StreamerCfg.lbl.Packeddiam = Diamètre emballé: -StreamerCfg.lbl.Deploysat = Déploiement à: -StreamerCfg.lbl.seconds = secondes -StreamerCfg.lbl.Altitude = Altitude: -StreamerCfg.tab.General = Général -StreamerCfg.tab.ttip.General = Propriétés générales -StreamerCfg.tab.Radialpos = Position sur le périmètre -StreamerCfg.tab.ttip.Radialpos = Configuration de la position sur le périmètre -StreamerCfg.lbl.Radialdistance = Rayon: -StreamerCfg.lbl.Radialdirection = Azimut: -StreamerCfg.but.Reset = Réinitialiser -StreamerCfg.lbl.plusdelay = Retard - -! ThicknessRingComponentConfig -ThicknessRingCompCfg.tab.Outerdiam = Diamètre externe: -ThicknessRingCompCfg.tab.Innerdiam = Diamètre interne: -ThicknessRingCompCfg.tab.Wallthickness = Epaisseur de la paroi: -ThicknessRingCompCfg.tab.Length = Longueur: -ThicknessRingCompCfg.tab.General = Général -ThicknessRingCompCfg.tab.Generalprop = Propriétés générales - -! TransitionConfig -TransitionCfg.lbl.Transitionshape = Forme de la transition: -TransitionCfg.checkbox.Clipped = Emboitée -TransitionCfg.lbl.Shapeparam = Paramètre de la forme: -TransitionCfg.lbl.Transitionlength = Longueur de la transition: -TransitionCfg.lbl.Forediam = Diamètre avant: -TransitionCfg.checkbox.Automatic = Automatique -TransitionCfg.lbl.Aftdiam = Diamètre arrière: -TransitionCfg.lbl.Wallthickness = Epaisseur de la paroi: -TransitionCfg.checkbox.Filled = Aspérités bouchées -TransitionCfg.tab.General = Général -TransitionCfg.tab.Generalproperties = Propriétés Générales -TransitionCfg.tab.Shoulder = Accotement -TransitionCfg.tab.Shoulderproperties = Propriétés de l'accotement - -! TrapezoidFinSetConfig -TrapezoidFinSetCfg.lbl.Nbroffins = Nombre d'ailerons: -TrapezoidFinSetCfg.lbl.ttip.Nbroffins = Le nombre d'ailerons composant le jeu. -TrapezoidFinSetCfg.lbl.Finrotation = Rotation de l'aileron: -TrapezoidFinSetCfg.lbl.ttip.Finrotation = Angle du premier aileron dans le jeu. -TrapezoidFinSetCfg.lbl.Fincant = Inclinaison de l'aileron: -TrapezoidFinSetCfg.lbl.ttip.Fincant = Angle d'inclinaison des ailerons par rapport au tube du corps de la fusée. -TrapezoidFinSetCfg.lbl.Rootchord = Longueur de la base de l'aileron: -TrapezoidFinSetCfg.lbl.Tipchord = Longueur du bout de l'aileron: -TrapezoidFinSetCfg.lbl.Height = Hauteur: -TrapezoidFinSetCfg.lbl.Sweeplength = Longueur du bord d'attaque: -TrapezoidFinSetCfg.lbl.Sweepangle = Angle du bord d'attaque: -TrapezoidFinSetCfg.lbl.FincrossSection = Coupe de l'aileron: -TrapezoidFinSetCfg.lbl.Thickness = Epaisseur: -TrapezoidFinSetCfg.lbl.Posrelativeto = Position relative à: -TrapezoidFinSetCfg.lbl.plus = plus -TrapezoidFinSetCfg.tab.General = Général -TrapezoidFinSetCfg.tab.Generalproperties = Propriétés générales - -!MotorConfigurationModel -MotorCfgModel.Editcfg = Modifier les configurations - -! StorageOptionChooser -StorageOptChooser.lbl.Simdatatostore = Données simulées à stocker: -StorageOptChooser.rdbut.Allsimdata = Toutes les données des simulations -StorageOptChooser.lbl.longA1 = Enregistrer toutes les données des simulations.
-StorageOptChooser.lbl.longA2 = Cela peut entraîner de très gros fichiers! -StorageOptChooser.rdbut.Every = Every -StorageOptChooser.lbl.longB1 = Store plottable values approximately this far apart.
-StorageOptChooser.lbl.longB2 = Des valeurs plus grandes produisent des fichiers plus petits. -StorageOptChooser.lbl.seconds = secondes -StorageOptChooser.rdbut.Onlyprimfig = Seuls les chiffres primaires -StorageOptChooser.lbl.longC1 = Stocker seulement les valeurs montrées dans le tableau récapitulatif.
-StorageOptChooser.lbl.longC2 = Cela produira des fichiers plus petit. -StorageOptChooser.checkbox.Compfile = Compresse le fichier -StorageOptChooser.lbl.UsingComp = Utiliser la compression réduit significativement la taille du fichier. -StorageOptChooser.lbl.longD1 = Une estimation sur la taille qu'aurait le fichier résultant avec les options actuelles. -StorageOptChooser.ttip.Saveopt = Options de sauvegarde -StorageOptChooser.lbl.Estfilesize = Taille estimée du fichier: -StorageOptChooser.lbl.Saveopt = Options de sauvegarde - -! ThrustCurveMotorSelectionPanel -TCMotorSelPan.lbl.Selrocketmotor = Choisir le moteur fusée: -TCMotorSelPan.checkbox.hideSimilar = Cacher les courbes de poussées similaires -TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Montrer tous les moteurs -TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Montrer les moteurs avec un diamètre inferieur au porte moteur -TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Montrer les moteurs avec un diamètre égale au porte moteur -TCMotorSelPan.lbl.Motormountdia = Diamètre du tube porte moteur: -TCMotorSelPan.lbl.Search = Rechercher: -TCMotorSelPan.lbl.Selectthrustcurve = Choisir la courbe de poussée: -TCMotorSelPan.lbl.Ejectionchargedelay = Retard de la charge d'éjection: -TCMotorSelPan.equalsIgnoreCase.None = Aucun -TCMotorSelPan.lbl.NumberofsecondsorNone = (Nombre de secondes ou \"Aucun\") -TCMotorSelPan.lbl.Totalimpulse = Impulsion totale: -TCMotorSelPan.lbl.Avgthrust = Poussée moyenne: -TCMotorSelPan.lbl.Maxthrust = Poussée Max.: -TCMotorSelPan.lbl.Burntime = Temps de combustion: -TCMotorSelPan.lbl.Launchmass = Masse au lancement: -TCMotorSelPan.lbl.Emptymass = Masse à vide: -TCMotorSelPan.lbl.Datapoints = Points de données: -TCMotorSelPan.lbl.Digest = Assimilation: -TCMotorSelPan.title.Thrustcurve = Courbe de poussée: -TCMotorSelPan.title.Thrust = Poussée -TCMotorSelPan.delayBox.None = Aucun - - -! PlotDialog -PlotDialog.title.Flightdataplot = Tracé du vol -PlotDialog.Chart.Simulatedflight = Simulation du vol -PlotDialog.CheckBox.Showdatapoints = Afficher un point pour chaque valeur -PlotDialog.lbl.Chart = Cliquer+déplacer en bas +droite pour agrandir, haut+gauche pour rétrécir - - -! "main" prefix is used for the main application dialog - -# FIXME: Rename the description keys - -main.menu.file = Fichier -main.menu.file.desc = File-handling related tasks -main.menu.file.new = Nouveau -main.menu.file.new.desc = Crée un nouveau projet fusée -main.menu.file.open = Ouvrir... -BasicFrame.item.Openrocketdesign = Ouvre un projet fusée -main.menu.file.openExample = Ouvrir un exemple... -BasicFrame.item.Openexamplerocketdesign = Ouvre un exemple de projet fusée -main.menu.file.save = Sauvegarder -BasicFrame.item.SavecurRocketdesign = Sauvegarde le projet fusée en cours -main.menu.file.saveAs = Sauvegarder sous... -BasicFrame.item.SavecurRocketdesnewfile = Sauvegarde le projet fusée en cour dans un nouveau fichier -main.menu.file.print = Imprimer/Exporter en PDF... -main.menu.file.print.desc = Imprimer ou sauvegarde en PDF la liste des pièces et les gabaries des ailerons -main.menu.file.close = Fermer -BasicFrame.item.Closedesign = Ferme le projet fusée en cour -main.menu.file.quit = Quitter -BasicFrame.item.Quitprogram = Quitte le programme - -main.menu.edit = Modifier -BasicFrame.menu.Rocketedt = Modification de la fusée -main.menu.edit.undo = Annuler modification -main.menu.edit.undo.desc = Annuler l'opération précédente -main.menu.edit.redo = Refaire modification -main.menu.edit.redo.desc = Refaire l'opération precedente qui avait été défaite -main.menu.edit.cut = Couper -main.menu.edit.copy = Copier -main.menu.edit.paste = Coller -main.menu.edit.delete = Effacer -main.menu.edit.resize = Redimensionner... -main.menu.edit.resize.desc = Redimensionner certaines parties de la fusée -main.menu.edit.preferences = Préférences -main.menu.edit.preferences.desc = Configure les préférences de l'application - -main.menu.analyze = Analyse -main.menu.analyze.desc = Analyses de la fusée -main.menu.analyze.componentAnalysis = Analyse des Pièces -main.menu.analyze.componentAnalysis.desc = Analyse séparé des pices de la fusée -main.menu.analyze.optimization = Optimisation de la fusée -main.menu.analyze.optimization.desc = Optimisation generale de la fusée - -main.menu.help = Aide -main.menu.help.desc = Information à propos d'OpenRocket -main.menu.help.license = Licence -main.menu.help.license.desc = Information sur la license d'OpenRocket -main.menu.help.bugReport = Rapport d'erreurs -main.menu.help.bugReport.desc = Information pour pouvoir sgnaler les bugs dans OpenRocket -main.menu.help.debugLog = Debug log -main.menu.help.debugLog.desc = Visualiser le fichier log d'OpenRocket -main.menu.help.about = A propos -main.menu.help.about.desc = Détails du Copyright d'OpenRocket - -main.menu.debug = Debug -main.menu.debug.whatisthismenu = Quel est ce menu? -main.menu.debug.createtestrocket = Créer une fusée test - -! database -! Translate here all material database -! - -! Material database -! BULK_MATERIAL -Databases.materials.Acrylic = Acrylique -Databases.materials.Balsa = Balsa -Databases.materials.Birch = Bouleau -Databases.materials.Cardboard = Carton -Databases.materials.Carbonfiber = Fibre de carbone -Databases.materials.Cork = Liège -Databases.materials.DepronXPS = Depron (XPS) -Databases.materials.Fiberglass = Fibre de verre -Databases.materials.Kraftphenolic = Kraft phénolique -Databases.materials.Maple = Érable -Databases.materials.Paperoffice = Papier (bureau) -Databases.materials.Pine = Pin -Databases.materials.Plywoodbirch = Contre-plaqué (bouleau) -Databases.materials.PolycarbonateLexan = Polycarbonate (Lexan) -Databases.materials.Polystyrene = Polystyrène -Databases.materials.PVC = PVC -Databases.materials.Spruce = Sapin -Databases.materials.StyrofoamgenericEPS = Polystyrène (générique EPS) -Databases.materials.StyrofoamBluefoamXPS = \"Mousse Bleue\" de polystyrène (XPS) -Databases.materials.Quantumtubing = Tube Quantum -Databases.materials.BlueTube = Blue tube -!SURFACE_MATERIAL -Databases.materials.Ripstopnylon = Ripstop nylon -Databases.materials.Mylar = Mylar -Databases.materials.Polyethylenethin = Polyéthylène (fin) -Databases.materials.Polyethyleneheavy = Polyéthylène (lourd) -Databases.materials.Silk = Soie -Databases.materials.Paperoffice = Papier (bureau) -Databases.materials.Cellophane = Cellophane -Databases.materials.Crepepaper = Papier crépon -! LINE_MATERIAL -Databases.materials.Threadheavy-duty = Fil(résistant) -Databases.materials.Elasticcordround2mm = Corde Elastique (ronde 2mm, 1/16 in) -Databases.materials.Elasticcordflat6mm = Corde Elastique (plate 6mm, 1/4 in) -Databases.materials.Elasticcordflat12mm = Corde Elastique (plate 12mm, 1/2 in) -Databases.materials.Elasticcordflat19mm = Corde Elastique (plate 19mm, 3/4 in) -Databases.materials.Elasticcordflat25mm = Corde Elastique (plate 25mm, 1 in) -Databases.materials.Braidednylon2mm = Nylon tressé (2 mm, 1/16 in) -Databases.materials.Braidednylon3mm = Nylon tressé (3 mm, 1/8 in) -Databases.materials.Tubularnylon11mm = Nylon tubulaire (11 mm, 7/16 in) -Databases.materials.Tubularnylon14mm = Nylon tubulaire (14 mm, 9/16 in) -Databases.materials.Tubularnylon25mm = Nylon tubulaire (25 mm, 1 in) - -! ExternalComponent -ExternalComponent.Rough = Rugueuse -ExternalComponent.Unfinished = Non peinte -ExternalComponent.Regularpaint = Peinture classique -ExternalComponent.Smoothpaint = Fine couche -ExternalComponent.Polished = Polie - -! LineStyle -LineStyle.Solid = Ligne pleine -LineStyle.Dashed = Tiret -LineStyle.Dotted = Ligne pointillée -LineStyle.Dash-dotted = Ligne Pointillée et Tiret -LineStyle.Defaultstyle = Style par défaut - -! Shape -Shape.Conical = Conique -Shape.Conical.desc1 = Un cône conique a un profil triangulaire. -Shape.Conical.desc2 = Une transition conique a des côtés droits. -Shape.Ogive = Ogive -Shape.Ogive.desc1 = Un cône ogival a un profil qui est un segment de cercle. La valeur du paramètre de forme 1 produit une ogive tangente, qui a une transition en douceur vers le tube de la fusée, des valeurs inférieures à 1 produisent des ogives sécantes. -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 ogive tangente, qui a une transition en douceur vers le tube de la fusée à l'extrémité arrière, des valeurs inférieures à 1 produisent des ogives sécantes. -Shape.Ellipsoid = Ellipsoïde -Shape.Ellipsoid.desc1 = Un cône ellipsoïdal a un profil d'une demi ellipse dont les axes principaux sont de longueurs 2×la longueur et diamètre. -Shape.Ellipsoid.desc2 = Une transition ellipsoïdale a un profil d'une demi ellipse dont les axes principaux sont de longueurs 2×longueur et diamètre. Si la transition n'est pas coupée alors le profil est étendu au centre par le rayon correspondant. -Shape.Powerseries = Série Haute puissance -Shape.Powerseries.desc1 = Un cône de puissance a un profil de Rayon × (x / Longueur)k ou k est le paramètre de la forme. Pour k=0,5 c'est une \u00BD-puissance ou une ogive parabolique, pour k=0,75 une \u00BE-puissance, et pour k=1 un cône conique. -Shape.Powerseries.desc2 = Une transition de la série haute puissance a un profile de Rayon × (x / Longueur)k ou k est le paramètre de la forme. Pour k=0,5 la transition est \u00BD-puissance ou parabolique, pour k=0,75 une \u00BE-puissance, et pour k=1 conique. -Shape.Parabolicseries = Série parabolique -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 parabole pleine qui est tangent au tube de la fusée, 0,75 produit un 3/4 de parabole, 0,5 produit une 1/2 parabole et 0 produit un cône conique. -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 parabole pleine qui est tangent au tube de la fusée à l'extrémité arrière, 0,75 produit une 3/4 parabole, 0,5 produit une 1/2 parabole et 0 produit une transition conique. -Shape.Haackseries = Série Haack -Shape.Haackseries.desc1 = Les cônes du type Haack sont conçus pour minimiser la trainée. Le paramètre de forme égale à 0 produit une LD-Haack ou un cône Von Karman, 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 LV-Haack, ce qui minimise la trainée pour une longueur et un volume fixe. -Shape.Haackseries.desc2 = Les cônes 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 LD-Haack ou Von Karman, tandis qu'une valeur de 0,333 produit une forme LV-Haack. - - -! RocketComponent -RocketComponent.Position.TOP = Haut de la pièce parent -RocketComponent.Position.MIDDLE = Milieu de la pièce parent(porteuse) -RocketComponent.Position.BOTTOM = Bas de la pièce parent -RocketComponent.Position.AFTER = Après la pièce parent -RocketComponent.Position.ABSOLUTE = Pointe de l'ogive - -! LaunchLug -LaunchLug.Launchlug = Tube de guidage -! NoseCone -NoseCone.NoseCone = Ogive -! Transition -Transition.Transition = Transition -!Stage -Stage.Stage = Etage -! BodyTube -BodyTube.BodyTube = Tube du corps -! TubeCoupler -TubeCoupler.TubeCoupler = Coupleur de tube -!InnerTube -InnerTube.InnerTube = Tube interne -! TrapezoidFinSet -TrapezoidFinSet.TrapezoidFinSet = Ailerons Trapézoïdaux -! FreeformFinSet -FreeformFinSet.FreeformFinSet = Ailerons personnalisés -!MassComponent -MassComponent.MassComponent = Poids -! Parachute -Parachute.Parachute = Parachute -! ShockCord -ShockCord.ShockCord = Cordon amortisseur -! Bulkhead -Bulkhead.Bulkhead = Cloison - -!Rocket -Rocket.motorCount.Nomotor = [aucun moteurs] -Rocket.compname.Rocket = Fusée - -!MotorMount -MotorMount.IgnitionEvent.AUTOMATIC = Automatique (lancement ou charge d'éjection) -MotorMount.IgnitionEvent.LAUNCH = Lancement -MotorMount.IgnitionEvent.EJECTION_CHARGE = Première charge d'éjection ou étage précédent -MotorMount.IgnitionEvent.BURNOUT = Première combustion totale de l'étage précédent -MotorMount.IgnitionEvent.NEVER = Jamais - -!ComponentIcons -ComponentIcons.Nosecone = Ogive -ComponentIcons.Bodytube = Tube -ComponentIcons.Transition = Transition -ComponentIcons.Trapezoidalfinset = Jeu d'ailerons de forme trapézoïdale -ComponentIcons.Ellipticalfinset = Jeu d'ailerons de forme elliptique -ComponentIcons.Freeformfinset = Jeu d'ailerons de forme personnalisé -ComponentIcons.Launchlug = Tube de guidage -ComponentIcons.Innertube = Tube interne -ComponentIcons.Tubecoupler = Coupleur de tube -ComponentIcons.Centeringring = Anneau de centrage -ComponentIcons.Bulkhead = Cloison -ComponentIcons.Engineblock = Bague de retension moteur -ComponentIcons.Parachute = Parachute -ComponentIcons.Streamer = Banderolle -ComponentIcons.Shockcord = Cordon amortisseur -ComponentIcons.Masscomponent = Piéce Masse -ComponentIcons.disabled = (désactivé) - -! StageAction -StageAction.Stage = Etage - -! RecoveryDevice -RecoveryDevice.DeployEvent.LAUNCH = Lancement(plus NN secondes) -RecoveryDevice.DeployEvent.EJECTION = Première charge d'éjection de cet étage -RecoveryDevice.DeployEvent.APOGEE = Apogée -RecoveryDevice.DeployEvent.ALTITUDE = Altitude spécifiée durant la descente -RecoveryDevice.DeployEvent.NEVER = Jamais - -! FlightEvent -FlightEvent.Type.LAUNCH = Lancement -FlightEvent.Type.IGNITION = Allumage du moteur -FlightEvent.Type.LIFTOFF = Décollage -FlightEvent.Type.LAUNCHROD = Dégagement de rampe de lancement -FlightEvent.Type.BURNOUT = Fin de combustion du moteur -FlightEvent.Type.EJECTION_CHARGE = Charge d'éjection -FlightEvent.Type.STAGE_SEPARATION = Séparation d'étage -FlightEvent.Type.APOGEE = Apogée -FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Déploiement du dispositif de récupération -FlightEvent.Type.GROUND_HIT = Atterrissage -FlightEvent.Type.SIMULATION_END = Fin de la simulation -FlightEvent.Type.ALTITUDE = Changement d'altitude - -! ThrustCurveMotorColumns -TCurveMotorCol.MANUFACTURER = Fabricant -TCurveMotorCol.DESIGNATION = Désignation -TCurveMotorCol.TYPE = Type -TCurveMotorCol.DIAMETER = Diamètre -TCurveMotorCol.LENGTH = Longueur - -! RocketInfo -RocketInfo.lengthLine.Length = Longueur -RocketInfo.lengthLine.maxdiameter = , diamètre max. -RocketInfo.massText1 = Masse avec moteurs -RocketInfo.massText2 = Masse sans moteurs -RocketInfo.at = à M= -RocketInfo.cgText = CG: -RocketInfo.cpText = CP: -RocketInfo.stabText = Stabilité: -RocketInfo.Warning = Avertissement: -RocketInfo.Calculating = Calcul en cours... -RocketInfo.Apogee = Apogée: -RocketInfo.Maxvelocity = Vitesse Max.: -RocketInfo.Maxacceleration = Accélération Max.: -RocketInfo.apogeeValue = N/A -RocketInfo.Mach = (Mach -RocketInfo.velocityValue = N/A -RocketInfo.accelerationValue = N/A - -! FinSet -FinSet.CrossSection.SQUARE = Carré -FinSet.CrossSection.ROUNDED = Arondie -FinSet.CrossSection.AIRFOIL = Airfoil -FinSet.TabRelativePosition.FRONT = Emplanture avant -FinSet.TabRelativePosition.CENTER = Emplanture centrale -FinSet.TabRelativePosition.END = Emplanture arrière - -! FlightDataType -FlightDataType.TYPE_TIME = Temps -FlightDataType.TYPE_ALTITUDE = Altitude -FlightDataType.TYPE_VELOCITY_Z = Vitesse verticale -FlightDataType.TYPE_ACCELERATION_Z = Accélération verticale -FlightDataType.TYPE_VELOCITY_TOTAL = Vitesse totale -FlightDataType.TYPE_ACCELERATION_TOTAL = Accélération totale -FlightDataType.TYPE_POSITION_X = Position contre le vent -FlightDataType.TYPE_POSITION_Y = Position parallèle au vent -FlightDataType.TYPE_POSITION_XY = Distance latérale -FlightDataType.TYPE_POSITION_DIRECTION = Direction latérale -FlightDataType.TYPE_VELOCITY_XY = Vitesse latérale -FlightDataType.TYPE_ACCELERATION_XY = Accélération latérale -FlightDataType.TYPE_AOA = Angle d'attaque -FlightDataType.TYPE_ROLL_RATE = Taux de roulis -FlightDataType.TYPE_PITCH_RATE = Taux de tangage -FlightDataType.TYPE_YAW_RATE = Taux d'embardée -FlightDataType.TYPE_MASS = Masse -FlightDataType.TYPE_LONGITUDINAL_INERTIA = Moment d'inertie longitudinale -FlightDataType.TYPE_ROTATIONAL_INERTIA = Moment d'inertie rotatif -FlightDataType.TYPE_CP_LOCATION = Emplacement du CP -FlightDataType.TYPE_CG_LOCATION = Emplacement du CG -FlightDataType.TYPE_STABILITY = Calibres marge de stabilité -FlightDataType.TYPE_MACH_NUMBER = Mach number -FlightDataType.TYPE_REYNOLDS_NUMBER = Nombre de Reynolds -FlightDataType.TYPE_THRUST_FORCE = Poussée -FlightDataType.TYPE_DRAG_FORCE = Force de traînée -FlightDataType.TYPE_DRAG_COEFF = Coefficient de traînée -FlightDataType.TYPE_AXIAL_DRAG_COEFF = Coefficient de trainée axiale -FlightDataType.TYPE_FRICTION_DRAG_COEFF = Coefficient de traînée de friction -FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Coefficient de traînée de pression -FlightDataType.TYPE_BASE_DRAG_COEFF = Coefficient de traînée de base -FlightDataType.TYPE_NORMAL_FORCE_COEFF = Coefficient de force normale -FlightDataType.TYPE_PITCH_MOMENT_COEFF = Coefficient de moment de tangage -FlightDataType.TYPE_YAW_MOMENT_COEFF = Coefficient de moment d'embardée -FlightDataType.TYPE_SIDE_FORCE_COEFF = Coefficient de force latérale -FlightDataType.TYPE_ROLL_MOMENT_COEFF = Coefficient de moment de roulis -FlightDataType.TYPE_ROLL_FORCING_COEFF = Coefficient de forçage de roulis -FlightDataType.TYPE_ROLL_DAMPING_COEFF = Coefficient d'amortissement de roulis -FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Coefficient d'amortissement de tangage -FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Coefficient d'amortissement d'embardée -FlightDataType.TYPE_REFERENCE_LENGTH = Longueur de référence -FlightDataType.TYPE_REFERENCE_AREA = Surface de référence -FlightDataType.TYPE_ORIENTATION_THETA = Orientation verticale (zénith) -FlightDataType.TYPE_ORIENTATION_PHI = Orientation latérale (azimut) -FlightDataType.TYPE_WIND_VELOCITY = Vitesse de vent -FlightDataType.TYPE_AIR_TEMPERATURE = Température de l'air -FlightDataType.TYPE_AIR_PRESSURE = Pression atmosphérique -FlightDataType.TYPE_SPEED_OF_SOUND = Vitesse du son -FlightDataType.TYPE_TIME_STEP = Pas de simulation du temps -FlightDataType.TYPE_COMPUTATION_TIME = Temps de calcul -FlightDataType.TYPE_LATITUDE = Latitude -FlightDataType.TYPE_LONGITUDE = Longitude -FlightDataType.TYPE_CORIOLIS_ACCELERATION = Accélération de Coriolis - -! PlotConfiguration -PlotConfiguration.Verticalmotion = Mouvement vertical par rapport au temps -PlotConfiguration.Totalmotion = Mouvement total par rapport au temps -PlotConfiguration.Flightside = Profil latéral du vol -PlotConfiguration.Stability = Stabilité par rapport au temps -PlotConfiguration.Dragcoef = Coefficients de traînée par rapport au Mach number -PlotConfiguration.Rollcharacteristics = Caractéristiques de roulis -PlotConfiguration.Angleofattack = Angle d'attaque et orientation par rapport au temps -PlotConfiguration.Simulationtime = Pas du temps et temps de calcul - -! Warning -Warning.LargeAOA.str1 = Grand angle d'attaque rencontré. -Warning.LargeAOA.str2 = Grand angle d'attaque rencontré ( -Warning.DISCONTINUITY = Discontinuité dans le diamètre du corps de la fusée. -Warning.THICK_FIN = Les ailerons fin ne seront peut être pas modélisés correctement. -Warning.JAGGED_EDGED_FIN = Des ailerons aux bords irréguliers ne seront pas modélisés correctement. -Warning.LISTENERS_AFFECTED = Listeners modified the flight simulation -Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Le dispositif de récupération s'est ouvert alors que la combustion du moteur n'était pas finie. -Warning.FILE_INVALID_PARAMETER = Paramètre invalide rencontré, ignorer. - - -! Scale dialog -ScaleDialog.lbl.scaleRocket = Fusée entière -ScaleDialog.lbl.scaleSubselection = La sélection et tous ses composants -ScaleDialog.lbl.scaleSelection = Seulement les composants sélectionnés -ScaleDialog.title = Redimensionner le projet -ScaleDialog.lbl.scale = Mise à l'échelle: -ScaleDialog.lbl.scale.ttip = Choisir de redimensionner tout le projet ou seulement la pièce choisie -ScaleDialog.lbl.scaling = Echelle à appliquer: -ScaleDialog.lbl.scaling.ttip = Taille résultante,les valeurs au-dessus de 100% agrandissent et les valeurs en-dessous de 100% réduisent le design. -! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]" -ScaleDialog.lbl.scaleFrom = Mise à l'échelle de -ScaleDialog.lbl.scaleTo = à -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 = Redimensionner -ScaleDialog.undo.scaleRocket = Redimensionner la fusée -ScaleDialog.undo.scaleComponent = Redimensionner une pièce -ScaleDialog.undo.scaleComponents = Redimensionner les pièces - -!icons -Icons.Undo = Undo -Icons.Redo = Redo - -OpenRocketPrintable.Partsdetail = Détail des pièces -OpenRocketPrintable.Fintemplates = Gabaries des ailerons -OpenRocketPrintable.DesignReport = Rapport de conception - -OpenRocketDocument.Redo = Refaire -OpenRocketDocument.Undo = Défaire - -!EllipticalFinSet -EllipticalFinSet.Ellipticalfinset = Ailerons elliptique - -! Optimization - -! Modifiers - -optimization.modifier.nosecone.length = Longueur du cône -optimization.modifier.nosecone.length.desc = Optimise la longueur du cône. -optimization.modifier.nosecone.diameter = Diamètre du cône -optimization.modifier.nosecone.diameter.desc = Optimise le diamètre du cône. -optimization.modifier.nosecone.thickness = Epaisseur du cône -optimization.modifier.nosecone.thickness.desc = Optimise l'épaisseur des parois du cône. -optimization.modifier.nosecone.shapeparameter = Paramètre de la forme -optimization.modifier.nosecone.shapeparameter.desc = Optimise les paramètres de forme du cône. - -optimization.modifier.transition.length = Longueur de la Transition -optimization.modifier.transition.length.desc = Optimise la longueur de la transition. -optimization.modifier.transition.forediameter = Diamètre avant de la Transition -optimization.modifier.transition.forediameter.desc = Optimise le diamètre avant de la transition. -optimization.modifier.transition.aftdiameter = Diamètre arrière de la transition -optimization.modifier.transition.aftdiameter.desc = Optimise le diamètre arrière de la transition. -optimization.modifier.transition.thickness = Epaisseur de la transition -optimization.modifier.transition.thickness.desc = Optimise l'épaisseur des parois de la transition. -optimization.modifier.transition.shapeparameter = Paramètre de la forme -optimization.modifier.transition.shapeparameter.desc = Optimise le paramètre de la forme. - -optimization.modifier.bodytube.length = Longueur du tube du corps -optimization.modifier.bodytube.length.desc = Optimise la longueur du tube du corps. -optimization.modifier.bodytube.outerDiameter = Diamètre externe du tube du corps -optimization.modifier.bodytube.outerDiameter.desc = Optimise le diamètre externe du tube du corps tout en maintenant l'épaisseur des parois. -optimization.modifier.bodytube.innerDiameter = Diamètre interne du tube du corps -optimization.modifier.bodytube.thickness = Epaisseur du tube du corps -optimization.modifier.bodytube.thickness.desc = Optimise l'épaisseur des parois du tube du corps. - -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 = Hauteur -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 = Hauteur -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 = Optimisation de la position du jeux d'ailerons sur le corps de la fusée. - -optimization.modifier.launchlug.length = Longueur -optimization.modifier.launchlug.length.desc = Optimisation de la longueur du tube de guidage. -optimization.modifier.launchlug.outerDiameter = Diamètre externe -optimization.modifier.launchlug.outerDiameter.desc = Optimisation du diamètre externe du tube de guidage. -optimization.modifier.launchlug.thickness = Epaisseur -optimization.modifier.launchlug.thickness.desc = Optimise l'épaisseur de la bague de guide tout en gardant le diamètre extérieur constant. -optimization.modifier.launchlug.position = Position -optimization.modifier.launchlug.position.desc = Optimise la position de la bague de guidage le long du corps de la fusée. - - -optimization.modifier.internalcomponent.position = Position -optimization.modifier.internalcomponent.position.desc = Optimise la position de la pièce par rapport à la pièce parent. - -optimization.modifier.masscomponent.mass = Masse -optimization.modifier.masscomponent.mass.desc = Optimise la masse du composant. - -optimization.modifier.parachute.diameter = Diamètre -optimization.modifier.parachute.diameter.desc = Optimise le diamètre de la coupole du parachute. -optimization.modifier.parachute.coefficient = Coefficient de trainée -optimization.modifier.parachute.coefficient.desc = Optimisation du coefficient de trainée du parachute. Un parachute type à un coefficient de trainée d'environ 0.8. - -optimization.modifier.streamer.length = Longueur -optimization.modifier.streamer.length.desc = Optimisation de la longueur de la banderole (streamer). -optimization.modifier.streamer.width = Largeur -optimization.modifier.streamer.width.desc = Optimisation de la largeur de la banderole (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 = Coefficient de trainée -optimization.modifier.streamer.coefficient.desc = Optimisation du coéfficient de trainée de la banderole (streamer). - -optimization.modifier.recoverydevice.deployDelay = Retard du déploiement -optimization.modifier.recoverydevice.deployDelay.desc = Optimise le délai du déploiement du système du récupération. -optimization.modifier.recoverydevice.deployAltitude = Altitude du déploiement -optimization.modifier.recoverydevice.deployAltitude.desc = Optimise l'altitude de déploiement du dispositif de récupération. - -optimization.modifier.rocketcomponent.overrideMass = Forcer la masse -optimization.modifier.rocketcomponent.overrideMass.desc = Optimise le forçage de la masse du composant. -optimization.modifier.rocketcomponent.overrideCG = forcer le CG -optimization.modifier.rocketcomponent.overrideCG.desc = Optimise le forçage du centre de gravité du composant. - -optimization.modifier.motormount.overhang = Surplomb du moteur -optimization.modifier.motormount.overhang.desc = Optimise le surplomb du moteur. -optimization.modifier.motormount.delay = Retard de l'allumage moteur -optimization.modifier.motormount.delay.desc = Optimisation du retard d'allumage du moteur. - - - - -! General rocket design optimization dialog - -GeneralOptimizationDialog.title = Optimisation de la fusée -GeneralOptimizationDialog.goal.maximize = Maximiser la valeur -GeneralOptimizationDialog.goal.minimize = Minimiser la valeur -GeneralOptimizationDialog.goal.seek = Cherchez la valeur de -GeneralOptimizationDialog.btn.start = Démarrer l'optimisation -GeneralOptimizationDialog.btn.stop = Terminer l'optimisation -GeneralOptimizationDialog.lbl.paramsToOptimize = Paramètres à optimiser: -GeneralOptimizationDialog.btn.add = Ajouter -GeneralOptimizationDialog.btn.add.ttip = Ajouter le paramètre sélectionné aux paramètres à optimiser -GeneralOptimizationDialog.btn.remove = Enlever -GeneralOptimizationDialog.btn.remove.ttip = Enlever le paramètre sélectionné des paramètres à optimiser -GeneralOptimizationDialog.btn.removeAll = Tout enlever -GeneralOptimizationDialog.btn.removeAll.ttip = Enlever tous les paramètres de l'optimisation -GeneralOptimizationDialog.lbl.availableParams = Paramètres disponible: -GeneralOptimizationDialog.lbl.optimizationOpts = Options pour l'optimisation -GeneralOptimizationDialog.lbl.optimizeSim = Optimiser la simulation: -GeneralOptimizationDialog.lbl.optimizeSim.ttip = Choisir la simulation à optimiser -GeneralOptimizationDialog.lbl.optimizeValue = Valeur optimum -GeneralOptimizationDialog.lbl.optimizeValue.ttip = Choisir quelle valeur à optimiser -GeneralOptimizationDialog.lbl.optimizeGoal = But de l'optimisation: -GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Choisir le but de l'optimisation -GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Valeur personnalisée à rechercher -GeneralOptimizationDialog.lbl.requireStability = Stabilité désirée -GeneralOptimizationDialog.lbl.requireMinStability = Stabilité minimum: -GeneralOptimizationDialog.lbl.requireMinStability.ttip = Exiger une marge de stabilité statique minimale pour le design -GeneralOptimizationDialog.lbl.requireMaxStability = Stabilité maximum: -GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Exiger une marge de stabilité statique maximale pour le design -GeneralOptimizationDialog.status.bestValue = Meilleure valeur: -GeneralOptimizationDialog.status.bestValue.ttip = Meilleure valeur optimum trouvé jusqu'à présent. -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 = Appliquer l'optimisation -GeneralOptimizationDialog.btn.apply.ttip = Appliquer les résultats de l'optimisation au design de la fusée -GeneralOptimizationDialog.btn.reset = Re-Réinitialiser -GeneralOptimizationDialog.btn.reset.ttip = Réinitialiser le design de la fusée au design actuel de la fusée -GeneralOptimizationDialog.btn.close = Fermer -GeneralOptimizationDialog.btn.close.ttip = Fermer la fenêtre de dialogue sans modifier la fusée -GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters. -GeneralOptimizationDialog.error.selectParams.title = Choisir les paramètres de l'optimisation -GeneralOptimizationDialog.error.optimizationFailure.text = L'optimisation n'a pas fonctionnée: -GeneralOptimizationDialog.error.optimizationFailure.title = L'optimisation n'a pas réussie -GeneralOptimizationDialog.undoText = Appliquer l'optimisation -GeneralOptimizationDialog.basicSimulationName = Simulation simple -GeneralOptimizationDialog.noSimulationName = Pas de simulation -GeneralOptimizationDialog.table.col.parameter = Paramètre -GeneralOptimizationDialog.table.col.current = Courant -GeneralOptimizationDialog.table.col.min = Minimum -GeneralOptimizationDialog.table.col.max = Maximum -GeneralOptimizationDialog.export.header = Inclure la ligne d'en tête -GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions. -GeneralOptimizationDialog.export.stability = Stabilité - - -! Dialog for plotting optimization results -OptimizationPlotDialog.title = Résultats de l'optimisation -OptimizationPlotDialog.lbl.zoomInstructions = Click et glisser en bas et à droite pour zoomer plus, en haut et à gauche pour zoomer moins -OptimizationPlotDialog.plot1d.title = Résultat de l'optimisation -OptimizationPlotDialog.plot1d.series = Résultat de l'optimisation -OptimizationPlotDialog.plot2d.title = Optimization path -OptimizationPlotDialog.plot2d.path = Chemin pour l'optimisation -OptimizationPlotDialog.plot2d.evals = Evaluations -OptimizationPlotDialog.plot.ttip.stability = Stabilité: -OptimizationPlotDialog.plot.label.optimum = Optimum - -! Optimization parameters -MaximumAltitudeParameter.name = Altitude de l'apogée -MaximumVelocityParameter.name = Vitesse maximum -MaximumAccelerationParameter.name = Accélération maximum -StabilityParameter.name = Stabilité -GroundHitVelocityParameter.name = Vitesse à l'atterrissage -LandingDistanceParameter.name = Distance à l'atterrissage -TotalFlightTimeParameter.name = Durée totale du vol -DeploymentVelocityParameter.name = Vitesse lors de l'ouverture du parachute - - -! Compass directions drawn on a compass rose. -CompassRose.lbl.north = N -CompassRose.lbl.east = E -CompassRose.lbl.south = S -CompassRose.lbl.west = O - -! 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 = SO -CompassSelectionButton.lbl.W = O -CompassSelectionButton.lbl.NW = NO - - -SlideShowDialog.btn.next = Suivant -SlideShowDialog.btn.prev = Précédent - -GuidedTourSelectionDialog.title = Tours d'horizon -GuidedTourSelectionDialog.lbl.selectTour = Choisir un tour d'horizon: -GuidedTourSelectionDialog.lbl.description = Description du tour d'horizon: -GuidedTourSelectionDialog.lbl.length = Nombre de diapositives: -GuidedTourSelectionDialog.btn.start = Commencer le tour d'horizon! diff --git a/core/resources/l10n/messages.properties b/core/resources/l10n/messages.properties new file mode 100644 index 00000000..3a51de44 --- /dev/null +++ b/core/resources/l10n/messages.properties @@ -0,0 +1,1546 @@ + +# +# 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 = This operation cannot be undone. +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 = 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 = If connected to the Internet, you can simply click Send bug report. +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 = You can report a bug in OpenRocket by filling in and submitting the form below.
You can also report bugs and include attachments on the project web site. +bugreport.reportDialog.txt2 = Please include a short description about what you were doing when the exception occurred. +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 = Motor mounts: +edtmotorconfdlg.title.Editmotorconf = Edit motor configurations +edtmotorconfdlg.selectcomp = Select which components function as motor mounts: +edtmotorconfdlg.lbl.Motorconfig = Motor configurations: +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 = The standard deviation of the windspeed.
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 = The turbulence intensity is the standard deviation divided by the average windspeed.
+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 = Select to use the International Standard Atmosphere model.
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 = The launch site latitude affects the gravitational pull of Earth.
Positive values are on the Northern hemisphere, negative values on the Southern hemisphere. + +simedtdlg.lbl.Longitude = Longitude: +simedtdlg.lbl.ttip.Longitude = Required for weather prediction and elevation models. + +simedtdlg.lbl.Altitude = Altitude: +simedtdlg.lbl.ttip.Altitude = The launch altitude above mean sea level.
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 = Direction of the launch rod relative to the wind.
+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 = The Extended Barrowman method calculates aerodynamic forces according
to the Barrowman equations extended to accommodate more components. +simedtdlg.lbl.ExtBarrowman = Extended Barrowman +simedtdlg.lbl.Simmethod = Simulation method: +simedtdlg.lbl.ttip.Simmethod1 = The six degree-of-freedom simulator allows the rocket total freedom during flight.
+simedtdlg.lbl.ttip.Simmethod2 = Integration is performed using a 4th 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 = The time between simulation steps.
A smaller time step results in a more accurate but slower simulation.
+simedtdlg.lbl.ttip.Timestep2 = The 4th 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 = Simulation listeners 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 = Perform geodetic computations assuming a spherical Earth.
This is sufficiently accurate for almost all purposes. +GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid +GeodeticComputationStrategy.wgs84.desc = Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.
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 = This operation cannot be undone. +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 = The string used to separate the fields in the exported file.
+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 = Pressure CD +componentanalysisdlg.dragTableModel.Col.Base = Base CD +componentanalysisdlg.dragTableModel.Col.friction = Friction CD +componentanalysisdlg.dragTableModel.Col.total = Total CD +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 = Total Cl +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 = An engine block stops the motor from moving forwards in the motor mount tube.

In order to add a motor, create a body tube or inner tube and mark it as a motor mount in the Motor 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 = The component finish affects the aerodynamic drag of the component.
+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 = The overridden mass does not include motors.
+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 = Split the cluster into separate components.
+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 = Drag coefficient CD: +ParachuteCfg.lbl.longB1 = The drag coefficient relative to the total area of the parachute.
+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 = Drag coefficient CD: +StreamerCfg.lbl.longB1 = The drag coefficient relative to the total area of the streamer.
+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 = Store all simulated data.
+StorageOptChooser.lbl.longA2 = This can result in very large files! +StorageOptChooser.rdbut.Every = Every +StorageOptChooser.lbl.longB1 = Store plottable values approximately this far apart.
+StorageOptChooser.lbl.longB2 = Larger values result in smaller files. +StorageOptChooser.lbl.seconds = seconds +StorageOptChooser.rdbut.Onlyprimfig = Only primary figures +StorageOptChooser.lbl.longC1 = Store only the values shown in the summary table.
+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 tangent ogive, which has a smooth transition to the body tube, values less than 1 produce secant ogives. +Shape.Ogive.desc2 = An ogive transition has a profile that is a segment of a circle. The shape parameter value 1 produces a tangent ogive, which has a smooth transition to the body tube at the aft end, values less than 1 produce secant ogives. +Shape.Ellipsoid = Ellipsoid +Shape.Ellipsoid.desc1 = An ellipsoidal nose cone has a profile of a half-ellipse with major axes of lengths 2×Length and Diameter. +Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×Length and Diameter. 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 Radius × (x / Length)k where k is the shape parameter. For k=0.5 this is a \u00BD-power or parabolic nose cone, for k=0.75 a \u00BE-power, and for k=1 a conical nose cone. +Shape.Powerseries.desc2 = A power series transition has a profile of Radius × (x / Length)k where k is the shape parameter. For k=0.5 the transition is \u00BD-power or parabolic, for k=0.75 a \u00BE-power, and for k=1 conical. +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 full parabola which is tangent to the body tube, 0.75 produces a 3/4 parabola, 0.5 procudes a 1/2 parabola and 0 produces a conical 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 full parabola which is tangent to the body tube at the aft end, 0.75 produces a 3/4 parabola, 0.5 procudes a 1/2 parabola and 0 produces a conical transition. +Shape.Haackseries = Haack series +Shape.Haackseries.desc1 = The Haack series nose cones are designed to minimize drag. The shape parameter 0 produces an LD-Haack or Von Karman nose cone, which minimizes drag for fixed length and diameter, while a value of 0.333 produces an LV-Haack nose cone, which minimizes drag for fixed length and volume. +Shape.Haackseries.desc2 = The Haack series nose cones 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 LD-Haack or Von Karman shape, while a value of 0.333 produces an LV-Haack 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! + + diff --git a/core/resources/l10n/messages_de.properties b/core/resources/l10n/messages_de.properties new file mode 100644 index 00000000..0b972fc1 --- /dev/null +++ b/core/resources/l10n/messages_de.properties @@ -0,0 +1,1528 @@ + +# +# German base translation file +# +# 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_de.properties + +! RocketActions +RocketActions.checkbox.Donotaskmeagain = Nicht wieder fragen +RocketActions.lbl.Youcanchangedefop = Die Standardaktion kann in den Einstellungen geändert werden. +RocketActions.showConfirmDialog.lbl1 = Simulationen löschen? +RocketActions.showConfirmDialog.lbl2 = Diese Aktion kann nicht rückgängig gemacht werden. +RocketActions.showConfirmDialog.title = Simulationen löschen +RocketActions.DelCompAct.Delete = Löschen +RocketActions.DelCompAct.ttip.Delete = Die ausgewählte Komponente löschen. +RocketActions.DelSimuAct.Delete = Löschen +RocketActions.DelSimuAct.ttip.Delete = Die ausgewählte Simulation löschen. +RocketActions.DelAct.Delete = Löschen +RocketActions.DelAct.ttip.Delete = Die ausgewählte Komponente oder Simulation löschen. +RocketActions.CutAction.Cut = Ausschneiden +RocketActions.CutAction.ttip.Cut = Diese Komponente oder Simulation ausschneiden und aus dem Design entfernen +RocketActions.CopyAct.Copy = Kopieren +RocketActions.CopyAct.ttip.Copy = Komponente (und Subkomponenten) in die Zwischenablage kopieren. +RocketActions.PasteAct.Paste = Einfügen +RocketActions.PasteAct.ttip.Paste = Fügt die Komponente oder Simulation aus der Zwischenablage in das Design ein. +RocketActions.EditAct.Edit = Bearbeiten +RocketActions.EditAct.ttip.Edit = Die ausgewählte Komponente bearbeiten. +RocketActions.NewStageAct.Newstage = Neue Stufe +RocketActions.NewStageAct.ttip.Newstage = Fügt eine neue Stufe in das Raketendesign ein. +RocketActions.ActBoosterstage = Booster-Stufe +RocketActions.MoveUpAct.Moveup = Nach oben verschieben +RocketActions.MoveUpAct.ttip.Moveup = Verschiebt diese Komponente nach oben. +RocketActions.MoveDownAct.Movedown = Nach unten verschieben +RocketActions.MoveDownAct.ttip.Movedown = Verschiebt diese Komponente nach unten. + +! RocketPanel +RocketPanel.FigTypeAct.Sideview = Seitenansicht +RocketPanel.FigTypeAct.ttip.Sideview = Seitenansicht +RocketPanel.FigTypeAct.Backview = Rückansicht +RocketPanel.FigTypeAct.ttip.Backview = Vorderansicht +RocketPanel.lbl.Motorcfg = Motorkonfiguration +RocketPanel.lbl.infoMessage = Zum Auswählen klicken   Shift+Klick andere auswählen    Doppelklick zum Bearbeiten    Klicken+Ziehen zum Verschieben + + +! BasicFrame +BasicFrame.SimpleFileFilter1 = Alle Raketendesigns (*.ork; *.rkt) +BasicFrame.SimpleFileFilter2 = OpenRocket Designs (*.ork) +BasicFrame.SimpleFileFilter3 = RockSim Designs (*.rkt) +BasicFrame.tab.Rocketdesign = Raketendesign +BasicFrame.tab.Flightsim = Flugsimulation +BasicFrame.title.Addnewcomp = Neue Komponente hinzufügen +BasicFrame.dlg.lbl1 = Design ' +BasicFrame.dlg.lbl2 = ' ist nicht gespeichert. +BasicFrame.dlg.lbl3 = Möchten Sie es speichern? +BasicFrame.dlg.title = Design nicht gespeichert +BasicFrame.StageName.Sustainer = Hauptstufe +BasicFrame.WarningDialog.txt1 = Die folgenden Probleme würden beim Öffnen festgestellt +BasicFrame.WarningDialog.txt2 = Einige Designeigenschaften wurde eventuell nicht korrekt geladen. +BasicFrame.WarningDialog.title = Warnungen während des Öffnens der Datei + + +! 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 +button.ok = OK +button.cancel = Abbrechen +button.close = Schließen + +! Common labels used in buttons of dialog windows +dlg.but.ok = OK +dlg.but.cancel = Abbrechen +dlg.but.close = Schließen + + +! 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 = Ins Deutsche übersetzt von: +AboutDialog.lbl.translator = Stefan Lobas (ERIG e.V.) +AboutDialog.lbl.translatorWebsite = http://www.er-ig.de/ +AboutDialog.lbl.translatorIcon = ERIG_Logo-small.png + + +! Print dialog +PrintDialog.title = Drucken oder exportieren +PrintDialog.but.previewAndPrint = Vorschau & Drucken +PrintDialog.checkbox.showByStage = In Stufen anzeigen +PrintDialog.lbl.selectElements = Elemente auswählen, die berücksichtigt werden sollen: +printdlg.but.saveaspdf = Als PDF speichern +printdlg.but.preview = Vorschau +printdlg.but.settings = Einstellungen +PrintDialog.error.preview.title = Vorschau kann nicht geöffnet werden +PrintDialog.error.preview.desc1 = PDF-Vorschau kann nicht geöffnet werden +PrintDialog.error.preview.desc2 = Bitte "Als PDF speichern" benutzen. + + +!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 = Fehlerbericht +bugreport.dlg.but.Sendbugreport = Fehlerbericht senden +bugreport.dlg.but.Sendbugreport.Ttip = Automatische einen Fehlerbericht an die OpenRocket-Entwickler senden. +bugreport.dlg.successmsg1 = Fehlerbericht erfolgreich gesendet. +bugreport.dlg.successmsg2 = Danke für die Hilfe, OpenRocket noch besser zu machen! +bugreport.dlg.successmsg3 = Fehlerbericht gesendet +bugreport.dlg.connectedInternet = Wenn Sie mit dem Internet verbunden sind, können Sie einfach auf Fehlerbericht senden klicken. +bugreport.dlg.otherwise = Sonst senden Sie den den folgenden Text an diese Adresse: +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! +bugreport.dlg.failedmsg1 = OpenRocket konnte den Fehlerbericht nicht versenden: +bugreport.dlg.failedmsg2 = Bitte senden Sie den Bericht manuell an +bugreport.dlg.failedmsg3 = Fehler beim Versenden des Berichts +bugreport.reportDialog.txt = Sie können eine Fehler in OpenRocket mitteilen, indem Sie das unten stehende Formular ausfüllen und abschicken.
Sie können Fehler mit angehängten Dateien auch auf der Projekt-Website mitteilen. +bugreport.reportDialog.txt2 = Bitte beschreiben Sie kurz, was Sie getan haben, als der Fehler auftrat. +bugreport.dlg.provideDescription = Please provide a description of the bug first. +bugreport.dlg.provideDescription.title = Bug description missing + + +! Debug log dialog +debuglogdlg.but.clear = Löschen +debuglogdlg.OpenRocketdebuglog = OpenRocket Fehler-Log +debuglogdlg.Displayloglines = Zeige Log-Zeilen: +debuglogdlg.Follow = Folgen +debuglogdlg.col.Time = Zeit +debuglogdlg.col.Level = Level +debuglogdlg.col.Location = Ort +debuglogdlg.col.Message = Nachricht +debuglogdlg.lbl.Loglinenbr = Log-Zeilennummer +debuglogdlg.lbl.Time = Zeit: +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 = Motor entfernen +edtmotorconfdlg.but.Selectmotor = Motor auswählen +edtmotorconfdlg.but.Removeconfiguration = Konfiguration entfernen +edtmotorconfdlg.but.Newconfiguration = Neue Konfiguration +edtmotorconfdlg.lbl.Motormounts = Motorhalterungen: +edtmotorconfdlg.title.Editmotorconf = Motorkonfiguration bearbeiten +edtmotorconfdlg.selectcomp = Auswählen, welche Komponenten Motorhalterungen sind: +edtmotorconfdlg.lbl.Motorconfig = Motorkonfigurationen: +edtmotorconfdlg.lbl.Configname = Name der Konfiguration: +edtmotorconfdlg.lbl.Leavenamedefault = Leer lassen für Standardwert. + +! Example design dialog +exdesigndlg.but.open = Öffnen +exdesigndlg.lbl.Selectexample = Beispieldesigns zum Öffnen auswählen: +exdesigndlg.lbl.Openexampledesign = Beispieldesign öffnen +exdesigndlg.lbl.Exampledesignsnotfound = Beispieldesigns konnten nicht gefunden werden. +exdesigndlg.lbl.Examplesnotfound = Beispieldesign konnten nicht gefunden werden + + +! Material edit panel +matedtpan.but.new = Neu +matedtpan.but.edit = Bearbeiten +matedtpan.but.delete = Löschen +matedtpan.but.revertall = Alle löschen +matedtpan.col.Material = Material +matedtpan.col.Type = Typ +matedtpan.col.Density = Dichte +matedtpan.col.but.ttip.New = Neues Material hinzufügen +matedtpan.title.Addcustmaterial = Benutzerdefiniertes Material hinzufügen +matedtpan.but.ttip.edit = Bestehendes Material bearbeiten +matedtpan.title.Editmaterial = Material bearbeiten +matedtpan.title2.Editmaterial = Die mitgelieferten Materialien können nicht verändert werden. +matedtpan.but.ttip.delete = Benutzerdefiniertes Material löschen +matedtpan.but.ttip.revertall = Alle benutzerdefinierten Materialien löschen +matedtpan.title.Deletealluser-defined = Alle benutzerdefinierten Materialien löschen? +matedtpan.title.Revertall = Alle löschen? +matedtpan.lbl.edtmaterials = Das Bearbeiten der Materialien beeinflusst keine bereits existierenden Raketendesigns. + +!MaterialModel +MaterialModel.title.Material = Material +MaterialModel.title.Defcustmat = Benutzerdefiniertes Material definieren + + +! Preference dialog +pref.dlg.but.add = Hinzufügen +pref.dlg.but.reset = Zurücksetzen +pref.dlg.but.checknow = Jetzt überprüfen +pref.dlg.but.defaultmetric = Metrisches System +pref.dlg.but.defaultimperial = Imperialistisches System +pref.dlg.title.Preferences = Einstellungen +pref.dlg.tab.Units = Einheiten +pref.dlg.tab.Defaultunits = Standardeinheiten +pref.dlg.tab.Materials = Materialien +pref.dlg.tab.Custommaterials = Benutzerdefinierte Materialien +pref.dlg.tab.Options = Optionen +pref.dlg.tab.Miscellaneousoptions = Weiter Optionen +pref.dlg.lbl.Positiontoinsert = Position, um neue Komponenten einzufügen: +pref.dlg.lbl.Confirmdeletion = Löschen von Simulationen bestätigen +pref.dlg.lbl.User-definedthrust = Benutzerdefinierte Schubkurven: +pref.dlg.Allthrustcurvefiles = Alle Schubkurvendateien (*.eng; *.rrse; *.zzip; Verzeichnisse) +pref.dlg.RASPfiles = RASP Schubkurven (*.eng) +pref.dlg.RockSimfiles = RockSim Schubkurven(*.rse) +pref.dlg.ZIParchives = ZIP-Archiv (*.zip) +pref.dlg.checkbox.Checkupdates = Beim Starten auf neue Version prüfen +pref.dlg.ttip.Checkupdatesnow = Jetzt auf neue Version prüfen +pref.dlg.lbl.Selectprefunits = Wählen Sie Ihre bevorzugten Einheiten aus: +pref.dlg.lbl.Rocketdimensions = Raketendimensionen: +pref.dlg.lbl.Linedensity = Liniendichte: +pref.dlg.lbl.Motordimensions = Motordimensionen: +pref.dlg.lbl.Surfacedensity = Oberflächendichte: +pref.dlg.lbl.Distance = Entfernung: +pref.dlg.lbl.Bulkdensity = Bulk density:: +pref.dlg.lbl.Velocity = Geschwindigkeit +pref.dlg.lbl.Surfaceroughness = Oberflächenrauhheit: +pref.dlg.lbl.Acceleration = Beschleunigung: +pref.dlg.lbl.Area = Fläche +pref.dlg.lbl.Mass = Masse: +pref.dlg.lbl.Angle = Winkel: +pref.dlg.lbl.Force = Kraft: +pref.dlg.lbl.Rollrate = Roll-Rate: +pref.dlg.lbl.Totalimpulse = Gesamtimpuls: +pref.dlg.lbl.Temperature = Temperatur: +pref.dlg.lbl.Momentofinertia = Trägheitsmoment: +pref.dlg.lbl.Pressure = Druck: +pref.dlg.lbl.Stability = Stabilität: +pref.dlg.lbl.FlightTime = Flight time: +pref.dlg.lbl.effect1 = Die Änderungen werden wirksam, wenn Sie das nächste Mal ein Fenster öffnen. +pref.dlg.lbl.Checkingupdates = Prüfe, ob Aktualisierungen verfügbar sind... +pref.dlg.lbl.msg1 = Ein Fehler trat bei der Kommunikation mit dem Server auf. +pref.dlg.lbl.msg2 = Es konnten keine Informationen über Programmaktualisierungen empfangen werden. +pref.dlg.lbl.msg3 = Sie benutzen die neueste Version von OpenRocket. +pref.dlg.lbl.msg4 = Keine Aktualisierungen verfügbar. +pref.dlg.PrefChoiseSelector1 = Immer fragen +pref.dlg.PrefChoiseSelector2 = in der Mitte einfügen +pref.dlg.PrefChoiseSelector3 = an das Ende anhängen +pref.dlg.PrefBooleanSelector1 = Löschen +pref.dlg.PrefBooleanSelector2 = Bestätigen +pref.dlg.Add = Hinzufügen +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. + +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 = Simulation starten +simedtdlg.but.resettodefault = Auf Standardeinstellungen zurücksetzen +simedtdlg.but.add = Hinzufügen +simedtdlg.but.remove = Entfernen +simedtdlg.title.Editsim = Simulation bearbeiten +simedtdlg.lbl.Simname = Name der Simulation: +simedtdlg.tab.Launchcond = Startbedingungen +simedtdlg.tab.Simopt = Simulationsoptionen +simedtdlg.tab.Plotdata = Daten plotten +simedtdlg.tab.Exportdata = Daten exportieren +simedtdlg.lbl.Motorcfg = Motorkonfiguration: +simedtdlg.lbl.ttip.Motorcfg = Motorkonfiguration auswählen +simedtdlg.combo.ttip.motorconf = Die Motorkonfiguration auswählen. +simedtdlg.lbl.Wind = Wind +simedtdlg.lbl.Averwindspeed = Durchschnittliche Windgeschwindigkeit: +simedtdlg.lbl.ttip.Averwindspeed = Die durchschnittliche Windgeschwindigkeit relativ zum Boden. +simedtdlg.lbl.Stddeviation = Standardabweichung +simedtdlg.lbl.ttip.Stddeviation = Die Standardabweichung der Windgeschwindigkeit.
Die Windgeschwindigkeit liegt im Durchschnitt zu 95% der Zeit in der doppelten Standardabweichung. +simedtdlg.lbl.Turbulenceintensity = Intensität der Turbulenz: +simedtdlg.lbl.ttip.Turbulenceintensity1 = Die Intensität der Turbulenz ist die Standardabweichung geteilt durch durch die durchschnittliche Windgeschwindigkeit.
+simedtdlg.lbl.ttip.Turbulenceintensity2 = Typischer Wertebereich von +simedtdlg.lbl.ttip.Turbulenceintensity3 = bis +simedtdlg.border.Atmoscond = Atmosphärische Bedingungen +simedtdlg.checkbox.InterStdAtmosphere = Internationale Standardatmosphäre benutzen +simedtdlg.checkbox.ttip.InterStdAtmosphere1 = Auswählen, um das Modell der Internationalen Standardatmosphäre zu verwenden.
In diesem Modell gilt eine Temperatur von +simedtdlg.checkbox.ttip.InterStdAtmosphere2 = und ein Luftdruck von +simedtdlg.checkbox.ttip.InterStdAtmosphere3 = auf Meeresniveau. +simedtdlg.lbl.Temperature = Temperatur: +simedtdlg.lbl.ttip.Temperature = Die Temperatur am Startplatz. +simedtdlg.lbl.Pressure = Luftdruck: +simedtdlg.lbl.ttip.Pressure = Der Luftdruck am Startplatz. +simedtdlg.lbl.Launchsite = Startplatz +simedtdlg.lbl.Latitude = Breitengrad: +simedtdlg.lbl.ttip.Latitude = Der Breitengrad des Startplatzes beeinflusst die wirksame Gravitationskraft.
Positive Werte liegen auf der Nordhalbkugel, negative Werte auf der Südhalbkugel. + +simedtdlg.lbl.Longitude = Longitude: +simedtdlg.lbl.ttip.Longitude = Required for weather prediction and elevation models. + +simedtdlg.lbl.Altitude = Höhe: +simedtdlg.lbl.ttip.Altitude = Die Höhe des Startplatzes über Meeresniveau.
Die Höhe des Startplatzes beeinflusst die Position der Rakete im atmosphärischen Modell. +simedtdlg.border.Launchrod = Startrampe +simedtdlg.lbl.Length = Länge: +simedtdlg.lbl.ttip.Length = Die Länge der Startrampe +simedtdlg.lbl.Angle = Winkel: +simedtdlg.lbl.ttip.Angle = Der Winkel der Startrampe aus der Vertikalen. +simedtdlg.lbl.Direction = Richtung: +simedtdlg.lbl.ttip.Direction1 = Richtung der Startrampe relativ zur Windrichtung
+simedtdlg.lbl.ttip.Direction2 = = gegen den Wind. +simedtdlg.lbl.ttip.Direction3 = = mit dem Wind +simedtdlg.border.Simopt = Simulationsoptionen +simedtdlg.lbl.Calcmethod = Berechnungsmethode +simedtdlg.lbl.ttip.Calcmethod = Die erweiterte Methode nach Barrowman berechnet die aerodynamischen Kräfte
nach den Gleichungen von Barrowman, die um weitere Faktoren erweitert wurden. +simedtdlg.lbl.ExtBarrowman = Barrowman (erweitert) +simedtdlg.lbl.Simmethod = Simulationsmethode: +simedtdlg.lbl.ttip.Simmethod1 = Der Sechs-Freiheitsgradsimulator erlaubt der Rakete völlige Bewegungsfreiheit während des Fluges.
+simedtdlg.lbl.ttip.Simmethod2 = Das Integrieren wird nach dem numerischen Runge-Kutta-Verfahren 4. Ordnung durchgeführt. +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 = Zeitschritt: +simedtdlg.lbl.ttip.Timestep1 = Die Zeit zwischen den Simulationsschritten.
Kleinere Schritte ergeben genauere Ergebnisse, die Simulationen dauern aber länger.
+simedtdlg.lbl.ttip.Timestep2 = Die Berechnung der Simulation mit dem Verfahren 4. Ordnung liefert gute Ergebnisse mit Zeitschritten von +simedtdlg.but.ttip.resettodefault = Zeitschritte zurücksetzen auf den Standardwert ( +simedtdlg.border.Simlist = Simulationsempfänger +simedtdlg.txt.longA1 = Simulationsempfänger sind ein fortgeschrittenes Feature, dass es benutzerdefinierten Programmen erlaubt, die Simulationsdaten zu empfangen und mit der Simulation zu interagieren. +simedtdlg.txt.longA2 = Mehr Information zum Schreiben von Simualtionsempfängern sind in der OpenRocket technical documentation zu finden. +simedtdlg.lbl.Curlist = Aktuelle Simulationsempfänger: +simedtdlg.lbl.Addsimlist = Simulationsempfänger hinzufügen +simedtdlg.lbl.Noflightdata = Keine Flugdaten verfügbar. +simedtdlg.lbl.runsimfirst = Bitte erst die Simulation ausführen. +simedtdlg.chart.Simflight = Simulierter Flug +simedtdlg.dlg.Simres = Ergebnisse der Simulation +simedtdlg.IntensityDesc.None = Keine +simedtdlg.IntensityDesc.Verylow = Sehr niedrig +simedtdlg.IntensityDesc.Low = Niedrig +simedtdlg.IntensityDesc.Medium = Mittel +simedtdlg.IntensityDesc.High = Hoch +simedtdlg.IntensityDesc.Veryhigh = Sehr hoch +simedtdlg.IntensityDesc.Extreme = Extrem + +GeodeticComputationStrategy.none.name = None +GeodeticComputationStrategy.none.desc = Perform no geodetic computations. +GeodeticComputationStrategy.spherical.name = Spherical approximation +GeodeticComputationStrategy.spherical.desc = Perform geodetic computations assuming a spherical Earth.
This is sufficiently accurate for almost all purposes. +GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid +GeodeticComputationStrategy.wgs84.desc = Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.
Slower and unnecessary in most cases. + + + + +! Simulation Panel +simpanel.but.newsimulation = Neue Simulation +simpanel.but.editsimulation = Simulation bearbeiten +simpanel.but.runsimulations = Simulation ausführen +simpanel.but.deletesimulations = Simulation löschen +simpanel.but.plotexport = Plotten / exportieren +simpanel.but.ttip.newsimulation = Neue Simulation hinzufügen +simpanel.but.ttip.editsim = Ausgewählte Simulation bearbeiten +simpanel.but.ttip.runsimu = Neuberechnen der ausgewählten Simulationen +simpanel.but.ttip.deletesim = Ausgewählte Simulationen löschen +simpanel.checkbox.donotask = Nicht wieder fragen +simpanel.lbl.defpref = Die Standardaktion kann in den Einstellungen geändert werden. +simpanel.dlg.lbl.DeleteSim1 = Die ausgewählten Simulationen löschen? +simpanel.dlg.lbl.DeleteSim2 = Diese Aktion kann nicht rückgängig gemacht werden. +simpanel.dlg.lbl.DeleteSim3 = Simulationen löschen +simpanel.col.Name = Name der Simulation: +simpanel.col.Motors = Motoren +simpanel.col.Apogee = Apogäum +simpanel.col.Maxvelocity = max. Geschwindigkeit +simpanel.col.Maxacceleration = max. Beschleunigung +simpanel.col.Timetoapogee = Zeit bis zum Apogäum +simpanel.col.Flighttime = Flugzeit +simpanel.col.Groundhitvelocity = Landegeschwindigkeit + +! SimulationRunDialog +SimuRunDlg.title.RunSim = Simuliere... +SimuRunDlg.lbl.Running = Arbeite... +SimuRunDlg.lbl.Simutime = Simulationsdauer: +SimuRunDlg.lbl.Altitude = Höhe: +SimuRunDlg.lbl.Velocity = Geschwindigkeit: +SimuRunDlg.msg.Unabletosim = Simulieren nicht möglich: +SimuRunDlg.msg.errorOccurred = Während der Simulation trat ein Fehler auf: +SimuRunDlg.msg.AnException1 = Während der Simulation trat eine Ausnahme auf: +SimuRunDlg.msg.AnException2 = Bitte berichten Sie diesen Fehler mit den unten stehenden Details. +SimuRunDlg.msg.AssertionError1 = Während der Simulation trat ein Berechnungsfehler auf: +SimuRunDlg.msg.AssertionError2 = Bitte berichten Sie diesen Fehler mit den unten stehenden Details. +SimuRunDlg.msg.unknownerror1 = Während der Simulation trat ein unbekannter Fehler auf: +SimuRunDlg.msg.unknownerror2 = Das Programm könnte instabil sein, speichern Sie Ihr Design und starten Sie OpenRocket neu! + + + +! SimulationExportPanel +SimExpPan.desc = Komma getrennte Werte (*.csv) +SimExpPan.border.Vartoexport = zu exportierende Variablen +SimExpPan.but.Selectall = Alle auswählen +SimExpPan.but.Selectnone = Keine auswählen +SimExpPan.border.Fieldsep = Feldtrennung +SimExpPan.lbl.Fieldsepstr = Trennzeichen +SimExpPan.lbl.longA1 = Das Trennzeichen wird benutzt, um die Felder in der exportierten Datei voneinander zu trennen.
+SimExpPan.lbl.longA2 = Für eine CSV-Datei (Comma Separated Values) ein ',' benutzen. +SimExpPan.checkbox.Includesimudesc = Simulationsbeschreibung einfügen +SimExpPan.checkbox.ttip.Includesimudesc = Fügt einen Kommentar mit einer Simulationsbeschreibung am Anfang der Datei ein. +SimExpPan.border.Comments = Kommentare +SimExpPan.checkbox.Includefielddesc = Feldbeschreibungen einfügen +SimExpPan.checkbox.ttip.Includefielddesc = Fügt eine Kommentarzeile mit der Beschreibung der exportierten Variablen ein. +SimExpPan.checkbox.Incflightevents = Flugereignisse einfügen +SimExpPan.checkbox.ttip.Incflightevents = Fügt eine Kommentarzeile für jedes Flugereignis ein. +SimExpPan.lbl.Commentchar = Kommentarzeichen: +SimExpPan.lbl.ttip.Commentchar = Zeichen, das einen Kommentar in der exportierten Datei kennzeichnet. +SimExpPan.but.Exporttofile = In Datei exportieren... +SimExpPan.Fileexists.desc1 = File \"",Datei \«" +SimExpPan.Fileexists.desc2 = \" existiert bereits. Überschreiben?" +SimExpPan.Fileexists.title = Datei existiert bereits +SimExpPan.ExportingVar.desc1 = Exportiere Variable 1 aus +SimExpPan.ExportingVar.desc2 = Exportiere +SimExpPan.ExportingVar.desc3 = Variablen aus +SimExpPan.Col.Variable = Variable +SimExpPan.Col.Unit = Einheit + + +CsvOptionPanel.separator.space = SPACE +CsvOptionPanel.separator.tab = TAB + + + +! MotorPlot +MotorPlot.title.Motorplot = Motorkurve +MotorPlot.but.Select = Auswahl +MotorPlot.Chart.Motorthrustcurve = Motorschubkurve +MotorPlot.Chart.Time = Zeit / s +MotorPlot.Chart.Thrust = Schub / N +MotorPlot.txt.Designation = Bezeichnung: +MotorPlot.txt.Manufacturer = Hersteller +MotorPlot.txt.Type = Typ: +MotorPlot.txt.Delays = Verzögerungen: +MotorPlot.txt.Comment = Kommentare:\n + + + +! Simulation plot panel +simplotpanel.lbl.Presetplotconf = Plotparameter setzen +simplotpanel.lbl.Xaxistype = X-Achse: +simplotpanel.lbl.Unit = Einheit: +simplotpanel.lbl.Yaxistypes = Y-Achse: +simplotpanel.lbl.Flightevents = Flugereignisse: +simplotpanel.but.All = Alle auswählen +simplotpanel.but.None = Keine +simplotpanel.but.NewYaxisplottype = Neuer Y-Achsenplot-Typ +simplotpanel.but.Plotflight = Flug plotten +simplotpanel.lbl.Axis = Achsen: +simplotpanel.but.ttip.Removethisplot = Diesen Plot löschen +simplotpanel.Desc = Die Daten werden in zeitlicher Reihenfolge geplottet, auch wenn der X-Achsen-Typ nicht Zeit ist. +simplotpanel.OptionPane.lbl1 = Es sind maximal 15 Plots erlaubt. +simplotpanel.OptionPane.lbl2 = Plot konnte nicht hinzugefügt werden +simplotpanel.AUTO_NAME = Auto +simplotpanel.LEFT_NAME = Links +simplotpanel.RIGHT_NAME = Rechts +simplotpanel.CUSTOM = Benutzerdefiniert + +! Component add buttons +compaddbuttons.Bodycompandfinsets = Körperteile und Leitwerke +compaddbuttons.Nosecone = Spitze +compaddbuttons.Bodytube = Körperrohr +compaddbuttons.Transition = Übergang +compaddbuttons.Trapezoidal = Trapeziod +compaddbuttons.Elliptical = Elliptisch +compaddbuttons.Freeform = Freiform +compaddbuttons.Launchlug = Leit-\nröhrchen +compaddbuttons.Innercomponent = Innenteile +compaddbuttons.Innertube = Innenrohr +compaddbuttons.Coupler = Koppler +compaddbuttons.Centeringring = Zentrier-\nring +compaddbuttons.Bulkhead = Schott +compaddbuttons.Engineblock = Motor-\nblock +compaddbuttons.Massobjects = Massenobjekte +compaddbuttons.Parachute = Fallschirm +compaddbuttons.Streamer = Strömer +compaddbuttons.Shockcord = Gummiband +compaddbuttons.Masscomponent = Massen-\nobjekt +compaddbuttons.Donotaskmeagain = Nicht wieder fragen +compaddbuttons.Selectcomppos = Komponentenposition auswählen +compaddbuttons.lbl.Youcanchange = Die Standardaktion kann in den Einstellungen geändert werden. +compaddbuttons.lbl.insertcomp = Die Komponente nach der aktuellen Komponente oder als letzte Komponente einfügen? +compaddbuttons.askPosition.Inserthere = Hier einfügen +compaddbuttons.askPosition.Addtotheend = Zum Ende hinzufügen +compaddbuttons.askPosition.Cancel = Abbrechen + +! Component Analysis Dialog +componentanalysisdlg.componentanalysis = Component analysis +componentanalysisdlg.lbl.winddir = Windrichtung +componentanalysisdlg.TitledBorder.warnings = Warnungen: +componentanalysisdlg.ToggleBut.worst = Worst +componentanalysisdlg.lbl.angleofattack = Angriffswinkel: +componentanalysisdlg.lbl.machnumber = Machzahl: +componentanalysisdlg.lbl.rollrate = Rollrate: +componentanalysisdlg.lbl.activestages = Aktive Stufen: +componentanalysisdlg.lbl.motorconf = Motorkonfiguration: +componentanalysisdlg.TabStability.Col = Komponente +componentanalysisdlg.TabStability = Stabilität +componentanalysisdlg.TabStability.ttip = Stabilitätsinformationen +componentanalysisdlg.dragTableModel.Col.Component = Komponente +componentanalysisdlg.dragTableModel.Col.Pressure = Druck CD +componentanalysisdlg.dragTableModel.Col.Base = Base CD +componentanalysisdlg.dragTableModel.Col.friction = Reibung CD +componentanalysisdlg.dragTableModel.Col.total = Gesamt CD +componentanalysisdlg.dragTabchar = Luftwiderstand +componentanalysisdlg.dragTabchar.ttip = Luftwiderstands-Eigenschaften +componentanalysisdlg.rollTableModel.Col.component = Komponente +componentanalysisdlg.rollTableModel.Col.rollforc = Roll forcing coefficient +componentanalysisdlg.rollTableModel.Col.rolldamp = Roll damping coefficient +componentanalysisdlg.rollTableModel.Col.total = Gesamt Cl +componentanalysisdlg.rollTableModel = Rolldynamik +componentanalysisdlg.rollTableModel.ttip = Rolldynamik +componentanalysisdlg.println.closingmethod = Closing method called: +componentanalysisdlg.println.settingnam = SETTING NAN VALUES +componentanalysisdlg.lbl.reflenght = Referenzlänge: +componentanalysisdlg.lbl.refarea = Referenzfläche: +!componentanalysisdlg.But.close =Close +componentanalysisdlg.TabStability.Col.Component = Component + +! Custom Material dialog +custmatdlg.title.Custommaterial = Benutzerdefiniertes Material +custmatdlg.lbl.Materialname = Name des Materials: +custmatdlg.lbl.Materialtype = Materialtyp +custmatdlg.lbl.Materialdensity = Materialdichte: +custmatdlg.checkbox.Addmaterial = Material zur Datenbank hinzufügen + + +! Ring Component Config +ringcompcfg.OuterRadius = Äußerer Radius +ringcompcfg.Automatic = Automatisch +ringcompcfg.InnerRadius = Innerer Radius +ringcompcfg.Thickness = Wandstärke +ringcompcfg.Length = Länge +ringcompcfg.Positionrelativeto = Relative Position zu: +ringcompcfg.plus = plus +ringcompcfg.PositionValue = Positionswert +ringcompcfg.Radialdistance = Radialer Abstand: +ringcompcfg.Distancefrom = Abstand von der Raketenmittellinie +ringcompcfg.Radialdirection = Radiale Richtung +ringcompcfg.radialdirectionfrom = Die radiale Richtung von der Raketenmittellinie +ringcompcfg.but.Reset = Zurücksetzen +ringcompcfg.but.Resetcomponant = Komponente auf die Raketenmittellinie zurücksetzen +ringcompcfg.EngineBlock.desc = Eine Motorhalterung verhindert, dass der Motor sich im Rohr nach vorne bewegt.

Um einen Motor hinzuzufügen, ein Körperrohr oder ein Innenrohr hinzufügen und im Reiter Motor als Motorhalterung markieren. +ringcompcfg.note.desc = Hinweis: Innenrohre beeinflussen die Aerodynamik der Rakete nicht, auch wenn sie außerhalb des Körperohres liegen. + + +! Body Tube Config +BodyTubecfg.lbl.Bodytubelength = Länge des Körperrohres: +BodyTubecfg.lbl.Outerdiameter = Außendurchmesser: +BodyTubecfg.lbl.Innerdiameter = Innendurchmesser: +BodyTubecfg.lbl.Wallthickness = Wandstärke: +BodyTubecfg.tab.General = Allgemein +BodyTubecfg.tab.Generalproperties = Allgemeine Eigenschaften +BodyTubecfg.tab.Motor = Motor +BodyTubecfg.tab.Motormountconf = Motorkonfiguration +BodyTubecfg.checkbox.Automatic = Automatisch +BodyTubecfg.checkbox.Filled = Gefüllt + +! FinSetConfig +FinSetConfig.tab.Fintabs = Leitwerke +FinSetConfig.tab.Through-the-wall = Durchsteckbare Leitwerke +FinSetConfig.but.Converttofreeform = In Freiform konvertieren +FinSetConfig.but.Converttofreeform.ttip = Konvertiert diese Leitwerke in eine Freiform +FinSetConfig.Convertfinset = Leitwerke konvertieren +FinSetConfig.but.Splitfins = Geteilte Leitwerke +FinSetConfig.but.Splitfins.ttip = Teilt den Leitwerkssatz in getrennte Leitwerke +FinSetConfig.lbl.Through-the-wall = Durchsteckbare Leitwerke: +FinSetConfig.lbl.Tablength = Länge: +FinSetConfig.ttip.Tablength = Länge des Leitwerks. +FinSetConfig.lbl.Tabheight = Höhe: +FinSetConfig.ttip.Tabheight = Spannweite des Leitwerks. +FinSetConfig.lbl.Tabposition = Position: +FinSetConfig.ttip.Tabposition = Position des Leitwerks. +FinSetConfig.lbl.relativeto = relativ zu + +! MotorDatabaseLoadingDialog +MotorDbLoadDlg.title = Lade Motoren +MotorDbLoadDlg.Loadingmotors = Lade Motoren... + +! RocketConfig +RocketCfg.lbl.Designname = Name der Rakete: +RocketCfg.lbl.Designer = Ersteller: +RocketCfg.lbl.Comments = Kommentare: +RocketCfg.lbl.Revisionhistory = Versionsgeschichte: +RocketCfg.lbl.Material = Material: + +! ShockCordConfig +ShockCordCfg.lbl.Shockcordlength = Gummibandlänge + +! RocketComponentConfig +RocketCompCfg.lbl.Componentname = Komponentenname: +RocketCompCfg.ttip.Thecomponentname = Name der Komponente. +RocketCompCfg.tab.Override = Werte überschreiben +RocketCompCfg.tab.MassandCGoverride = Massen- und Schwerpunktsoptionen +RocketCompCfg.tab.Figure = Form +RocketCompCfg.tab.Figstyleopt = Formoptionen +RocketCompCfg.tab.Comment = Kommentar +RocketCompCfg.tab.Specifyacomment = Kommentar zu dieser Komponente +RocketCompCfg.lbl.Mass = Masse: +RocketCompCfg.lbl.Componentmass = Masse der Komponente: +RocketCompCfg.lbl.overriddento = (überschrieben auf +RocketCompCfg.lbl.overriddenby = (überschrieben durch +RocketCompCfg.lbl.Componentmaterial = Material: +RocketCompCfg.lbl.Componentfinish = Oberfläche: +RocketCompCfg.lbl.ttip.componentmaterialaffects = Das Material beeinflusst die Masse der Komponente. +RocketCompCfg.combo.ttip.componentmaterialaffects = Das Material beeinflusst die Masse der Komponente. +RocketCompCfg.lbl.longA1 = Die Oberfläche beeinflusst den aerodynamischen Widerstand der Komponente.
+RocketCompCfg.lbl.longA2 = Der angegebene Wert ist die durchschnittliche Rautiefe der Oberfläche. +RocketCompCfg.but.Setforall = Für alle setzen +RocketCompCfg.but.ttip.Setforall = Diese Oberflächen für alle Komponenten der Rakete setzen. +RocketCompCfg.lbl.Overridemassorcenter = Überschreiben von Masse oder Schwerpunkts von +RocketCompCfg.checkbox.Overridemass = Masse überschreiben: +RocketCompCfg.checkbox.Overridecenterofgrav = Schwerpunkt überschreiben: +RocketCompCfg.checkbox.OverridemassandCG = Masse und Schwerpunkt für alle Unterkomponenten überschreiben +RocketCompCfg.lbl.longB1 = Die überschriebene Masse enthält keine Motoren.
+RocketCompCfg.lbl.longB2 = Die Messung des Schwerpunktes beginnt am Ende von +RocketCompCfg.lbl.Commentsonthe = Kommentare zu +RocketCompCfg.lbl.Figurestyle = Form: +RocketCompCfg.lbl.Componentcolor = Farbe: +RocketCompCfg.lbl.Choosecolor = Farbe auswählen +RocketCompCfg.checkbox.Usedefaultcolor = Standardfarbe verwenden +RocketCompCfg.lbl.Complinestyle = Linienstil: +RocketCompCfg.but.Saveasdefstyle = Als Standardstil speichern +RocketCompCfg.lbl.Diameter = Durchmesser: +RocketCompCfg.lbl.Length = Länge: +RocketCompCfg.lbl.Thickness = Wandstärke: +RocketCompCfg.checkbox.Endcapped = Verschlossenes Ende +RocketCompCfg.ttip.Endcapped = Gibt an, ob das Ende der Schulter geschlossen ist. +RocketCompCfg.title.Noseconeshoulder = Spitzenschulter +RocketCompCfg.title.Aftshoulder = Schulter hinten +RocketCompCfg.border.Foreshoulder = Schulter vorn +!RocketCompCfg.lbl.Length = Length: + +! BulkheadConfig +BulkheadCfg.tab.Radius = Radius: +BulkheadCfg.tab.Thickness = Wandstärke: +BulkheadCfg.tab.General = Allgemein +BulkheadCfg.tab.Generalproperties = Allgemeine Eigenschaften + +!CenteringRingConfig +CenteringRingCfg.tab.Outerdiam = Außendurchmesser: +CenteringRingCfg.tab.Innerdiam = Innendurchmesser: +CenteringRingCfg.tab.Thickness = Wandstärke: +CenteringRingCfg.tab.General = Allgemein +CenteringRingCfg.tab.Generalproperties = Allgemeine Eigenschaften + +!ComponentConfigDialog +ComponentCfgDlg.configuration = Konfiguration +ComponentCfgDlg.configuration1 = +ComponentCfgDlg.Modify = Verändern + +!EllipticalFinSetConfig +EllipticalFinSetCfg.Nbroffins = Anzahl der Leitwerke +EllipticalFinSetCfg.Rotation = Rotation: +EllipticalFinSetCfg.Fincant = Neigung: +EllipticalFinSetCfg.Rootchord = Blatttiefe: +EllipticalFinSetCfg.Height = Höhe: +EllipticalFinSetCfg.Positionrelativeto = Position relativ zu: +EllipticalFinSetCfg.plus = plus +EllipticalFinSetCfg.FincrossSection = Querschnitt: +EllipticalFinSetCfg.Thickness = Wandstärke: +EllipticalFinSetCfg.General = Allgemein +EllipticalFinSetCfg.Generalproperties = Allgemeine Eigenschaften +EllipticalFinSetCfg.ttip.Fincant = Der Winkel, in dem die Leitwerke zum Körperrohr geneigt sind. + +!FreeformFinSetConfig +FreeformFinSetCfg.tab.General = Allgemein +FreeformFinSetCfg.tab.ttip.General = Allgemeine Eigenschaften +FreeformFinSetCfg.tab.Shape = Form +FreeformFinSetCfg.tab.ttip.Finshape = Leitwerksform +FreeformFinSetCfg.lbl.Numberoffins = Anzahl der Leitwerke +FreeformFinSetCfg.lbl.Finrotation = Rotation: +FreeformFinSetCfg.lbl.Fincant = Neigung: +FreeformFinSetCfg.lbl.ttip.Fincant = Der Winkel, in dem die Leitwerke zum Körperrohr geneigt sind. +FreeformFinSetCfg.lbl.Posrelativeto = Position relativ zu: +FreeformFinSetCfg.lbl.plus = plus +FreeformFinSetCfg.lbl.FincrossSection = Querschnitt: +FreeformFinSetCfg.lbl.Thickness = Wandstärke: +! 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 = Motorkonfiguration +InnerTubeCfg.tab.Cluster = Cluster +InnerTubeCfg.tab.ttip.Cluster = Cluster-Konfiguration +InnerTubeCfg.tab.Radialpos = Radiale Position +InnerTubeCfg.tab.ttip.Radialpos = Radiale Position +InnerTubeCfg.lbl.Selectclustercfg = Cluster-Konfiguration auswählen: +InnerTubeCfg.lbl.TubeSep = Rohrtrennung +InnerTubeCfg.lbl.ttip.TubeSep = Die Trennung der Rohre, 1.0 = die Rohre berühren sich +InnerTubeCfg.lbl.Rotation = Rotation: +InnerTubeCfg.lbl.ttip.Rotation = Rotationswinkel der Cluster-Konfiguration +InnerTubeCfg.lbl.Rotangle = Rotationswinkel der Cluster-Konfiguration +InnerTubeCfg.but.Splitcluster = Cluster aufteilen +InnerTubeCfg.lbl.longA1 = Den Cluster in einzelne Komponenten aufteilen.
+InnerTubeCfg.lbl.longA2 = Die dupliziert alle Komponenten innerhalb dieses Innenrohrs. +InnerTubeCfg.but.Resetsettings = Einstellungen zurücksetzen +InnerTubeCfg.but.ttip.Resetsettings = Setzt die Aufteilung und Rotation auf die Standardwerte zurück + +! LaunchLugConfig +LaunchLugCfg.lbl.Length = Länge: +LaunchLugCfg.lbl.Outerdiam = Außendurchmesser: +LaunchLugCfg.lbl.Innerdiam = Innendurchmesser: +LaunchLugCfg.lbl.Thickness = Wandstärke: +LaunchLugCfg.lbl.Radialpos = Radiale Position: +LaunchLugCfg.lbl.Posrelativeto = Position relativ zu: +LaunchLugCfg.lbl.plus = plus +LaunchLugCfg.tab.General = Allgemein +LaunchLugCfg.tab.Generalprop = Allgemeine Eigenschaften + +! MassComponentConfig +MassComponentCfg.lbl.Mass = Masse +MassComponentCfg.lbl.Length = Länge +MassComponentCfg.lbl.Diameter = Durchmesser +MassComponentCfg.lbl.PosRelativeto = Position relativ zu: +MassComponentCfg.lbl.plus = plus +MassComponentCfg.tab.General = Allgemein +MassComponentCfg.tab.ttip.General = Allgemeine Eigenschaften +MassComponentCfg.tab.Radialpos = Radiale Position +MassComponentCfg.tab.ttip.Radialpos = Konfiguration der radialen Position +MassComponentCfg.lbl.Radialdistance = Radialer Abstand: +MassComponentCfg.lbl.Radialdirection = radiale Richtung: +MassComponentCfg.but.Reset = Zurücksetzen + +! MotorConfig +MotorCfg.checkbox.compmotormount = Diese Komponente ist eine Motorhalterung +MotorCfg.lbl.Motorcfg = Motorkonfiguration +MotorCfg.but.New = Neu +MotorCfg.lbl.Currentmotor = Aktueller Motor: +MotorCfg.lbl.Motoroverhang = Motorüberstand: +MotorCfg.lbl.Ignitionat = Zündung bei: +MotorCfg.lbl.plus = plus +MotorCfg.lbl.seconds = Sekunden +MotorCfg.lbl.longA1 = Das aktuelle Design hat im Moment nur eine Stufe. +MotorCfg.lbl.longA2 = Stufen können durch Klicken auf \«Neue Stufe\« hinzugefügt werden. +MotorCfg.lbl.longB1 = Das aktuelle Design hat im Moment nur eine Stufe. +MotorCfg.lbl.longB2 = Stufen. +MotorCfg.but.Selectmotor = Motor auswählen +MotorCfg.but.Removemotor = Motor entfernen +MotorCfg.lbl.motorLabel = Keiner + +! NoseConeConfig +NoseConeCfg.lbl.Noseconeshape = Spitzenform: +NoseConeCfg.lbl.Shapeparam = Formparameter: +NoseConeCfg.lbl.Noseconelength = Spitzenlänge: +NoseConeCfg.lbl.Basediam = Basisdurchmesser: +NoseConeCfg.checkbox.Automatic = Automatisch +NoseConeCfg.lbl.Wallthickness = Wandstärke: +NoseConeCfg.checkbox.Filled = gefüllt +NoseConeCfg.tab.General = Allgemein +NoseConeCfg.tab.ttip.General = Allgemeine Eigenschaften +NoseConeCfg.tab.Shoulder = Schulter +NoseConeCfg.tab.ttip.Shoulder = Schultereigenschaften + +! ParachuteConfig +ParachuteCfg.lbl.Canopy = Fallschirmkappe: +ParachuteCfg.lbl.Diameter = Durchmesser: +ParachuteCfg.lbl.Material = Material: +ParachuteCfg.combo.MaterialModel = Das Material beeinflusst die Masse der Komponente. +ParachuteCfg.lbl.longA1 = Luftwiderstandskoeffizient CD: +ParachuteCfg.lbl.longB1 = Der Luftwiderstandsbeiwert relativ zur Gesamtfläche des Fallschirms.
+ParachuteCfg.lbl.longB2 = Ein größerer Luftwiderstand führt zu einer kleineren Sinkrate. +ParachuteCfg.lbl.longB3 = Ein typischer Wert für Fallschirme ist 0,8. +ParachuteCfg.but.Reset = Zurücksetzen +ParachuteCfg.lbl.Shroudlines = Fangleinen: +ParachuteCfg.lbl.Numberoflines = Anzahl der Leinen: +ParachuteCfg.lbl.Linelength = Länge der Leinen: +ParachuteCfg.lbl.Material = Material: +ParachuteCfg.lbl.Posrelativeto = Position relativ zu: +ParachuteCfg.lbl.plus = plus +ParachuteCfg.lbl.Packedlength = gepackte Länge: +ParachuteCfg.lbl.Packeddiam = gepackter Durchmesser: +ParachuteCfg.lbl.Deploysat = Auswurf bei +ParachuteCfg.lbl.seconds = Sekunden +ParachuteCfg.lbl.Altitude = Höhe: +ParachuteCfg.tab.General = Allgemein +ParachuteCfg.tab.ttip.General = Allgemeine Eigenschaften +ParachuteCfg.tab.Radialpos = Radiale Position +ParachuteCfg.tab.ttip.Radialpos = Konfiguration der radialen Position +ParachuteCfg.lbl.Radialdistance = Radialer Abstand: +ParachuteCfg.lbl.Radialdirection = radiale Richtung: +ParachuteCfg.but.Reset = Zurücksetzen +ParachuteCfg.lbl.plusdelay = plus + +! ShockCordConfig +ShockCordCfg.lbl.Shockcordlength = Länge des Gummibands +ShockCordCfg.lbl.Shockcordmaterial = Material des Gummibands: +ShockCordCfg.lbl.Posrelativeto = Position relativ zu: +ShockCordCfg.lbl.plus = plus +ShockCordCfg.lbl.Packedlength = gepackte Länge: +ShockCordCfg.lbl.Packeddiam = gepackter Durchmesser: +ShockCordCfg.tab.General = Allgemein +ShockCordCfg.tab.ttip.General = Allgemeine Eigenschaften + +!SleeveConfig +SleeveCfg.tab.Outerdiam = Außendurchmesser: +SleeveCfg.tab.Innerdiam = Innendurchmesser: +SleeveCfg.tab.Wallthickness = Wandstärke: +SleeveCfg.tab.Length = Länge: +SleeveCfg.tab.General = Allgemein +SleeveCfg.tab.Generalproperties = Allgemeine Eigenschaften + +! StreamerConfig +StreamerCfg.lbl.Striplength = Länge des Strömers: +StreamerCfg.lbl.Stripwidth = Breite des Strömers: +StreamerCfg.lbl.Striparea = Fläche des Strömers: +StreamerCfg.lbl.Aspectratio = Seitenverhältnis: +StreamerCfg.lbl.Material = Material: +StreamerCfg.combo.ttip.MaterialModel = Das Material beeinflusst die Masse der Komponente. +StreamerCfg.lbl.longA1 = Widerstandskoeffizient CD: +StreamerCfg.lbl.longB1 = Der Widerstandskoeffizient des Strömers hängt von der Gesamtfläche ab.
+StreamerCfg.lbl.longB2 = Ein größerer Luftwiderstandskoeffizient führt zu einer kleineren Sinkrate. +StreamerCfg.lbl.Automatic = Automatisch +StreamerCfg.lbl.longC1 = Der Luftwiderstandskoeffizient hängt von der Fläche des Strömers ab. +StreamerCfg.lbl.Posrelativeto = Position relativ zu: +StreamerCfg.lbl.plus = plus +StreamerCfg.lbl.Packedlength = gepackte Länge: +StreamerCfg.lbl.Packeddiam = gepackter Durchmesser: +StreamerCfg.lbl.Deploysat = Auswurf bei +StreamerCfg.lbl.seconds = Sekunden +StreamerCfg.lbl.Altitude = Höhe: +StreamerCfg.tab.General = Allgemein +StreamerCfg.tab.ttip.General = Allgemeine Eigenschaften +StreamerCfg.tab.Radialpos = Radiale Position +StreamerCfg.tab.ttip.Radialpos = Konfiguration der radialen Position +StreamerCfg.lbl.Radialdistance = Radialer Abstand: +StreamerCfg.lbl.Radialdirection = radiale Richtung: +StreamerCfg.but.Reset = Zurücksetzen +StreamerCfg.lbl.plusdelay = plus + +! ThicknessRingComponentConfig +ThicknessRingCompCfg.tab.Outerdiam = Außendurchmesser: +ThicknessRingCompCfg.tab.Innerdiam = Innendurchmesser: +ThicknessRingCompCfg.tab.Wallthickness = Wandstärke: +ThicknessRingCompCfg.tab.Length = Länge: +ThicknessRingCompCfg.tab.General = Allgemein +ThicknessRingCompCfg.tab.Generalprop = Allgemeine Eigenschaften + +! TransitionConfig +TransitionCfg.lbl.Transitionshape = Form des Übergangs +TransitionCfg.checkbox.Clipped = geklemmt +TransitionCfg.lbl.Shapeparam = Formparameter: +TransitionCfg.lbl.Transitionlength = Länge des Übergangs: +TransitionCfg.lbl.Forediam = Vorderer Durchmesser +TransitionCfg.checkbox.Automatic = Automatisch +TransitionCfg.lbl.Aftdiam = Hinterer Durchmesser +TransitionCfg.lbl.Wallthickness = Wandstärke: +TransitionCfg.checkbox.Filled = gefüllt +TransitionCfg.tab.General = Allgemein +TransitionCfg.tab.Generalproperties = Allgemeine Eigenschaften +TransitionCfg.tab.Shoulder = Schulter +TransitionCfg.tab.Shoulderproperties = Schultereigenschaften + +! TrapezoidFinSetConfig +TrapezoidFinSetCfg.lbl.Nbroffins = Anzahl der Leitwerke +TrapezoidFinSetCfg.lbl.ttip.Nbroffins = Anzahl der Leitwerke in diesem Satz +TrapezoidFinSetCfg.lbl.Finrotation = Rotation der Leitwerke +TrapezoidFinSetCfg.lbl.ttip.Finrotation = Winkel des ersten Leitwerks in diesem Satz +TrapezoidFinSetCfg.lbl.Fincant = Neigung: +TrapezoidFinSetCfg.lbl.ttip.Fincant = Der Winkel, in dem die Leitwerke zum Körperrohr geneigt sind. +TrapezoidFinSetCfg.lbl.Rootchord = Blatttiefe: +TrapezoidFinSetCfg.lbl.Tipchord = Blatttiefe (Spitze) +TrapezoidFinSetCfg.lbl.Height = Höhe: +TrapezoidFinSetCfg.lbl.Sweeplength = Blattbreite: +TrapezoidFinSetCfg.lbl.Sweepangle = Pfeilungswinkel +TrapezoidFinSetCfg.lbl.FincrossSection = Leitwerksquerschnitt +TrapezoidFinSetCfg.lbl.Thickness = Wandstärke: +TrapezoidFinSetCfg.lbl.Posrelativeto = Position relativ zu: +TrapezoidFinSetCfg.lbl.plus = plus +TrapezoidFinSetCfg.tab.General = Allgemein +TrapezoidFinSetCfg.tab.Generalproperties = Allgemeine Eigenschaften + +!MotorConfigurationModel +MotorCfgModel.Editcfg = Konfiguration bearbeiten + +! StorageOptionChooser +StorageOptChooser.lbl.Simdatatostore = Zu speichernde Simulationsdaten: +StorageOptChooser.rdbut.Allsimdata = Alle Simulationsdaten +StorageOptChooser.lbl.longA1 = Speichert alle Simulationsdaten.
+StorageOptChooser.lbl.longA2 = Dies kann sehr große Dateien erzeugen! +StorageOptChooser.rdbut.Every = Alle Simulationsdaten +StorageOptChooser.lbl.longB1 = Speicher plotbare Daten in etwa diesem Abstand.
+StorageOptChooser.lbl.longB2 = Größere Werte erzeugen kleinere Dateien. +StorageOptChooser.lbl.seconds = Sekunden +StorageOptChooser.rdbut.Onlyprimfig = Nur die wichtigsten Werte +StorageOptChooser.lbl.longC1 = Speichert nur die Werte, die in der Zusammenfassung stehen.
+StorageOptChooser.lbl.longC2 = Dies ergibt die kleinsten Dateien +StorageOptChooser.checkbox.Compfile = Datei komprimieren +StorageOptChooser.lbl.UsingComp = Kompression der Datei verringert die Größe signifikant. +StorageOptChooser.lbl.longD1 = Eine Schätzung der Dateigröße mit den gegebenen Optionen. +StorageOptChooser.ttip.Saveopt = Speicheroptionen +StorageOptChooser.lbl.Estfilesize = Voraussichtliche Dateigröße: +StorageOptChooser.lbl.Saveopt = Speicheroptionen + +! ThrustCurveMotorSelectionPanel +TCMotorSelPan.lbl.Selrocketmotor = Raketenmotor auswählen: +TCMotorSelPan.checkbox.hideSimilar = Ähnliche Schubkurven verbergen +TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Alle Motoren anzeigen +TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Motoren anzeigen, deren Durchmesser kleiner als der der Motorhalterung ist +TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Motoren anzeigen, deren Durchmesser gleich der der Motorhalterung ist +TCMotorSelPan.lbl.Motormountdia = Durchmesser der Motorhalterung +TCMotorSelPan.lbl.Search = Suchen: +TCMotorSelPan.lbl.Selectthrustcurve = Schubkurve auswählen: +TCMotorSelPan.lbl.Ejectionchargedelay = Verzögerung der Ausstoßladung: +TCMotorSelPan.equalsIgnoreCase.None = keine +TCMotorSelPan.lbl.NumberofsecondsorNone = (Anzahl der Sekunden oder \«keine\«) +TCMotorSelPan.lbl.Totalimpulse = Gesamtimpuls: +TCMotorSelPan.lbl.Avgthrust = Durchschn. Schub: +TCMotorSelPan.lbl.Maxthrust = max. Schub +TCMotorSelPan.lbl.Burntime = Brenndauer: +TCMotorSelPan.lbl.Launchmass = Startmasse: +TCMotorSelPan.lbl.Emptymass = Leermasse: +TCMotorSelPan.lbl.Datapoints = Datenpunkte: +TCMotorSelPan.lbl.Digest = Übersicht: +TCMotorSelPan.title.Thrustcurve = Schubkurve: +TCMotorSelPan.title.Thrust = Schub: +TCMotorSelPan.delayBox.None = keine + + +! PlotDialog +PlotDialog.title.Flightdataplot = Flugdatenplot +PlotDialog.Chart.Simulatedflight = Simulierter Flug +PlotDialog.CheckBox.Showdatapoints = Datenpunkte anzeigen +PlotDialog.lbl.Chart = Klicken+ziehen: runter+rechts um hinein zu zoomen, hoch+links um heraus zu zoomen + + +! "main" prefix is used for the main application dialog + +# FIXME: Rename the description keys + +main.menu.file = Datei +main.menu.file.desc = File-handling related tasks +main.menu.file.new = Neu +main.menu.file.new.desc = Create a new rocket design +main.menu.file.open = Öffnen.. +BasicFrame.item.Openrocketdesign = Raketendesign öffnen +main.menu.file.openExample = Beispiel öffnen.. +BasicFrame.item.Openexamplerocketdesign = Beispieldesign öffnen +main.menu.file.save = Speichern +BasicFrame.item.SavecurRocketdesign = Aktuelles Raketendesign speichern +main.menu.file.saveAs = Speichern unter... +BasicFrame.item.SavecurRocketdesnewfile = Aktuelles Raketendesign in eine neue Datei speichern +main.menu.file.print = Drucken / als PDF exportieren... +BasicFrame.item.Printpart = Komponentenliste und Leitwerkschablone drucken +main.menu.file.close = Schließen +BasicFrame.item.Closedesign = Aktuelles Raketendesign schließen +main.menu.file.quit = Beenden +BasicFrame.item.Quitprogram = Programm beenden + +main.menu.edit = Bearbeiten +BasicFrame.menu.Rocketedt = Rakete bearbeiten +main.menu.edit.undo = Rückgängig +main.menu.edit.undo.desc = Undo the previous operation +main.menu.edit.redo = Wiederholen +main.menu.edit.redo.desc = Redo the previously undone operation +main.menu.edit.cut = Ausschneiden +main.menu.edit.copy = Kopieren +main.menu.edit.paste = Einfügen +main.menu.edit.delete = Löschen +main.menu.edit.resize = Scale... +main.menu.edit.resize.desc = Scale parts of the rocket design +main.menu.edit.preferences = Einstellungen +main.menu.edit.preferences.desc = Setup the application preferences + +main.menu.analyze = Analysieren +main.menu.analyze.desc = Rocket analysis +main.menu.analyze.componentAnalysis = Komponente analysieren +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 = Hilfe +main.menu.help.desc = Information about OpenRocket +main.menu.help.license = Lizenz +main.menu.help.license.desc = OpenRocket license information +main.menu.help.bugReport = Fehlerbericht +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 = Über +main.menu.help.about.desc = Copyright details about OpenRocket + +main.menu.debug = Debug +main.menu.debug.whatisthismenu = Was macht diese Menü? +main.menu.debug.createtestrocket = Eine Testrakete erstellen + +! database +! Translate here all material database +! + +! Material database +! BULK_MATERIAL +Databases.materials.Acrylic = Acryl +Databases.materials.Balsa = Balsa +Databases.materials.Birch = Birke +Databases.materials.Cardboard = Karton +Databases.materials.Carbonfiber = Kohlefaser +Databases.materials.Cork = Kork +Databases.materials.DepronXPS = Depron (XPS) +Databases.materials.Fiberglass = Glasfaser +Databases.materials.Kraftphenolic = Pertinax +Databases.materials.Maple = Ahorn +Databases.materials.Paperoffice = Papier (Büro) +Databases.materials.Pine = Kiefer +Databases.materials.Plywoodbirch = Sperrholz (Birke) +Databases.materials.PolycarbonateLexan = Polycarbonat (Lexan) +Databases.materials.Polystyrene = Polystyrène +Databases.materials.PVC = PVC +Databases.materials.Spruce = Fichte +Databases.materials.StyrofoamgenericEPS = Styropor (EPS) +Databases.materials.StyrofoamBluefoamXPS = Styrodur (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 = Polyethylen (dünn) +Databases.materials.Polyethyleneheavy = Polyethylen (schwer) +Databases.materials.Silk = Seide +Databases.materials.Paperoffice = Papier (Büro) +Databases.materials.Cellophane = Zellophan +Databases.materials.Crepepaper = Krepppapier +! LINE_MATERIAL +Databases.materials.Threadheavy-duty = Faden (stark) +Databases.materials.Elasticcordround2mm = Elastikband (rund, 2mm, 1/16 in) +Databases.materials.Elasticcordflat6mm = Elastikband (flach, 6mm, 1/4 in) +Databases.materials.Elasticcordflat12mm = Elastikband (flach, 12mm, 1/2 in) +Databases.materials.Elasticcordflat19mm = Elastikband (flach, 19mm, 3/4 in) +Databases.materials.Elasticcordflat25mm = Elastikband (flach, 25mm, 1 in) +Databases.materials.Braidednylon2mm = Nylonflachband (2 mm, 1/16 in) +Databases.materials.Braidednylon3mm = Nylonflachband (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 = Rau +ExternalComponent.Unfinished = unbehandelt +ExternalComponent.Regularpaint = normale Farbe +ExternalComponent.Smoothpaint = glatte Farbe +ExternalComponent.Polished = poliert + +! LineStyle +LineStyle.Solid = durchgehend +LineStyle.Dashed = gestrichelt +LineStyle.Dotted = gepunktet +LineStyle.Dash-dotted = Strich-Punkt +LineStyle.Defaultstyle = Standardstil + +! Shape +Shape.Conical = Konisch +Shape.Conical.desc1 = Eine konische Spitze hat ein dreieckiges Profil +Shape.Conical.desc2 = Ein konischer Übergang hat gerade Kanten +Shape.Ogive = Ogive +Shape.Ogive.desc1 = Eine ogive Spitze hat das Profil eines Kreissegments. Der Formparamter 1 erzeugt eine tangentiale Ogive, die einen weichen Übergang zum Körperrohr hat, Werte kleiner 1 erzeugen eine sekante Ogive. +Shape.Ogive.desc2 = Eine ogive Spitze hat das Profil eines Kreissegments. Der Formparamter 1 erzeugt eine tangentiale Ogive, die einen weichen Übergang zum Körperrohr am hinteren Ende hat, Werte kleiner 1 erzeugen eine sekante Ogive. +Shape.Ellipsoid = Ellipsoid +Shape.Ellipsoid.desc1 = Eine ellipsoide Spitze hat ein Profil einer Halbellipse mit der einer Hauptachsenlänge von 2×Länge und Durchmesser +Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×Length and Diameter. 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 Radius × (x / Length)k where k is the shape parameter. For k=0.5 this is a \u00BD-power or parabolic nose cone, for k=0.75 a \u00BE-power, and for k=1 a conical nose cone. +Shape.Powerseries.desc2 = A power series transition has a profile of Radius × (x / Length)k where k is the shape parameter. For k=0.5 the transition is \u00BD-power or parabolic, for k=0.75 a \u00BE-power, and for k=1 conical. +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 full parabola which is tangent to the body tube, 0.75 produces a 3/4 parabola, 0.5 procudes a 1/2 parabola and 0 produces a conical 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 full parabola which is tangent to the body tube at the aft end, 0.75 produces a 3/4 parabola, 0.5 procudes a 1/2 parabola and 0 produces a conical transition. +Shape.Haackseries = Haack series +Shape.Haackseries.desc1 = The Haack series nose cones are designed to minimize drag. The shape parameter 0 produces an LD-Haack or Von Karman nose cone, which minimizes drag for fixed length and diameter, while a value of 0.333 produces an LV-Haack nose cone, which minimizes drag for fixed length and volume. +Shape.Haackseries.desc2 = The Haack series nose cones 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 LD-Haack or Von Karman shape, while a value of 0.333 produces an LV-Haack shape. + + +! RocketComponent +RocketComponent.Position.TOP = oberes Ende der übergeordneten Komponente +RocketComponent.Position.MIDDLE = Mitte der übergeordneten Komponente +RocketComponent.Position.BOTTOM = unteres Ende der übergeordneten Komponente +RocketComponent.Position.AFTER = nach der übergeordneten Komponente +RocketComponent.Position.ABSOLUTE = zur Spitze + +! LaunchLug +LaunchLug.Launchlug = Leitröhrchen +! NoseCone +NoseCone.NoseCone = Spitze +! Transition +Transition.Transition = Übergang +!Stage +Stage.Stage = Stufe +! BodyTube +BodyTube.BodyTube = Körperrohr +! TubeCoupler +TubeCoupler.TubeCoupler = Koppler +!InnerTube +InnerTube.InnerTube = Innenrohr +! TrapezoidFinSet +TrapezoidFinSet.TrapezoidFinSet = Trapezoide Leitwerke +! FreeformFinSet +FreeformFinSet.FreeformFinSet = Frei geformte Leitwerke +!MassComponent +MassComponent.MassComponent = Masse +! Parachute +Parachute.Parachute = Fallschirm +! ShockCord +ShockCord.ShockCord = Gummiband +! Bulkhead +Bulkhead.Bulkhead = Schott + +!Rocket +Rocket.motorCount.Nomotor = [Keine Motoren] +Rocket.compname.Rocket = Rakete + +!MotorMount +MotorMount.IgnitionEvent.AUTOMATIC = Automatisch (Start oder Ausstoßladung) +MotorMount.IgnitionEvent.LAUNCH = Start +MotorMount.IgnitionEvent.EJECTION_CHARGE = Erste Ausstoßladung der vorherigen Stufe +MotorMount.IgnitionEvent.BURNOUT = Erster Brennschluss der vorherigen Stufe +MotorMount.IgnitionEvent.NEVER = Nie + +!ComponentIcons +ComponentIcons.Nosecone = Spitze +ComponentIcons.Bodytube = Körperrohr +ComponentIcons.Transition = Übergang +ComponentIcons.Trapezoidalfinset = Trapezoide Leitwerke +ComponentIcons.Ellipticalfinset = Elliptische Leitwerke +ComponentIcons.Freeformfinset = Frei geformte Leitwerke +ComponentIcons.Launchlug = Leitröhrchen +ComponentIcons.Innertube = Innenrohr +ComponentIcons.Tubecoupler = Koppler +ComponentIcons.Centeringring = Zentrierring +ComponentIcons.Bulkhead = Schott +ComponentIcons.Engineblock = Motorhalterung +ComponentIcons.Parachute = Fallschirm +ComponentIcons.Streamer = Strömer +ComponentIcons.Shockcord = Gummiband +ComponentIcons.Masscomponent = Masse +ComponentIcons.disabled = (deaktiviert) + +! StageAction +StageAction.Stage = Stufe + +! RecoveryDevice +RecoveryDevice.DeployEvent.LAUNCH = Start (plus NN Sekunden) +RecoveryDevice.DeployEvent.EJECTION = Erste Ausstoßladung dieser Stufe +RecoveryDevice.DeployEvent.APOGEE = Apogäum +RecoveryDevice.DeployEvent.ALTITUDE = Spezifische Höhe während der Landephase +RecoveryDevice.DeployEvent.NEVER = Nie + +! FlightEvent +FlightEvent.Type.LAUNCH = Start +FlightEvent.Type.IGNITION = Motorzündung +FlightEvent.Type.LIFTOFF = Abheben +FlightEvent.Type.LAUNCHROD = Verlassen der Startrampe +FlightEvent.Type.BURNOUT = Motorbrennschluss +FlightEvent.Type.EJECTION_CHARGE = Ausstoßladung +FlightEvent.Type.STAGE_SEPARATION = Stufentrennung +FlightEvent.Type.APOGEE = Apogäum +FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Auslösung des Bergungssystems +FlightEvent.Type.GROUND_HIT = Landung +FlightEvent.Type.SIMULATION_END = Ende der Simulation +FlightEvent.Type.ALTITUDE = Höhenänderung + +! ThrustCurveMotorColumns +TCurveMotorCol.MANUFACTURER = Hersteller +TCurveMotorCol.DESIGNATION = Bezeichnung +TCurveMotorCol.TYPE = Typ +TCurveMotorCol.DIAMETER = Durchmesser +TCurveMotorCol.LENGTH = Länge + +! RocketInfo +RocketInfo.lengthLine.Length = Länge +RocketInfo.lengthLine.maxdiameter = , max. Durchmesser +RocketInfo.massText1 = Masse mit Motoren +RocketInfo.massText2 = Masse ohne Motoren +RocketInfo.at = bei M= +RocketInfo.cgText = CG: +RocketInfo.cpText = CP: +RocketInfo.stabText = Stabilität: +RocketInfo.Warning = Warnung: +RocketInfo.Calculating = Berechne... +RocketInfo.Apogee = Apogäum: +RocketInfo.Maxvelocity = max. Geschwindigkeit: +RocketInfo.Maxacceleration = max. Beschleunigung: +RocketInfo.apogeeValue = N/A +RocketInfo.Mach = (Mach +RocketInfo.velocityValue = N/A +RocketInfo.accelerationValue = N/A + +! FinSet +FinSet.CrossSection.SQUARE = Quadrat +FinSet.CrossSection.ROUNDED = Abgerundet +FinSet.CrossSection.AIRFOIL = Tragfläche +FinSet.TabRelativePosition.FRONT = Root chord leading edge +FinSet.TabRelativePosition.CENTER = Root chord midpoint +FinSet.TabRelativePosition.END = Root chord trailing edge + +! FlightDataType +FlightDataType.TYPE_TIME = Zeit +FlightDataType.TYPE_ALTITUDE = Höhe +FlightDataType.TYPE_VELOCITY_Z = Vertikalgeschwindigkeit +FlightDataType.TYPE_ACCELERATION_Z = Vertikalbeschleunigung +FlightDataType.TYPE_VELOCITY_TOTAL = Gesamtgeschwindigkeit +FlightDataType.TYPE_ACCELERATION_TOTAL = Gesamtbeschleunigung +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 = Angriffswinkel +FlightDataType.TYPE_ROLL_RATE = Rollrate +FlightDataType.TYPE_PITCH_RATE = Nickrate +FlightDataType.TYPE_YAW_RATE = Gierrate +FlightDataType.TYPE_MASS = Masse +FlightDataType.TYPE_LONGITUDINAL_INERTIA = Longitudinal moment of inertia +FlightDataType.TYPE_ROTATIONAL_INERTIA = Rotational moment of inertia +FlightDataType.TYPE_CP_LOCATION = Position vom CP +FlightDataType.TYPE_CG_LOCATION = Position vom CG +FlightDataType.TYPE_STABILITY = Stabilität in Kalibern +FlightDataType.TYPE_MACH_NUMBER = Machzahl +FlightDataType.TYPE_REYNOLDS_NUMBER = Reynoldszahl +FlightDataType.TYPE_THRUST_FORCE = Schub +FlightDataType.TYPE_DRAG_FORCE = Luftwiderstandskraft +FlightDataType.TYPE_DRAG_COEFF = Luftwiderstandskoeffizient +FlightDataType.TYPE_AXIAL_DRAG_COEFF = Axial drag coefficient +FlightDataType.TYPE_FRICTION_DRAG_COEFF = Reibungskoeffizient +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 = Referenzlänge +FlightDataType.TYPE_REFERENCE_AREA = Referenzfläche +FlightDataType.TYPE_ORIENTATION_THETA = Vertical orientation (zenith) +FlightDataType.TYPE_ORIENTATION_PHI = Lateral orientation (azimuth) +FlightDataType.TYPE_WIND_VELOCITY = Windgeschwindigkeit +FlightDataType.TYPE_AIR_TEMPERATURE = Lufttemperatur +FlightDataType.TYPE_AIR_PRESSURE = Luftdruck +FlightDataType.TYPE_SPEED_OF_SOUND = Schallgeschwindigkeit +FlightDataType.TYPE_TIME_STEP = Simulationsintervall +FlightDataType.TYPE_COMPUTATION_TIME = Berechnnungszeit +FlightDataType.TYPE_LATITUDE = Latitude +FlightDataType.TYPE_LONGITUDE = Longitude +FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration + +! PlotConfiguration +PlotConfiguration.Verticalmotion = Vertikale Bewegung über Zeit +PlotConfiguration.Totalmotion = Gesamte Bewegung über Zeit +PlotConfiguration.Flightside = Flight side profile +PlotConfiguration.Stability = Stabilität über Zeit +PlotConfiguration.Dragcoef = Drag coefficients vs. Mach number +PlotConfiguration.Rollcharacteristics = Roll characteristics +PlotConfiguration.Angleofattack = Angle of attack and orientation vs. time +PlotConfiguration.Simulationtime = Simulationszeitschritt und Berechnungszeit + +! Warning +Warning.LargeAOA.str1 = Large angle of attack encountered. +Warning.LargeAOA.str2 = Large angle of attack encountered ( +Warning.DISCONTINUITY = Unstetigkeit im Raketendurchmesser +Warning.THICK_FIN = Dicke Leitwerke können nicht präzise modelliert werden. +Warning.JAGGED_EDGED_FIN = Gezackte Ecken in Leitwerken können unpräzise Ergebnisse liefern. +Warning.LISTENERS_AFFECTED = Simulationsempfänger haben die Simulation beeinflusst. +Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Bergungssystem wurde ausgelöst während der Motor noch gebrannt hat. +Warning.FILE_INVALID_PARAMETER = Ignoriere ungültigen Parameter. + + +! 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.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! diff --git a/core/resources/l10n/messages_es.properties b/core/resources/l10n/messages_es.properties new file mode 100644 index 00000000..1fa041df --- /dev/null +++ b/core/resources/l10n/messages_es.properties @@ -0,0 +1,1534 @@ +# +# 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 = Esta operación no puede deshacerse. +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 = 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 = Si está conectado a Internet, haga Clik en Enviar informe de errores. +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 = Puede realizar un informe de errores escribiendo en el formulario de abajo y enviarlo.
También puede informar de los errores adjuntando el archivo de su proyecto por email. +bugreport.reportDialog.txt2 = Por favor incluya una breve descripción de lo que estaba haciendo cuando ocurrió el error. +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 = Porta motor: +edtmotorconfdlg.title.Editmotorconf = Mostrar las configuraciones de motor +edtmotorconfdlg.selectcomp = Seleccionar qué componentes tienen la función de porta motor: +edtmotorconfdlg.lbl.Motorconfig = Configuraciones del motor: +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 = Desviación estándar de la velocidad del viento.
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 = La intensidad de la turbulencia es la desviación estándar dividida por la velocidad media del viento.
+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 = Seleccionar para usar el modelo de la International Standard Atmosphere.
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 = La latitud del lugar de lanzamiento afecta la atracción terrestre.
Los valores positivos se dan en el hemisferio Norte, los negativos en el hemisferio Sur. + +simedtdlg.lbl.Longitude = Longitud: +simedtdlg.lbl.ttip.Longitude = Requerido para modelos de elevación y predicción meteorológica. + +simedtdlg.lbl.Altitude = Altitud: +simedtdlg.lbl.ttip.Altitude = Los valores por encima del nivel del mar
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 = Dirección de la varilla de lanzamiento relativa al viento.
+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 = El método Barrowman extendido considera las fuerzas aerodinámicas
que actúan sobre cuerpos cilíndricos en cohetes que vuelan con un
ángulo de ataque (AOA) superior a 10 grados. +simedtdlg.lbl.ExtBarrowman = Barrowman Extendido +simedtdlg.lbl.Simmethod = Método de simulación: +simedtdlg.lbl.ttip.Simmethod1 = El simulador de seis-grados-de-libertad permite al cohete una total libertad durante el vuelo.
+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 = Tiempo entre etapas de simulación.
Un tiempo mas corto de etapa origina una simulación mas exacta pero mas lenta.
+simedtdlg.lbl.ttip.Timestep2 = Con 4th 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 = Extensiones del simulador 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 = Al incluir las computaciones geodésicas se considera una Tierra esférica.
Este aspecto es bastante preciso en la mayoría de los proyectos. +GeodeticComputationStrategy.wgs84.name = Elipsoidal WGS84 +GeodeticComputationStrategy.wgs84.desc = Incluye las computaciones geodésicas sobre la referencia elipsoidal WGS84 utilizando el método de Vicenty.
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 = Esta operación no puede deshacerse. +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 = Caracter para separar campos en el documento exportado.
+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 = Presión CD +componentanalysisdlg.dragTableModel.Col.Base = Base CD +componentanalysisdlg.dragTableModel.Col.friction = Rozamiento CD +componentanalysisdlg.dragTableModel.Col.total = Total CD +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 = Total Cl +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 = Un retén de motor impide que el motor se desplace hacia delante, por dentro del tubo porta motor.

Para añadir un motor, cree un Cuerpo tubular o Tubo interior y desígnelo como porta motor en el casillero Motor. +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 = El acabado del componente afecta a su coeficiente de rozamiento.
+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 = En la masa especificada no se incluye la de los motores.
+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 = Separar los tubos del cluster para convertirlos en componentes internos independientes.
+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 = Coeficiente de arrastre CD: +ParachuteCfg.lbl.longB1 = Coeficiente de rozamiento relativo al área total del paracaídas.
+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 = Coeficiente de rozamiento CD: +StreamerCfg.lbl.longB1 = Coeficiente de rozamiento relativo al área total de la banderola.
+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 = Almacenar todos los datos simulados.
+StorageOptChooser.lbl.longA2 = puede generar archivos muy grandes +StorageOptChooser.rdbut.Every = Cada +StorageOptChooser.lbl.longB1 = Almacenar los valores de impresión de este apartado.
+StorageOptChooser.lbl.longB2 = Genera valores grandes en archivos más pequeños. +StorageOptChooser.lbl.seconds = Segundos +StorageOptChooser.rdbut.Onlyprimfig = Sólo figuras principales +StorageOptChooser.lbl.longC1 = Almacenar sólo los valores en la tabla resumen.
+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 Ojiva tangente, mientras que un valor inferior a 1 produce una Ojiva secante con un perfil más afilado. +Shape.Ogive.desc2 = Transición con perfil de arco de circunferencia. Un valor de forma igual a 1 produce una Transición tangente, mientras que un valor inferior a 1 produce una Transición secante con un perfil más afilado. +Shape.Ellipsoid = Elíptica +Shape.Ellipsoid.desc1 = Ojiva con perfil de media elipse. Por defecto, una elipse de longitud igual al triple de su diámetro. +Shape.Ellipsoid.desc2 = Transición con perfil de media elipse. Por defecto, una elipse de longitud igual al triple de su diámetro. +Shape.Powerseries = Serie potencial +Shape.Powerseries.desc1 = Ojiva cuyo perfil es una curva obtenida a partir de una función potencial f(x)k. Un valor de forma k=0.5 produce una ojiva con perfil de parábola, para k=0.75 se produce una ojiva con perfil potencial, y para k=1 se produce una ojiva con perfil recto u Ojiva cónica. +Shape.Powerseries.desc2 = Transición cuyo perfil es una curva obtenida a partir de una función potencial de Radio  =; (x / L)k donde k es el parámetro de forma. Para k=0.5 la transición es \u00BD-potencial o parabólica, para k=0.75 a \u00BE-potencia, y para k=1 cónica. +Shape.Parabolicseries = Serie parabólica +Shape.Parabolicseries.desc1 = Ojiva con perfil de arco de parábola. Un valor de forma igual a 1 produce una Ojiva tangente, un valor igual a 0.75 produce una parábola de 3/4, un valor igual a 0.5 produce una parábola de 1/2, y un valor igual a 0 produce un perfil recto u Ojiva cónica. +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 parábola de 3/4, un valor de 0.5 produce una parábola de 1/2, 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 Ojiva LD Haack u Ojiva Von Karman que minimiza el arrastre aerodinámico para una determinada longitud y diámetro de la base, mientras que un valor igual a 0.333 produce una Ojiva LV-Haack 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 LD-Haack o Von Karman, mientras que un valor de 0.333 produce una forma LV-Haack. + + +! 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! + diff --git a/core/resources/l10n/messages_fr.properties b/core/resources/l10n/messages_fr.properties new file mode 100644 index 00000000..c095ee74 --- /dev/null +++ b/core/resources/l10n/messages_fr.properties @@ -0,0 +1,1524 @@ + +# +# French base translation file +# Translated by Tripoli France +# 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_fr.properties + +! RocketActions +RocketActions.checkbox.Donotaskmeagain = Ne plus me demander +RocketActions.lbl.Youcanchangedefop = Vous pouvez changer le mode opératoire par defaut dans les préferences. +RocketActions.showConfirmDialog.lbl1 = Supprimer les simulations sélectionnées? +RocketActions.showConfirmDialog.lbl2 = Cette opération n'est pas réversible. +RocketActions.showConfirmDialog.title = Effacer les simulations +RocketActions.DelCompAct.Delete = Effacer +RocketActions.DelCompAct.ttip.Delete = Effacer la pièce sélectionnée. +RocketActions.DelSimuAct.Delete = Effacer +RocketActions.DelSimuAct.ttip.Delete = Effacer la simulation sélectionnée. +RocketActions.DelAct.Delete = Effacer +RocketActions.DelAct.ttip.Delete = Effacer la pièce ou la simulation sélectionnée. +RocketActions.CutAction.Cut = Couper +RocketActions.CutAction.ttip.Cut = Couper cette pièce ou simulation, l'ajouter au presse papier et l'enlever du projet +RocketActions.CopyAct.Copy = Copier +RocketActions.CopyAct.ttip.Copy = Copier les pièces (et les pièces liées) dans le presse papier. +RocketActions.PasteAct.Paste = Coller +RocketActions.PasteAct.ttip.Paste = Coller la pièce ou simulation présente dans le presse papier dans le projet. +RocketActions.EditAct.Edit = Modifier +RocketActions.EditAct.ttip.Edit = Modifier la pièce sélectionnée. +RocketActions.NewStageAct.Newstage = Nouvel étage +RocketActions.NewStageAct.ttip.Newstage = Ajouter un nouvel étage au projet. +RocketActions.ActBoosterstage = Etage Booster +RocketActions.MoveUpAct.Moveup = Monter +RocketActions.MoveUpAct.ttip.Moveup = Monter la pièce. +RocketActions.MoveDownAct.Movedown = Descendre +RocketActions.MoveDownAct.ttip.Movedown = Descendre la pièce. + +! RocketPanel +RocketPanel.FigTypeAct.Sideview = Vue de coté +RocketPanel.FigTypeAct.ttip.Sideview = Vue de coté +RocketPanel.FigTypeAct.Backview = Vue arrière +RocketPanel.FigTypeAct.ttip.Backview = Vue arrière +RocketPanel.lbl.Motorcfg = Configuration Moteur: +RocketPanel.lbl.infoMessage = Cliquer pour sélectionner    Shift+cliquer pour sélectionner plusieurs    Double-cliquer pour modifier    Click+déplacer pour déplacer + + +! BasicFrame +BasicFrame.SimpleFileFilter1 = Tous les fichiers fusée (*.ork; *.rkt) +BasicFrame.SimpleFileFilter2 = Fichiers OpenRocket (*.ork) +BasicFrame.SimpleFileFilter3 = Fichiers RockSim (*.rkt) +BasicFrame.tab.Rocketdesign = Projet fusée +BasicFrame.tab.Flightsim = Simulations de vol +BasicFrame.title.Addnewcomp = Ajouter une nouvelle pièce +BasicFrame.dlg.lbl1 = Le projet ' +BasicFrame.dlg.lbl2 = ' N'a pas été sauvegardé. +BasicFrame.dlg.lbl3 = Voulez vous le sauvegarder? +BasicFrame.dlg.title = Projet non sauvegardé +BasicFrame.StageName.Sustainer = Sustainer +BasicFrame.WarningDialog.txt1 = Les problèmes suivant sont survenus lors de l'ouverture de +BasicFrame.WarningDialog.txt2 = Certains éléments du projet n'ont peut être pas été chargé correctement. +BasicFrame.WarningDialog.title = Avertissement lors de l'ouverture du fichier + +! General error messages used in multiple contexts +error.fileExists.title = Le fichier existe déjà +error.fileExists.desc = Le fichier '{filename}' existe déjà. Voulez vous l'ecraser? + +error.writing.title = Erreur d'éciture du fichier +error.writing.desc = Une erreur est survenue lors de l'écriture dans le fichier: + +! Labels used in buttons of dialog windows +button.ok = OK +button.cancel = Annuler +button.close = Fermer + +! Common labels used in buttons of dialog windows +dlg.but.ok = Accepter +dlg.but.cancel = Annuler +dlg.but.close = Fermer + + +! General file type names +filetypes.pdf = fichier PDF + + +! 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 = Traduit en français par: +AboutDialog.lbl.translator = Tripoli France +AboutDialog.lbl.translatorWebsite = http://tripoli.france.free.fr/ +AboutDialog.lbl.translatorIcon = logoTripoliFrance.png + +! Print dialog +PrintDialog.title = Imprimer ou exporter +PrintDialog.but.previewAndPrint = Pré-visualiser et imprimer +PrintDialog.checkbox.showByStage = Montrer par étage +PrintDialog.lbl.selectElements = Choisir les éléments à inclure: +printdlg.but.saveaspdf = Sauvegarder en PDF +printdlg.but.preview = Prévisualisation +printdlg.but.settings = Configuration +PrintDialog.error.preview.title = Impossible d'ouvrir la prévisualisation +PrintDialog.error.preview.desc1 = Impossible d'ouvrir la prévisualisation PDF. +PrintDialog.error.preview.desc2 = S'il vous plait utilisez l'option "Sauvegarder en PDF" à la place. + + +!PrintSettingsDialog +PrintSettingsDialog.title = Configuration impression +PrintSettingsDialog.lbl.Templatefillcolor = Couleur de remplissage du modèle: +PrintSettingsDialog.lbl.Templatebordercolor = Couleur des bords du modèle: +PrintSettingsDialog.lbl.Papersize = Dimensions du papier: +PrintSettingsDialog.lbl.Paperorientation = Orientation du papier: +PrintSettingsDialog.but.Reset = Réinitialiser +PrintSettingsDialog.but.Close = Fermer + + +! Bug Report dialog +bugreport.dlg.title = Rapport d'erreurs +bugreport.dlg.but.Sendbugreport = Envoyer un rapport d'erreurs +bugreport.dlg.but.Sendbugreport.Ttip = Envoyer automatiquement un rapport d'erreurs aux développeurs d'OpenRocket +bugreport.dlg.successmsg1 = Rapport d'erreurs envoyé avec succès. +bugreport.dlg.successmsg2 = Merci d'avoir contribué à l'amélioration d'OpenRocket! +bugreport.dlg.successmsg3 = Rapport d'erreurs envoyé +bugreport.dlg.connectedInternet = Si vous êtes connecté sur Internet, vous pouvez tout simplement cliquer sur Envoyer un rapport d'erreurs. +bugreport.dlg.otherwise = Sinon envoyez le texte ci-dessous à l'adresse: +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. +bugreport.dlg.failedmsg1 = OpenRocket n'a pas réussi à envoyer le rapport d'erreur: +bugreport.dlg.failedmsg2 = S'il vous plait envoyez le rapport manuellement à +bugreport.dlg.failedmsg3 = Erreur d'envoi du rapport +bugreport.reportDialog.txt = Vous pouvez signaler une erreur avec OpenRocket en remplissant et en envoyant le message ci-dessous.
Vous pouvez également signaler des erreurs et inclure des pièces jointes sur le site web du projet. +bugreport.reportDialog.txt2 = S'il vous plait ajoutez une courte description de ce que vous faisiez lorsque l'erreur s'est produite. +bugreport.dlg.provideDescription = S'il vous plait veuillez fournir d'abord une description du bug. +bugreport.dlg.provideDescription.title = La description du bug est absente + + +! Debug log dialog +debuglogdlg.but.clear = Effacer +debuglogdlg.OpenRocketdebuglog = Fichier debug d'OpenRocket +debuglogdlg.Displayloglines = Afficher les numéros des lignes: +debuglogdlg.Follow = Suivre +debuglogdlg.col.Time = Heure +debuglogdlg.col.Level = Niveau +debuglogdlg.col.Location = Emplacement +debuglogdlg.col.Message = Message +debuglogdlg.lbl.Loglinenbr = Numéro de la ligne: +debuglogdlg.lbl.Time = Heure: +debuglogdlg.lbl.Level = Niveau: +debuglogdlg.lbl.Location = Emplacement: +debuglogdlg.lbl.Logmessage = Texte du message: +debuglogdlg.lbl.Stacktrace = Stack trace: + + +! Edit Motor configuration dialog +edtmotorconfdlg.but.removemotor = Enlever le moteur +edtmotorconfdlg.but.Selectmotor = Choisir le moteur +edtmotorconfdlg.but.Removeconfiguration = Supprimer la configuration +edtmotorconfdlg.but.Newconfiguration = Nouvelle configuration +edtmotorconfdlg.lbl.Motormounts = Portes moteur: +edtmotorconfdlg.title.Editmotorconf = Changer la configuration moteur +edtmotorconfdlg.selectcomp = Choisir les pièces utilisées par le porte moteur: +edtmotorconfdlg.lbl.Motorconfig = Configurations moteur: +edtmotorconfdlg.lbl.Configname = Nom de la configuration: +edtmotorconfdlg.lbl.Leavenamedefault = Laisser le champ vide par défaut. + +! Example design dialog +exdesigndlg.but.open = Ouvrir +exdesigndlg.lbl.Selectexample = Choisir l'exemple de projet à ouvrir: +exdesigndlg.lbl.Openexampledesign = Ouvrir un exemple de projet +exdesigndlg.lbl.Exampledesignsnotfound = Impossible de trouver les exemples de projets. +exdesigndlg.lbl.Examplesnotfound = Exemples non trouvés + + +! Material edit panel +matedtpan.but.new = Nouveau +matedtpan.but.edit = Editer +matedtpan.but.delete = Effacer +matedtpan.but.revertall = Revenir aux valeurs précédentes +matedtpan.col.Material = Matériaux +matedtpan.col.Type = Type +matedtpan.col.Density = Densité +matedtpan.col.but.ttip.New = Ajouter un nouveau matériau +matedtpan.title.Addcustmaterial = Ajouter un matériau personnalisé +matedtpan.but.ttip.edit = Modifier un matériau existant +matedtpan.title.Editmaterial = Modifier un matériau +matedtpan.title2.Editmaterial = Les matériaux prédéfinis ne peuvent pas être modifiés. +matedtpan.but.ttip.delete = Supprimer un matériau personnalisé +matedtpan.but.ttip.revertall = Supprimer tous les matériaux personnalisés +matedtpan.title.Deletealluser-defined = Effacer tous les matériaux personalisés? +matedtpan.title.Revertall = Revenir aux valeurs précédentes? +matedtpan.lbl.edtmaterials = Modifier les matériaux n'affectera pas les projets fusée existants. + +!MaterialModel +MaterialModel.title.Material = Matériau +MaterialModel.title.Defcustmat = Définir un matériau personnalisé + + +! Preference dialog +pref.dlg.but.add = Ajouter +pref.dlg.but.reset = Réinitialiser +pref.dlg.but.checknow = Vérifier maintenant +pref.dlg.but.defaultmetric = Système métrique +pref.dlg.but.defaultimperial = Système impérial +pref.dlg.title.Preferences = Préférences +pref.dlg.tab.Units = Unités +pref.dlg.tab.Defaultunits = Unités par défaut +pref.dlg.tab.Materials = Matériaux +pref.dlg.tab.Custommaterials = Matériaux personnalisés +pref.dlg.tab.Options = Options +pref.dlg.tab.Miscellaneousoptions = Autres options +pref.dlg.lbl.Positiontoinsert = Position pour insérer des composants internes: +pref.dlg.lbl.Confirmdeletion = Confirmer l'effacement des simulations: +pref.dlg.lbl.User-definedthrust = Courbes de poussée personnalisées: +pref.dlg.Allthrustcurvefiles = Tous les fichiers de courbes de poussée (*.eng; *.rse; *.zip; répertoires) +pref.dlg.RASPfiles = Fichiers moteur RASP (*.eng) +pref.dlg.RockSimfiles = Fichiers moteur RockSim (*.rse) +pref.dlg.ZIParchives = Archives ZIP (*.zip) +pref.dlg.checkbox.Checkupdates = Rechercher les mises à jour au démarrage +pref.dlg.ttip.Checkupdatesnow = Recherchez les mises à jour maintenant +pref.dlg.lbl.Selectprefunits = Choisissez vos unités favorites: +pref.dlg.lbl.Rocketdimensions = Dimensions de la fusée: +pref.dlg.lbl.Linedensity = Epaisseur des lignes: +pref.dlg.lbl.Motordimensions = Dimensions du moteur: +pref.dlg.lbl.Surfacedensity = Densité de la Surface: +pref.dlg.lbl.Distance = Distance: +pref.dlg.lbl.Bulkdensity = Densité apparente: +pref.dlg.lbl.Velocity = Vitesse: +pref.dlg.lbl.Surfaceroughness = Rugosité de la Surface: +pref.dlg.lbl.Acceleration = Accélération: +pref.dlg.lbl.Area = Surface: +pref.dlg.lbl.Mass = Masse: +pref.dlg.lbl.Angle = Angle: +pref.dlg.lbl.Force = Force: +pref.dlg.lbl.Rollrate = Taux de roulis: +pref.dlg.lbl.Totalimpulse = Impulsion totale: +pref.dlg.lbl.Temperature = Température: +pref.dlg.lbl.Momentofinertia = Moment d'inertie: +pref.dlg.lbl.Pressure = Pression: +pref.dlg.lbl.Stability = Stabilité: +pref.dlg.lbl.FlightTime = Durée du vol: +pref.dlg.lbl.effect1 = Les changements prendront effet la prochaine fois que vous ouvrirez une fenêtre. +pref.dlg.lbl.Checkingupdates = Recherche des mises à jour... +pref.dlg.lbl.msg1 = Une erreur est survenue durant la communication avec le serveur. +pref.dlg.lbl.msg2 = Incapable de récupérer les informations de mise à jour +pref.dlg.lbl.msg3 = Vous utilisez la dernière version d'OpenRocket. +pref.dlg.lbl.msg4 = Pas de mises à jour disponible +pref.dlg.PrefChoiseSelector1 = Toujours demander +pref.dlg.PrefChoiseSelector2 = Insérer au milieu +pref.dlg.PrefChoiseSelector3 = Ajouter à la fin +pref.dlg.PrefBooleanSelector1 = Supprimer +pref.dlg.PrefBooleanSelector2 = Confirmer +pref.dlg.Add = Ajouter +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. + +PreferencesDialog.lbl.language = Langue du programme: +PreferencesDialog.languages.default = Valeur système par défaut +PreferencesDialog.lbl.languageEffect = La langue sera changée après avoir redémarré OpenRocket. + +! Simulation edit dialog +simedtdlg.but.runsimulation = Lancer la simulation +simedtdlg.but.resettodefault = Restaurer les paramètres par défaut +simedtdlg.but.add = Ajouter +simedtdlg.but.remove = Enlever +simedtdlg.title.Editsim = Modifier la simulation +simedtdlg.lbl.Simname = Nom de la simulation: +simedtdlg.tab.Launchcond = Conditions de lancement +simedtdlg.tab.Simopt = Options de simulation +simedtdlg.tab.Plotdata = Tracer les données +simedtdlg.tab.Exportdata = Exporter les données +simedtdlg.lbl.Motorcfg = Configuration moteur: +simedtdlg.lbl.ttip.Motorcfg = Choisir la configuration moteur à utiliser. +simedtdlg.combo.ttip.motorconf = Choisir la configuration moteur à utiliser. +simedtdlg.lbl.Wind = Vent +simedtdlg.lbl.Averwindspeed = Vitesse moyenne du vent: +simedtdlg.lbl.ttip.Averwindspeed = Vitesse moyenne du vent par rapport au sol. +simedtdlg.lbl.Stddeviation = Dérive standard: +simedtdlg.lbl.ttip.Stddeviation = La dérive standard de la vitesse du vent.
La vitesse du vent est le double de l'écart-type de la moyenne dans 95% des cas. +simedtdlg.lbl.Turbulenceintensity = Intensité de la turbulence: +simedtdlg.lbl.ttip.Turbulenceintensity1 = L'intensité de la turbulence résulte de la division de la dérive par la vitesse moyenne de vent.
+simedtdlg.lbl.ttip.Turbulenceintensity2 = Les valeurs typiques vont de +simedtdlg.lbl.ttip.Turbulenceintensity3 = à +simedtdlg.border.Atmoscond = Conditions atmosphériques +simedtdlg.checkbox.InterStdAtmosphere = Utiliser les paramètres de l'Atmosphère Standard +simedtdlg.checkbox.ttip.InterStdAtmosphere1 = Sélectionner pour utiliser les paramètres de l'Atmosphère Standard.
Ce modèle à une température de +simedtdlg.checkbox.ttip.InterStdAtmosphere2 = et une pression de +simedtdlg.checkbox.ttip.InterStdAtmosphere3 = au niveau de la mer. +simedtdlg.lbl.Temperature = Température: +simedtdlg.lbl.ttip.Temperature = Température du site de lancement. +simedtdlg.lbl.Pressure = Pression: +simedtdlg.lbl.ttip.Pressure = Pression atmosphérique du site de lancement. +simedtdlg.lbl.Launchsite = Site de lancement +simedtdlg.lbl.Latitude = Latitude: +simedtdlg.lbl.ttip.Latitude = La latitude du site de lancement affecte l'attraction gravitationnelle de la Terre.
> Les valeurs positives sont dans l'hémisphère Nord, les valeurs négatives sur l'hémisphère Sud. + +simedtdlg.lbl.Longitude = Longitude: +simedtdlg.lbl.ttip.Longitude = Nécessaire pour les prédictions du temps and elevation models. + +simedtdlg.lbl.Altitude = Altitude: +simedtdlg.lbl.ttip.Altitude = Altitude du site de lancement par rapport au niveau de la mer.
Cela affecte la position de la fusée dans le modèle atmosphérique. +simedtdlg.border.Launchrod = Rampe de lancement +simedtdlg.lbl.Length = Longueur: +simedtdlg.lbl.ttip.Length = Longueur de la rampe. +simedtdlg.lbl.Angle = Angle: +simedtdlg.lbl.ttip.Angle = Angle de la rampe de lancement par rapport à la verticale. +simedtdlg.lbl.Direction = Direction: +simedtdlg.lbl.ttip.Direction1 = Direction de la rampe de lance par rapport au vent.
+simedtdlg.lbl.ttip.Direction2 = = Face au vent, +simedtdlg.lbl.ttip.Direction3 = = vent arrière. +simedtdlg.border.Simopt = Options de simulation +simedtdlg.lbl.Calcmethod = Méthode de calcul: +simedtdlg.lbl.ttip.Calcmethod = La méthode Barrowman étendue calcule les forces aérodynamique selon
les équations de Barrowman étendues pour arranger plus de pièces. +simedtdlg.lbl.ExtBarrowman = Barrowman étendu +simedtdlg.lbl.Simmethod = Méthode de Simulation: +simedtdlg.lbl.ttip.Simmethod1 = Le simulateur de six degrés de liberté permet la liberté totale de fusée en vol.
+simedtdlg.lbl.ttip.Simmethod2 = Integration is performed using a 4th order Runge-Kutta 4 numerical integration. +simedtdlg.lbl.GeodeticMethod = Calculs Geodetic: +simedtdlg.lbl.ttip.GeodeticMethodTip = Relate to the calculation of coordinates on the earth. This also enables coriolis effect computations. +simedtdlg.lbl.Timestep = Réglage du pas de temps: +simedtdlg.lbl.ttip.Timestep1 = Le temps entre les étapes de la simulation.
Avec un pas de temps plus petit la simulation est plus lente mais également plus précise.
+simedtdlg.lbl.ttip.Timestep2 = The 4th order simulation method is quite accurate with a time step of +simedtdlg.but.ttip.resettodefault = Réinitialiser le pas de temps à sa valeur par défaut ( +simedtdlg.border.Simlist = Auditeurs de simulation +simedtdlg.txt.longA1 = Les auditeurs de simulation sont une fonction avancé qui permet à l'utilisateur d'écrire du code pour suivre et interagir avec la simulation. +simedtdlg.txt.longA2 = Pour plus de détails sur les auditeurs de simulation, reférez vous à la documentation technique d'OpenRocket. +simedtdlg.lbl.Curlist = Auditeurs de simulation actuel: +simedtdlg.lbl.Addsimlist = Ajouter un "auditeur de simulation" +simedtdlg.lbl.Noflightdata = Aucune donnée de vol disponible. +simedtdlg.lbl.runsimfirst = S'il vous plait faites tourner la simulation d'abord. +simedtdlg.chart.Simflight = Vol simulé +simedtdlg.dlg.Simres = Résultats de la simulation +simedtdlg.IntensityDesc.None = Aucune +simedtdlg.IntensityDesc.Verylow = Très basse +simedtdlg.IntensityDesc.Low = Basse +simedtdlg.IntensityDesc.Medium = Moyenne +simedtdlg.IntensityDesc.High = Haute +simedtdlg.IntensityDesc.Veryhigh = Très haute +simedtdlg.IntensityDesc.Extreme = Extrême + +GeodeticComputationStrategy.none.name = Aucune +GeodeticComputationStrategy.none.desc = Ne pas faire de calculs geodetic. +GeodeticComputationStrategy.spherical.name = Approximation sphérique +GeodeticComputationStrategy.spherical.desc = Perform geodetic computations assuming a spherical Earth.
This is sufficiently accurate for almost all purposes. +GeodeticComputationStrategy.wgs84.name = ellipsoïde WGS84 +GeodeticComputationStrategy.wgs84.desc = Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.
Slower and unnecessary in most cases. + + + +! Simulation Panel +simpanel.but.newsimulation = Nouvelle simulation +simpanel.but.editsimulation = Modifier la simulation +simpanel.but.runsimulations = Lancer les simulations +simpanel.but.deletesimulations = Effacer les simulations +simpanel.but.plotexport = Tracer / exporter +simpanel.but.ttip.newsimulation = Ajouter une nouvelle simulation +simpanel.but.ttip.editsim = Modifier la simulation sélectionnée +simpanel.but.ttip.runsimu = Recommencer la simulation sélectionnée +simpanel.but.ttip.deletesim = Effacer les simulations sélectionnées +simpanel.checkbox.donotask = Ne plus me demander +simpanel.lbl.defpref = Vous pouvez changer le mode opératoire par défaut dans préférences. +simpanel.dlg.lbl.DeleteSim1 = Effacer les simulations sélectionnées? +simpanel.dlg.lbl.DeleteSim2 = Cette opération n'est pas réversible. +simpanel.dlg.lbl.DeleteSim3 = Effacer les simulations +simpanel.col.Name = Nom +simpanel.col.Motors = Moteurs +simpanel.col.Apogee = Apogée +simpanel.col.Maxvelocity = Vitesse Max. +simpanel.col.Maxacceleration = Accélération Max. +simpanel.col.Timetoapogee = Temps pour atteindre l'apogée +simpanel.col.Flighttime = Temps de vol +simpanel.col.Groundhitvelocity = Vitesse à l'atterrissage + +! SimulationRunDialog +SimuRunDlg.title.RunSim = Simulations en cour... +SimuRunDlg.lbl.Running = En cour ... +SimuRunDlg.lbl.Simutime = Temps de simulation: +SimuRunDlg.lbl.Altitude = Altitude: +SimuRunDlg.lbl.Velocity = Vitesse: +SimuRunDlg.msg.Unabletosim = Simulation impossible: +SimuRunDlg.msg.errorOccurred = Une erreur s'est produite durant la simulation: +SimuRunDlg.msg.AnException1 = Une exception s'est produite lors de la simulation: +SimuRunDlg.msg.AnException2 = S'il vous plaît faites un rapport d'erreurs avec les détails ci-dessous. +SimuRunDlg.msg.AssertionError1 = Une erreur de calcul s'est produite lors de la simulation. +SimuRunDlg.msg.AssertionError2 = S'il vous plaît faites un rapport d'erreurs avec les détails ci-dessous. +SimuRunDlg.msg.unknownerror1 = Une erreur inconnue s'est produite lors de la simulation. +SimuRunDlg.msg.unknownerror2 = Le programme peut être instable, vous devez enregistrer toutes vos créations et redémarrez OpenRocket maintenant! + + + +! SimulationExportPanel +SimExpPan.desc = Fichiers dont les données sont séparées par une virgule (*.csv) +SimExpPan.border.Vartoexport = Variables à exporter +SimExpPan.but.Selectall = Tout sélectionner +SimExpPan.but.Selectnone = Ne rien sélectionner +SimExpPan.border.Fieldsep = Séparateur de champ +SimExpPan.lbl.Fieldsepstr = Séparateur de champ: +SimExpPan.lbl.longA1 = La chaîne utilisée pour séparer les champs dans le fichier exporté.
+SimExpPan.lbl.longA2 = Utiliser ',' pour un fichier (CSV). +SimExpPan.checkbox.Includesimudesc = Inclure la description de la simulation +SimExpPan.checkbox.ttip.Includesimudesc = Inclure un commentaire au début du fichier pour décrire la simulation. +SimExpPan.border.Comments = Commentaires +SimExpPan.checkbox.Includefielddesc = Inclure les descriptions des champs +SimExpPan.checkbox.ttip.Includefielddesc = Inclure une ligne de commentaire avec la description des variables exportées. +SimExpPan.checkbox.Incflightevents = Inclure les événements de vol +SimExpPan.checkbox.ttip.Incflightevents = Inclure une ligne de commentaire pour chaque évènement de vol. +SimExpPan.lbl.Commentchar = Symbole pour les commentaires: +SimExpPan.lbl.ttip.Commentchar = Le symbole utilisé pour une ligne de commentaires. +SimExpPan.but.Exporttofile = Exporter dans un fichier... +SimExpPan.Fileexists.desc1 = Le fichier \" +SimExpPan.Fileexists.desc2 = \" existe déjà. Ecraser? +SimExpPan.Fileexists.title = Le fichier existe +SimExpPan.ExportingVar.desc1 = Exporter 1 variable sur un total de +SimExpPan.ExportingVar.desc2 = Exportation +SimExpPan.ExportingVar.desc3 = variable sur un total de +SimExpPan.Col.Variable = Variable +SimExpPan.Col.Unit = Unité + + +CsvOptionPanel.separator.space = SPACE +CsvOptionPanel.separator.tab = TAB + + + +! MotorPlot +MotorPlot.title.Motorplot = Courbe du moteur +MotorPlot.but.Select = Sélection +MotorPlot.Chart.Motorthrustcurve = Courbe de poussée moteur +MotorPlot.Chart.Time = Temps / s +MotorPlot.Chart.Thrust = Poussée / N +MotorPlot.txt.Designation = Désignation: +MotorPlot.txt.Manufacturer = Manufacturer: +MotorPlot.txt.Type = Type: +MotorPlot.txt.Delays = Retards: +MotorPlot.txt.Comment = Commentaires:\n + + + +! Simulation plot panel +simplotpanel.lbl.Presetplotconf = Prédéfinir les paramètres du tracé: +simplotpanel.lbl.Xaxistype = Axe des X: +simplotpanel.lbl.Unit = Unités: +simplotpanel.lbl.Yaxistypes = Axe des Y: +simplotpanel.lbl.Flightevents = Evénements du vol: +simplotpanel.but.All = Tous +simplotpanel.but.None = Aucun +simplotpanel.but.NewYaxisplottype = Nouveau type de tracé de l'axe Y +simplotpanel.but.Plotflight = Tracer le vol +simplotpanel.lbl.Axis = Axes: +simplotpanel.but.ttip.Removethisplot = Effacer le tracé +simplotpanel.Desc = Les données seront tracées en fonction du temps même si le type d'Axe des abscisses n'est pas le temps. +simplotpanel.OptionPane.lbl1 = Un maximum de 15 tracés est permis. +simplotpanel.OptionPane.lbl2 = Impossible d'ajouter le tracé +simplotpanel.AUTO_NAME = Auto +simplotpanel.LEFT_NAME = Gauche +simplotpanel.RIGHT_NAME = Droite +simplotpanel.CUSTOM = Personnalisé + +! Component add buttons +compaddbuttons.Bodycompandfinsets = Pièces du corps et ailerons +compaddbuttons.Nosecone = Cône +compaddbuttons.Bodytube = Tube du\ncorps +compaddbuttons.Transition = Transition +compaddbuttons.Trapezoidal = Trapézoïdale +compaddbuttons.Elliptical = Elliptique +compaddbuttons.Freeform = Forme libre +compaddbuttons.Launchlug = Tube de\nguidage +compaddbuttons.Innercomponent = Pièces internes +compaddbuttons.Innertube = Tube interne +compaddbuttons.Coupler = Coupleur +compaddbuttons.Centeringring = Anneau de\ncentrage +compaddbuttons.Bulkhead = Cloison +compaddbuttons.Engineblock = Bague de\nrétention\nmoteur +compaddbuttons.Massobjects = Pièces pleines +compaddbuttons.Parachute = Parachute +compaddbuttons.Streamer = Banderole +compaddbuttons.Shockcord = Cordon\namortisseur +compaddbuttons.Masscomponent = Poids +compaddbuttons.Donotaskmeagain = Ne plus me poser la question +compaddbuttons.Selectcomppos = Position de la pièce +compaddbuttons.lbl.Youcanchange = Vous pouvez modifier le fonctionnement par défaut dans les préférences. +compaddbuttons.lbl.insertcomp = Insérez la pièce après l'élément actuel ou en tant que dernier élément? +compaddbuttons.askPosition.Inserthere = Ajouter ici +compaddbuttons.askPosition.Addtotheend = Ajouter à la fin +compaddbuttons.askPosition.Cancel = Annuler + +! Component Analysis Dialog +componentanalysisdlg.componentanalysis = Analyse pièce +componentanalysisdlg.lbl.winddir = Direction du vent: +componentanalysisdlg.TitledBorder.warnings = Avertissements: +componentanalysisdlg.ToggleBut.worst = Pire +componentanalysisdlg.lbl.angleofattack = Angle d'attaque: +componentanalysisdlg.lbl.machnumber = Mach number: +componentanalysisdlg.lbl.rollrate = Taux de roulis: +componentanalysisdlg.lbl.activestages = Etages actifs: +componentanalysisdlg.lbl.motorconf = Configuration moteur: +componentanalysisdlg.TabStability.Col.Component = Pièce +componentanalysisdlg.TabStability = Stabilité +componentanalysisdlg.TabStability.ttip = Information de stabilité +componentanalysisdlg.dragTableModel.Col.Component = Pièce +componentanalysisdlg.dragTableModel.Col.Pressure = Pression CD +componentanalysisdlg.dragTableModel.Col.Base = Base CD +componentanalysisdlg.dragTableModel.Col.friction = Friction CD +componentanalysisdlg.dragTableModel.Col.total = Total CD +componentanalysisdlg.dragTabchar = Caractéristiques de traînée +componentanalysisdlg.dragTabchar.ttip = Caractéristiques de traînée +componentanalysisdlg.rollTableModel.Col.component = Pièce +componentanalysisdlg.rollTableModel.Col.rollforc = Coefficient de forçage de roulis +componentanalysisdlg.rollTableModel.Col.rolldamp = Coefficient amortisseur de roulis +componentanalysisdlg.rollTableModel.Col.total = Total Cl +componentanalysisdlg.rollTableModel = Dynamique du roulis +componentanalysisdlg.rollTableModel.ttip = Dynamique du roulis +componentanalysisdlg.println.closingmethod = Méthode de clôture appelée: +componentanalysisdlg.println.settingnam = SETTING NAN VALUES +componentanalysisdlg.lbl.reflenght = Longueur de référence: +componentanalysisdlg.lbl.refarea = Aire de référence: +!componentanalysisdlg.but.close =Fermer +componentanalysisdlg.TabStability.Col.Component = Pièce + +! Custom Material dialog +custmatdlg.title.Custommaterial = Matériau personnalisé +custmatdlg.lbl.Materialname = Nom du matériau: +custmatdlg.lbl.Materialtype = Type de matériau: +custmatdlg.lbl.Materialdensity = Densité du matériau: +custmatdlg.checkbox.Addmaterial = Ajouter la pièce dans la base de données + + +! Ring Component Config +ringcompcfg.OuterRadius = Diamètre extérieur +ringcompcfg.Automatic = Automatique +ringcompcfg.InnerRadius = Diamètre intérieur +ringcompcfg.Thickness = Epaisseur +ringcompcfg.Length = Longueur +ringcompcfg.Positionrelativeto = Position relative à: +ringcompcfg.plus = plus +!ringcompcfg.PositionValue = PositionValue +ringcompcfg.Radialdistance = Rayon: +ringcompcfg.Distancefrom = Distance de l'axe central de la fusée +ringcompcfg.Radialdirection = Azimut +ringcompcfg.radialdirectionfrom = Sens par rapport à l'axe central de la fusée +ringcompcfg.but.Reset = Réinitialisation +ringcompcfg.but.Resetcomponant = Réinitialiser la pièce à l'axe de la fusée +ringcompcfg.EngineBlock.desc = Un bloc moteur empêche le moteur de se déplacer vers l'avant dans le tube porte moteur.

Pour ajouter un moteur, créer un tube ou un tube interne et marquer le comme porte moteur dans l'onglet Moteur. +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. + + +! Body Tube Config +BodyTubecfg.lbl.Bodytubelength = Longueur du tube: +BodyTubecfg.lbl.Outerdiameter = Diamètre externe: +BodyTubecfg.lbl.Innerdiameter = Diamètre interne: +BodyTubecfg.lbl.Wallthickness = Epaisseur des parois: +BodyTubecfg.tab.General = Général +BodyTubecfg.tab.Generalproperties = Propriétés générales +BodyTubecfg.tab.Motor = Moteur +BodyTubecfg.tab.Motormountconf = Configuration du porte moteur +BodyTubecfg.checkbox.Automatic = Automatique +BodyTubecfg.checkbox.Filled = Aspérités bouchées + +! FinSetConfig +FinSetConfig.tab.Fintabs = Pattes des ailerons +FinSetConfig.tab.Through-the-wall = Ailerons traversant le fuselage +FinSetConfig.but.Converttofreeform = Convertir en forme libre +FinSetConfig.but.Converttofreeform.ttip = Convertir ce jeu d'ailerons en forme libre +FinSetConfig.Convertfinset = Convertir le jeu d'ailerons +FinSetConfig.but.Splitfins = Séparer les ailerons +FinSetConfig.but.Splitfins.ttip = Diviser le jeu d'ailerons en aileron indépendant +FinSetConfig.lbl.Through-the-wall = Ailerons traversant le fuselage: +FinSetConfig.lbl.Tablength = Longueur de la patte: +FinSetConfig.ttip.Tablength = La longueur de la patte de l'aileron. +FinSetConfig.lbl.Tabheight = Hauteur de la patte: +FinSetConfig.ttip.Tabheight = La hauteur de l'envergure de la patte de l'aileron. +FinSetConfig.lbl.Tabposition = Position de la patte: +FinSetConfig.ttip.Tabposition = La position de la patte de l'aileron. +FinSetConfig.lbl.relativeto = relative à + +! MotorDatabaseLoadingDialog +MotorDbLoadDlg.title = Chargement des moteurs +MotorDbLoadDlg.Loadingmotors = Chargement des moteurs... + +! RocketConfig +RocketCfg.lbl.Designname = Nom du projet: +RocketCfg.lbl.Designer = Concepteur: +RocketCfg.lbl.Comments = Commentaires: +RocketCfg.lbl.Revisionhistory = Historique des modifications: +RocketCfg.lbl.Material = Matériaux: + +! ShockCordConfig +ShockCordCfg.lbl.Shockcordlength = Longueur du cordon amortisseur + +! RocketComponentConfig +RocketCompCfg.lbl.Componentname = Nom de la pièce: +RocketCompCfg.ttip.Thecomponentname = Le nom de la pièce. +RocketCompCfg.tab.Override = Forcer la valeur +RocketCompCfg.tab.MassandCGoverride = Forçage de la Masse et du CG +RocketCompCfg.tab.Figure = Forme +RocketCompCfg.tab.Figstyleopt = Options de la forme +RocketCompCfg.tab.Comment = Commentaires +RocketCompCfg.tab.Specifyacomment = Commentaires concernant la pièce +RocketCompCfg.lbl.Mass = Masse: +RocketCompCfg.lbl.Componentmass = Masse de la pièce: +RocketCompCfg.lbl.overriddento = (forcé à +RocketCompCfg.lbl.overriddenby = (forcé par +RocketCompCfg.lbl.Componentmaterial = Matériaux composant la pièce: +RocketCompCfg.lbl.Componentfinish = Finition de la pièce: +RocketCompCfg.lbl.ttip.componentmaterialaffects = Les matériaux utilisés pour la pièce affectent le poids de la pièce. +RocketCompCfg.combo.ttip.componentmaterialaffects = Les matériaux utilisés pour la pièce affectent le poids de la pièce. +RocketCompCfg.lbl.longA1 = La finition de la pièce affecte l'aérodynamisme de la pièce.
+RocketCompCfg.lbl.longA2 = La valeur indiquée est la hauteur moyenne de la rugosité de la surface. +RocketCompCfg.but.Setforall = Appliquer à tous +RocketCompCfg.but.ttip.Setforall = Régler la finition pour tous les composants de la fusée. +RocketCompCfg.lbl.Overridemassorcenter = Forcer la masse ou le centre de gravité du +RocketCompCfg.checkbox.Overridemass = Forcer la masse: +RocketCompCfg.checkbox.Overridecenterofgrav = Forcer le centre de gravité: +RocketCompCfg.checkbox.OverridemassandCG = Forcer la masse et le centre de gravité de tous les sous composants +RocketCompCfg.lbl.longB1 = Le forçage de la masse n'inclus pas le ou les moteurs.
+RocketCompCfg.lbl.longB2 = Le centre de gravité est mesuré à partir de l'extrémité avant de la fusée +RocketCompCfg.lbl.Commentsonthe = Commentaires à propos du +RocketCompCfg.lbl.Figurestyle = Modèle de forme: +RocketCompCfg.lbl.Componentcolor = Couleur de la pièce: +RocketCompCfg.lbl.Choosecolor = Choisir la couleur +RocketCompCfg.checkbox.Usedefaultcolor = Utiliser la couleur par défaut +RocketCompCfg.lbl.Complinestyle = Style de lignes pour les pièces: +RocketCompCfg.but.Saveasdefstyle = Sauver le modèle par défaut +RocketCompCfg.lbl.Diameter = Diamètre: +RocketCompCfg.lbl.Length = Longueur: +RocketCompCfg.lbl.Thickness = Epaisseur: +RocketCompCfg.checkbox.Endcapped = Arrière clos +RocketCompCfg.ttip.Endcapped = Précise si l'arrière du cône est clos. +RocketCompCfg.title.Noseconeshoulder = Accotement du cône +RocketCompCfg.title.Aftshoulder = Accotement arrière +RocketCompCfg.border.Foreshoulder = Accotement avant +!RocketCompCfg.lbl.Length = Length: + +! BulkheadConfig +BulkheadCfg.tab.Radius = Rayon: +BulkheadCfg.tab.Thickness = Epaisseur: +BulkheadCfg.tab.General = Général +BulkheadCfg.tab.Generalproperties = Propriétés générales + +!CenteringRingConfig +CenteringRingCfg.tab.Outerdiam = Diamètre externe: +CenteringRingCfg.tab.Innerdiam = Diamètre interne: +CenteringRingCfg.tab.Thickness = Epaisseur: +CenteringRingCfg.tab.General = Général +CenteringRingCfg.tab.Generalproperties = Propriétés Générales + +!ComponentConfigDialog +ComponentCfgDlg.configuration = +ComponentCfgDlg.configuration1 = configuration +ComponentCfgDlg.Modify = Modifier + +!EllipticalFinSetConfig +EllipticalFinSetCfg.Nbroffins = Nombre d'ailerons: +EllipticalFinSetCfg.Rotation = Rotation: +EllipticalFinSetCfg.Fincant = Inclinaison de l'aileron: +EllipticalFinSetCfg.Rootchord = Emplanture: +EllipticalFinSetCfg.Height = Hauteur: +EllipticalFinSetCfg.Positionrelativeto = Position relative à: +EllipticalFinSetCfg.plus = plus +EllipticalFinSetCfg.FincrossSection = Coupe de l'aileron: +EllipticalFinSetCfg.Thickness = Epaisseur: +EllipticalFinSetCfg.General = Général +EllipticalFinSetCfg.Generalproperties = Propriétés Générales +EllipticalFinSetCfg.ttip.Fincant = Angle d'inclinaison des ailerons par rapport au corps de la fusée + +!FreeformFinSetConfig +FreeformFinSetCfg.tab.General = Général +FreeformFinSetCfg.tab.ttip.General = Propriétés générales +FreeformFinSetCfg.tab.Shape = Forme +FreeformFinSetCfg.tab.ttip.Finshape = Forme de l'aileron +FreeformFinSetCfg.lbl.Numberoffins = Nombre d'ailerons: +FreeformFinSetCfg.lbl.Finrotation = Rotation des ailerons: +FreeformFinSetCfg.lbl.Fincant = Inclinaison de l'aileron: +FreeformFinSetCfg.lbl.ttip.Fincant = angle d'inclinaison des ailerons par rapport au corps de la fusée. +FreeformFinSetCfg.lbl.Posrelativeto = Position par rapport à: +FreeformFinSetCfg.lbl.plus = plus +FreeformFinSetCfg.lbl.FincrossSection = Coupe de l'aileron: +FreeformFinSetCfg.lbl.Thickness = Epaisseur: +! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle +FreeformFinSetCfg.lbl.doubleClick1 = Double-click +FreeformFinSetCfg.lbl.doubleClick2 = pour éditer +FreeformFinSetCfg.lbl.clickDrag = Cliquer+déplacer: Ajouter et déplacer des points +FreeformFinSetCfg.lbl.ctrlClick = Ctrl+cliquer: Enlever un point + + +!InnerTubeConfig +InnerTubeCfg.tab.Motor = Moteur +InnerTubeCfg.tab.ttip.Motor = Configuration du porte moteur +InnerTubeCfg.tab.Cluster = Cluster +InnerTubeCfg.tab.ttip.Cluster = Configuration du cluster +InnerTubeCfg.tab.Radialpos = Position circulaire +InnerTubeCfg.tab.ttip.Radialpos = Position circulaire +InnerTubeCfg.lbl.Selectclustercfg = Choisir la configuration du cluster: +InnerTubeCfg.lbl.TubeSep = Séparation du tube: +InnerTubeCfg.lbl.ttip.TubeSep = La Séparation des tubes, 1.0 = chacun se touche +InnerTubeCfg.lbl.Rotation = Rotation: +InnerTubeCfg.lbl.ttip.Rotation = Angle de rotation du cluster +InnerTubeCfg.lbl.Rotangle = Angle de rotation de la configuration du cluster +InnerTubeCfg.but.Splitcluster = Séparer le cluster +InnerTubeCfg.lbl.longA1 = séparer le cluster en pièces distinctes.
+InnerTubeCfg.lbl.longA2 = Cela duplique également tous les composants rattacher à ce tube interne. +InnerTubeCfg.but.Resetsettings = Réinitialiser les réglages +InnerTubeCfg.but.ttip.Resetsettings = Réinitialiser la séparation et la rotation aux valeurs par défauts + +! LaunchLugConfig +LaunchLugCfg.lbl.Length = Longueur: +LaunchLugCfg.lbl.Outerdiam = Diamètre externe: +LaunchLugCfg.lbl.Innerdiam = Diamètre interne: +LaunchLugCfg.lbl.Thickness = Epaisseur: +LaunchLugCfg.lbl.Radialpos = Position circulaire: +LaunchLugCfg.lbl.Posrelativeto = Position relative à: +LaunchLugCfg.lbl.plus = plus +LaunchLugCfg.tab.General = Général +LaunchLugCfg.tab.Generalprop = Propriétés Générales + +! MassComponentConfig +MassComponentCfg.lbl.Mass = Masse +MassComponentCfg.lbl.Length = Longueur +MassComponentCfg.lbl.Diameter = Diamètre +MassComponentCfg.lbl.PosRelativeto = Position relative à: +MassComponentCfg.lbl.plus = plus +MassComponentCfg.tab.General = Général +MassComponentCfg.tab.ttip.General = Propriétés Générales +MassComponentCfg.tab.Radialpos = Position sur le périmètre +MassComponentCfg.tab.ttip.Radialpos = Configuration de la position sur le périmètre +MassComponentCfg.lbl.Radialdistance = Rayon: +MassComponentCfg.lbl.Radialdirection = Azimut: +MassComponentCfg.but.Reset = Réinitialiser + +! MotorConfig +MotorCfg.checkbox.compmotormount = Cette pièce est un porte moteur +MotorCfg.lbl.Motorcfg = Configuration du moteur: +MotorCfg.but.New = Nouveau +MotorCfg.lbl.Currentmotor = Moteur actuel: +MotorCfg.lbl.Motoroverhang = Surplomb du moteur: +MotorCfg.lbl.Ignitionat = Allumage à: +MotorCfg.lbl.plus = plus +MotorCfg.lbl.seconds = secondes +MotorCfg.lbl.longA1 = Le projet actuel n'a qu'un étage. +MotorCfg.lbl.longA2 = Des étages peuvent-être ajoutés en cliquant \"Nouvel étage\". +MotorCfg.lbl.longB1 = Le projet actuel a +MotorCfg.lbl.longB2 = étage(s). +MotorCfg.but.Selectmotor = Choisir le moteur +MotorCfg.but.Removemotor = Enlever le moteur +MotorCfg.lbl.motorLabel = Aucun + +! NoseConeConfig +NoseConeCfg.lbl.Noseconeshape = Forme du cône de la fusée: +NoseConeCfg.lbl.Shapeparam = Paramètre de la forme: +NoseConeCfg.lbl.Noseconelength = Longueur du cône de la fusée: +NoseConeCfg.lbl.Basediam = Diamètre de la base: +NoseConeCfg.checkbox.Automatic = Automatique +NoseConeCfg.lbl.Wallthickness = Epaisseur de la paroi: +NoseConeCfg.checkbox.Filled = Aspérités bouchées +NoseConeCfg.tab.General = Général +NoseConeCfg.tab.ttip.General = Propriétés générales +NoseConeCfg.tab.Shoulder = Accotement +NoseConeCfg.tab.ttip.Shoulder = Propriétés de l'accotement + +! ParachuteConfig +ParachuteCfg.lbl.Canopy = Canopée: +ParachuteCfg.lbl.Diameter = Diamètre: +ParachuteCfg.lbl.Material = Matériau: +ParachuteCfg.combo.MaterialModel = La nature du matériau affecte le poids de la pièce. +ParachuteCfg.lbl.longA1 = Coefficient de traînée CD: +ParachuteCfg.lbl.longB1 = Le coefficient de traînée dépend de la surface totale du parachute.
+ParachuteCfg.lbl.longB2 = Un plus grand coefficient de trainée produit une descente plus lente. +ParachuteCfg.lbl.longB3 = Une valeur standard pour le parachute est 0.8. +ParachuteCfg.but.Reset = Réinitialiser +ParachuteCfg.lbl.Shroudlines = Suspentes: +ParachuteCfg.lbl.Numberoflines = Nombre de suspentes: +ParachuteCfg.lbl.Linelength = Longueur des suspentes: +ParachuteCfg.lbl.Material = Matériau: +ParachuteCfg.lbl.Posrelativeto = Position relative à: +ParachuteCfg.lbl.plus = plus +ParachuteCfg.lbl.Packedlength = Longueur plié: +ParachuteCfg.lbl.Packeddiam = Diamètre plié: +ParachuteCfg.lbl.Deploysat = Déploiement à: +ParachuteCfg.lbl.seconds = secondes +ParachuteCfg.lbl.Altitude = Altitude: +ParachuteCfg.tab.General = Général +ParachuteCfg.tab.ttip.General = Propriétés générales +ParachuteCfg.tab.Radialpos = Position sur le périmètre +ParachuteCfg.tab.ttip.Radialpos = Configuration de la position radial +ParachuteCfg.lbl.Radialdistance = Rayon: +ParachuteCfg.lbl.Radialdirection = Azimut: +ParachuteCfg.but.Reset = Réinitialiser +ParachuteCfg.lbl.plusdelay = Retard + +! ShockCordConfig +ShockCordCfg.lbl.Shockcordlength = Longueur du cordon amortisseur +ShockCordCfg.lbl.Shockcordmaterial = Matériau du cordon amortisseur: +ShockCordCfg.lbl.Posrelativeto = Position relative à: +ShockCordCfg.lbl.plus = plus +ShockCordCfg.lbl.Packedlength = Longueur emballé: +ShockCordCfg.lbl.Packeddiam = Diamètre emballé: +ShockCordCfg.tab.General = Général +ShockCordCfg.tab.ttip.General = Propriétés générales + +!SleeveConfig +SleeveCfg.tab.Outerdiam = Diamètre externe: +SleeveCfg.tab.Innerdiam = Diamètre interne: +SleeveCfg.tab.Wallthickness = Epaisseur des parois: +SleeveCfg.tab.Length = Longueur: +SleeveCfg.tab.General = Général +SleeveCfg.tab.Generalproperties = Propriétés générales + +! StreamerConfig +StreamerCfg.lbl.Striplength = Longueur de la bande: +StreamerCfg.lbl.Stripwidth = Largeur de la bande: +StreamerCfg.lbl.Striparea = Surface de la bande: +StreamerCfg.lbl.Aspectratio = Proportions: +StreamerCfg.lbl.Material = Matériau: +StreamerCfg.combo.ttip.MaterialModel = La nature du matériau affecte le poids de la pièce. +StreamerCfg.lbl.longA1 = Coefficient de traînée CD: +StreamerCfg.lbl.longB1 = Le coefficient de trainée dépend de la surface totale de la banderole.
+StreamerCfg.lbl.longB2 = Un plus grand coefficient de trainée produit une descente plus lente. +StreamerCfg.lbl.Automatic = Automatique +StreamerCfg.lbl.longC1 = le coefficient de trainée dépend de la surface totale de la banderole. +StreamerCfg.lbl.Posrelativeto = Position relative à: +StreamerCfg.lbl.plus = plus +StreamerCfg.lbl.Packedlength = Longueur emballé: +StreamerCfg.lbl.Packeddiam = Diamètre emballé: +StreamerCfg.lbl.Deploysat = Déploiement à: +StreamerCfg.lbl.seconds = secondes +StreamerCfg.lbl.Altitude = Altitude: +StreamerCfg.tab.General = Général +StreamerCfg.tab.ttip.General = Propriétés générales +StreamerCfg.tab.Radialpos = Position sur le périmètre +StreamerCfg.tab.ttip.Radialpos = Configuration de la position sur le périmètre +StreamerCfg.lbl.Radialdistance = Rayon: +StreamerCfg.lbl.Radialdirection = Azimut: +StreamerCfg.but.Reset = Réinitialiser +StreamerCfg.lbl.plusdelay = Retard + +! ThicknessRingComponentConfig +ThicknessRingCompCfg.tab.Outerdiam = Diamètre externe: +ThicknessRingCompCfg.tab.Innerdiam = Diamètre interne: +ThicknessRingCompCfg.tab.Wallthickness = Epaisseur de la paroi: +ThicknessRingCompCfg.tab.Length = Longueur: +ThicknessRingCompCfg.tab.General = Général +ThicknessRingCompCfg.tab.Generalprop = Propriétés générales + +! TransitionConfig +TransitionCfg.lbl.Transitionshape = Forme de la transition: +TransitionCfg.checkbox.Clipped = Emboitée +TransitionCfg.lbl.Shapeparam = Paramètre de la forme: +TransitionCfg.lbl.Transitionlength = Longueur de la transition: +TransitionCfg.lbl.Forediam = Diamètre avant: +TransitionCfg.checkbox.Automatic = Automatique +TransitionCfg.lbl.Aftdiam = Diamètre arrière: +TransitionCfg.lbl.Wallthickness = Epaisseur de la paroi: +TransitionCfg.checkbox.Filled = Aspérités bouchées +TransitionCfg.tab.General = Général +TransitionCfg.tab.Generalproperties = Propriétés Générales +TransitionCfg.tab.Shoulder = Accotement +TransitionCfg.tab.Shoulderproperties = Propriétés de l'accotement + +! TrapezoidFinSetConfig +TrapezoidFinSetCfg.lbl.Nbroffins = Nombre d'ailerons: +TrapezoidFinSetCfg.lbl.ttip.Nbroffins = Le nombre d'ailerons composant le jeu. +TrapezoidFinSetCfg.lbl.Finrotation = Rotation de l'aileron: +TrapezoidFinSetCfg.lbl.ttip.Finrotation = Angle du premier aileron dans le jeu. +TrapezoidFinSetCfg.lbl.Fincant = Inclinaison de l'aileron: +TrapezoidFinSetCfg.lbl.ttip.Fincant = Angle d'inclinaison des ailerons par rapport au tube du corps de la fusée. +TrapezoidFinSetCfg.lbl.Rootchord = Longueur de la base de l'aileron: +TrapezoidFinSetCfg.lbl.Tipchord = Longueur du bout de l'aileron: +TrapezoidFinSetCfg.lbl.Height = Hauteur: +TrapezoidFinSetCfg.lbl.Sweeplength = Longueur du bord d'attaque: +TrapezoidFinSetCfg.lbl.Sweepangle = Angle du bord d'attaque: +TrapezoidFinSetCfg.lbl.FincrossSection = Coupe de l'aileron: +TrapezoidFinSetCfg.lbl.Thickness = Epaisseur: +TrapezoidFinSetCfg.lbl.Posrelativeto = Position relative à: +TrapezoidFinSetCfg.lbl.plus = plus +TrapezoidFinSetCfg.tab.General = Général +TrapezoidFinSetCfg.tab.Generalproperties = Propriétés générales + +!MotorConfigurationModel +MotorCfgModel.Editcfg = Modifier les configurations + +! StorageOptionChooser +StorageOptChooser.lbl.Simdatatostore = Données simulées à stocker: +StorageOptChooser.rdbut.Allsimdata = Toutes les données des simulations +StorageOptChooser.lbl.longA1 = Enregistrer toutes les données des simulations.
+StorageOptChooser.lbl.longA2 = Cela peut entraîner de très gros fichiers! +StorageOptChooser.rdbut.Every = Every +StorageOptChooser.lbl.longB1 = Store plottable values approximately this far apart.
+StorageOptChooser.lbl.longB2 = Des valeurs plus grandes produisent des fichiers plus petits. +StorageOptChooser.lbl.seconds = secondes +StorageOptChooser.rdbut.Onlyprimfig = Seuls les chiffres primaires +StorageOptChooser.lbl.longC1 = Stocker seulement les valeurs montrées dans le tableau récapitulatif.
+StorageOptChooser.lbl.longC2 = Cela produira des fichiers plus petit. +StorageOptChooser.checkbox.Compfile = Compresse le fichier +StorageOptChooser.lbl.UsingComp = Utiliser la compression réduit significativement la taille du fichier. +StorageOptChooser.lbl.longD1 = Une estimation sur la taille qu'aurait le fichier résultant avec les options actuelles. +StorageOptChooser.ttip.Saveopt = Options de sauvegarde +StorageOptChooser.lbl.Estfilesize = Taille estimée du fichier: +StorageOptChooser.lbl.Saveopt = Options de sauvegarde + +! ThrustCurveMotorSelectionPanel +TCMotorSelPan.lbl.Selrocketmotor = Choisir le moteur fusée: +TCMotorSelPan.checkbox.hideSimilar = Cacher les courbes de poussées similaires +TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Montrer tous les moteurs +TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Montrer les moteurs avec un diamètre inferieur au porte moteur +TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Montrer les moteurs avec un diamètre égale au porte moteur +TCMotorSelPan.lbl.Motormountdia = Diamètre du tube porte moteur: +TCMotorSelPan.lbl.Search = Rechercher: +TCMotorSelPan.lbl.Selectthrustcurve = Choisir la courbe de poussée: +TCMotorSelPan.lbl.Ejectionchargedelay = Retard de la charge d'éjection: +TCMotorSelPan.equalsIgnoreCase.None = Aucun +TCMotorSelPan.lbl.NumberofsecondsorNone = (Nombre de secondes ou \"Aucun\") +TCMotorSelPan.lbl.Totalimpulse = Impulsion totale: +TCMotorSelPan.lbl.Avgthrust = Poussée moyenne: +TCMotorSelPan.lbl.Maxthrust = Poussée Max.: +TCMotorSelPan.lbl.Burntime = Temps de combustion: +TCMotorSelPan.lbl.Launchmass = Masse au lancement: +TCMotorSelPan.lbl.Emptymass = Masse à vide: +TCMotorSelPan.lbl.Datapoints = Points de données: +TCMotorSelPan.lbl.Digest = Assimilation: +TCMotorSelPan.title.Thrustcurve = Courbe de poussée: +TCMotorSelPan.title.Thrust = Poussée +TCMotorSelPan.delayBox.None = Aucun + + +! PlotDialog +PlotDialog.title.Flightdataplot = Tracé du vol +PlotDialog.Chart.Simulatedflight = Simulation du vol +PlotDialog.CheckBox.Showdatapoints = Afficher un point pour chaque valeur +PlotDialog.lbl.Chart = Cliquer+déplacer en bas +droite pour agrandir, haut+gauche pour rétrécir + + +! "main" prefix is used for the main application dialog + +# FIXME: Rename the description keys + +main.menu.file = Fichier +main.menu.file.desc = File-handling related tasks +main.menu.file.new = Nouveau +main.menu.file.new.desc = Crée un nouveau projet fusée +main.menu.file.open = Ouvrir... +BasicFrame.item.Openrocketdesign = Ouvre un projet fusée +main.menu.file.openExample = Ouvrir un exemple... +BasicFrame.item.Openexamplerocketdesign = Ouvre un exemple de projet fusée +main.menu.file.save = Sauvegarder +BasicFrame.item.SavecurRocketdesign = Sauvegarde le projet fusée en cours +main.menu.file.saveAs = Sauvegarder sous... +BasicFrame.item.SavecurRocketdesnewfile = Sauvegarde le projet fusée en cour dans un nouveau fichier +main.menu.file.print = Imprimer/Exporter en PDF... +main.menu.file.print.desc = Imprimer ou sauvegarde en PDF la liste des pièces et les gabaries des ailerons +main.menu.file.close = Fermer +BasicFrame.item.Closedesign = Ferme le projet fusée en cour +main.menu.file.quit = Quitter +BasicFrame.item.Quitprogram = Quitte le programme + +main.menu.edit = Modifier +BasicFrame.menu.Rocketedt = Modification de la fusée +main.menu.edit.undo = Annuler modification +main.menu.edit.undo.desc = Annuler l'opération précédente +main.menu.edit.redo = Refaire modification +main.menu.edit.redo.desc = Refaire l'opération precedente qui avait été défaite +main.menu.edit.cut = Couper +main.menu.edit.copy = Copier +main.menu.edit.paste = Coller +main.menu.edit.delete = Effacer +main.menu.edit.resize = Redimensionner... +main.menu.edit.resize.desc = Redimensionner certaines parties de la fusée +main.menu.edit.preferences = Préférences +main.menu.edit.preferences.desc = Configure les préférences de l'application + +main.menu.analyze = Analyse +main.menu.analyze.desc = Analyses de la fusée +main.menu.analyze.componentAnalysis = Analyse des Pièces +main.menu.analyze.componentAnalysis.desc = Analyse séparé des pices de la fusée +main.menu.analyze.optimization = Optimisation de la fusée +main.menu.analyze.optimization.desc = Optimisation generale de la fusée + +main.menu.help = Aide +main.menu.help.desc = Information à propos d'OpenRocket +main.menu.help.license = Licence +main.menu.help.license.desc = Information sur la license d'OpenRocket +main.menu.help.bugReport = Rapport d'erreurs +main.menu.help.bugReport.desc = Information pour pouvoir sgnaler les bugs dans OpenRocket +main.menu.help.debugLog = Debug log +main.menu.help.debugLog.desc = Visualiser le fichier log d'OpenRocket +main.menu.help.about = A propos +main.menu.help.about.desc = Détails du Copyright d'OpenRocket + +main.menu.debug = Debug +main.menu.debug.whatisthismenu = Quel est ce menu? +main.menu.debug.createtestrocket = Créer une fusée test + +! database +! Translate here all material database +! + +! Material database +! BULK_MATERIAL +Databases.materials.Acrylic = Acrylique +Databases.materials.Balsa = Balsa +Databases.materials.Birch = Bouleau +Databases.materials.Cardboard = Carton +Databases.materials.Carbonfiber = Fibre de carbone +Databases.materials.Cork = Liège +Databases.materials.DepronXPS = Depron (XPS) +Databases.materials.Fiberglass = Fibre de verre +Databases.materials.Kraftphenolic = Kraft phénolique +Databases.materials.Maple = Érable +Databases.materials.Paperoffice = Papier (bureau) +Databases.materials.Pine = Pin +Databases.materials.Plywoodbirch = Contre-plaqué (bouleau) +Databases.materials.PolycarbonateLexan = Polycarbonate (Lexan) +Databases.materials.Polystyrene = Polystyrène +Databases.materials.PVC = PVC +Databases.materials.Spruce = Sapin +Databases.materials.StyrofoamgenericEPS = Polystyrène (générique EPS) +Databases.materials.StyrofoamBluefoamXPS = \"Mousse Bleue\" de polystyrène (XPS) +Databases.materials.Quantumtubing = Tube Quantum +Databases.materials.BlueTube = Blue tube +!SURFACE_MATERIAL +Databases.materials.Ripstopnylon = Ripstop nylon +Databases.materials.Mylar = Mylar +Databases.materials.Polyethylenethin = Polyéthylène (fin) +Databases.materials.Polyethyleneheavy = Polyéthylène (lourd) +Databases.materials.Silk = Soie +Databases.materials.Paperoffice = Papier (bureau) +Databases.materials.Cellophane = Cellophane +Databases.materials.Crepepaper = Papier crépon +! LINE_MATERIAL +Databases.materials.Threadheavy-duty = Fil(résistant) +Databases.materials.Elasticcordround2mm = Corde Elastique (ronde 2mm, 1/16 in) +Databases.materials.Elasticcordflat6mm = Corde Elastique (plate 6mm, 1/4 in) +Databases.materials.Elasticcordflat12mm = Corde Elastique (plate 12mm, 1/2 in) +Databases.materials.Elasticcordflat19mm = Corde Elastique (plate 19mm, 3/4 in) +Databases.materials.Elasticcordflat25mm = Corde Elastique (plate 25mm, 1 in) +Databases.materials.Braidednylon2mm = Nylon tressé (2 mm, 1/16 in) +Databases.materials.Braidednylon3mm = Nylon tressé (3 mm, 1/8 in) +Databases.materials.Tubularnylon11mm = Nylon tubulaire (11 mm, 7/16 in) +Databases.materials.Tubularnylon14mm = Nylon tubulaire (14 mm, 9/16 in) +Databases.materials.Tubularnylon25mm = Nylon tubulaire (25 mm, 1 in) + +! ExternalComponent +ExternalComponent.Rough = Rugueuse +ExternalComponent.Unfinished = Non peinte +ExternalComponent.Regularpaint = Peinture classique +ExternalComponent.Smoothpaint = Fine couche +ExternalComponent.Polished = Polie + +! LineStyle +LineStyle.Solid = Ligne pleine +LineStyle.Dashed = Tiret +LineStyle.Dotted = Ligne pointillée +LineStyle.Dash-dotted = Ligne Pointillée et Tiret +LineStyle.Defaultstyle = Style par défaut + +! Shape +Shape.Conical = Conique +Shape.Conical.desc1 = Un cône conique a un profil triangulaire. +Shape.Conical.desc2 = Une transition conique a des côtés droits. +Shape.Ogive = Ogive +Shape.Ogive.desc1 = Un cône ogival a un profil qui est un segment de cercle. La valeur du paramètre de forme 1 produit une ogive tangente, qui a une transition en douceur vers le tube de la fusée, des valeurs inférieures à 1 produisent des ogives sécantes. +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 ogive tangente, qui a une transition en douceur vers le tube de la fusée à l'extrémité arrière, des valeurs inférieures à 1 produisent des ogives sécantes. +Shape.Ellipsoid = Ellipsoïde +Shape.Ellipsoid.desc1 = Un cône ellipsoïdal a un profil d'une demi ellipse dont les axes principaux sont de longueurs 2×la longueur et diamètre. +Shape.Ellipsoid.desc2 = Une transition ellipsoïdale a un profil d'une demi ellipse dont les axes principaux sont de longueurs 2×longueur et diamètre. Si la transition n'est pas coupée alors le profil est étendu au centre par le rayon correspondant. +Shape.Powerseries = Série Haute puissance +Shape.Powerseries.desc1 = Un cône de puissance a un profil de Rayon × (x / Longueur)k ou k est le paramètre de la forme. Pour k=0,5 c'est une \u00BD-puissance ou une ogive parabolique, pour k=0,75 une \u00BE-puissance, et pour k=1 un cône conique. +Shape.Powerseries.desc2 = Une transition de la série haute puissance a un profile de Rayon × (x / Longueur)k ou k est le paramètre de la forme. Pour k=0,5 la transition est \u00BD-puissance ou parabolique, pour k=0,75 une \u00BE-puissance, et pour k=1 conique. +Shape.Parabolicseries = Série parabolique +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 parabole pleine qui est tangent au tube de la fusée, 0,75 produit un 3/4 de parabole, 0,5 produit une 1/2 parabole et 0 produit un cône conique. +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 parabole pleine qui est tangent au tube de la fusée à l'extrémité arrière, 0,75 produit une 3/4 parabole, 0,5 produit une 1/2 parabole et 0 produit une transition conique. +Shape.Haackseries = Série Haack +Shape.Haackseries.desc1 = Les cônes du type Haack sont conçus pour minimiser la trainée. Le paramètre de forme égale à 0 produit une LD-Haack ou un cône Von Karman, 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 LV-Haack, ce qui minimise la trainée pour une longueur et un volume fixe. +Shape.Haackseries.desc2 = Les cônes 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 LD-Haack ou Von Karman, tandis qu'une valeur de 0,333 produit une forme LV-Haack. + + +! RocketComponent +RocketComponent.Position.TOP = Haut de la pièce parent +RocketComponent.Position.MIDDLE = Milieu de la pièce parent(porteuse) +RocketComponent.Position.BOTTOM = Bas de la pièce parent +RocketComponent.Position.AFTER = Après la pièce parent +RocketComponent.Position.ABSOLUTE = Pointe de l'ogive + +! LaunchLug +LaunchLug.Launchlug = Tube de guidage +! NoseCone +NoseCone.NoseCone = Ogive +! Transition +Transition.Transition = Transition +!Stage +Stage.Stage = Etage +! BodyTube +BodyTube.BodyTube = Tube du corps +! TubeCoupler +TubeCoupler.TubeCoupler = Coupleur de tube +!InnerTube +InnerTube.InnerTube = Tube interne +! TrapezoidFinSet +TrapezoidFinSet.TrapezoidFinSet = Ailerons Trapézoïdaux +! FreeformFinSet +FreeformFinSet.FreeformFinSet = Ailerons personnalisés +!MassComponent +MassComponent.MassComponent = Poids +! Parachute +Parachute.Parachute = Parachute +! ShockCord +ShockCord.ShockCord = Cordon amortisseur +! Bulkhead +Bulkhead.Bulkhead = Cloison + +!Rocket +Rocket.motorCount.Nomotor = [aucun moteurs] +Rocket.compname.Rocket = Fusée + +!MotorMount +MotorMount.IgnitionEvent.AUTOMATIC = Automatique (lancement ou charge d'éjection) +MotorMount.IgnitionEvent.LAUNCH = Lancement +MotorMount.IgnitionEvent.EJECTION_CHARGE = Première charge d'éjection ou étage précédent +MotorMount.IgnitionEvent.BURNOUT = Première combustion totale de l'étage précédent +MotorMount.IgnitionEvent.NEVER = Jamais + +!ComponentIcons +ComponentIcons.Nosecone = Ogive +ComponentIcons.Bodytube = Tube +ComponentIcons.Transition = Transition +ComponentIcons.Trapezoidalfinset = Jeu d'ailerons de forme trapézoïdale +ComponentIcons.Ellipticalfinset = Jeu d'ailerons de forme elliptique +ComponentIcons.Freeformfinset = Jeu d'ailerons de forme personnalisé +ComponentIcons.Launchlug = Tube de guidage +ComponentIcons.Innertube = Tube interne +ComponentIcons.Tubecoupler = Coupleur de tube +ComponentIcons.Centeringring = Anneau de centrage +ComponentIcons.Bulkhead = Cloison +ComponentIcons.Engineblock = Bague de retension moteur +ComponentIcons.Parachute = Parachute +ComponentIcons.Streamer = Banderolle +ComponentIcons.Shockcord = Cordon amortisseur +ComponentIcons.Masscomponent = Piéce Masse +ComponentIcons.disabled = (désactivé) + +! StageAction +StageAction.Stage = Etage + +! RecoveryDevice +RecoveryDevice.DeployEvent.LAUNCH = Lancement(plus NN secondes) +RecoveryDevice.DeployEvent.EJECTION = Première charge d'éjection de cet étage +RecoveryDevice.DeployEvent.APOGEE = Apogée +RecoveryDevice.DeployEvent.ALTITUDE = Altitude spécifiée durant la descente +RecoveryDevice.DeployEvent.NEVER = Jamais + +! FlightEvent +FlightEvent.Type.LAUNCH = Lancement +FlightEvent.Type.IGNITION = Allumage du moteur +FlightEvent.Type.LIFTOFF = Décollage +FlightEvent.Type.LAUNCHROD = Dégagement de rampe de lancement +FlightEvent.Type.BURNOUT = Fin de combustion du moteur +FlightEvent.Type.EJECTION_CHARGE = Charge d'éjection +FlightEvent.Type.STAGE_SEPARATION = Séparation d'étage +FlightEvent.Type.APOGEE = Apogée +FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Déploiement du dispositif de récupération +FlightEvent.Type.GROUND_HIT = Atterrissage +FlightEvent.Type.SIMULATION_END = Fin de la simulation +FlightEvent.Type.ALTITUDE = Changement d'altitude + +! ThrustCurveMotorColumns +TCurveMotorCol.MANUFACTURER = Fabricant +TCurveMotorCol.DESIGNATION = Désignation +TCurveMotorCol.TYPE = Type +TCurveMotorCol.DIAMETER = Diamètre +TCurveMotorCol.LENGTH = Longueur + +! RocketInfo +RocketInfo.lengthLine.Length = Longueur +RocketInfo.lengthLine.maxdiameter = , diamètre max. +RocketInfo.massText1 = Masse avec moteurs +RocketInfo.massText2 = Masse sans moteurs +RocketInfo.at = à M= +RocketInfo.cgText = CG: +RocketInfo.cpText = CP: +RocketInfo.stabText = Stabilité: +RocketInfo.Warning = Avertissement: +RocketInfo.Calculating = Calcul en cours... +RocketInfo.Apogee = Apogée: +RocketInfo.Maxvelocity = Vitesse Max.: +RocketInfo.Maxacceleration = Accélération Max.: +RocketInfo.apogeeValue = N/A +RocketInfo.Mach = (Mach +RocketInfo.velocityValue = N/A +RocketInfo.accelerationValue = N/A + +! FinSet +FinSet.CrossSection.SQUARE = Carré +FinSet.CrossSection.ROUNDED = Arondie +FinSet.CrossSection.AIRFOIL = Airfoil +FinSet.TabRelativePosition.FRONT = Emplanture avant +FinSet.TabRelativePosition.CENTER = Emplanture centrale +FinSet.TabRelativePosition.END = Emplanture arrière + +! FlightDataType +FlightDataType.TYPE_TIME = Temps +FlightDataType.TYPE_ALTITUDE = Altitude +FlightDataType.TYPE_VELOCITY_Z = Vitesse verticale +FlightDataType.TYPE_ACCELERATION_Z = Accélération verticale +FlightDataType.TYPE_VELOCITY_TOTAL = Vitesse totale +FlightDataType.TYPE_ACCELERATION_TOTAL = Accélération totale +FlightDataType.TYPE_POSITION_X = Position contre le vent +FlightDataType.TYPE_POSITION_Y = Position parallèle au vent +FlightDataType.TYPE_POSITION_XY = Distance latérale +FlightDataType.TYPE_POSITION_DIRECTION = Direction latérale +FlightDataType.TYPE_VELOCITY_XY = Vitesse latérale +FlightDataType.TYPE_ACCELERATION_XY = Accélération latérale +FlightDataType.TYPE_AOA = Angle d'attaque +FlightDataType.TYPE_ROLL_RATE = Taux de roulis +FlightDataType.TYPE_PITCH_RATE = Taux de tangage +FlightDataType.TYPE_YAW_RATE = Taux d'embardée +FlightDataType.TYPE_MASS = Masse +FlightDataType.TYPE_LONGITUDINAL_INERTIA = Moment d'inertie longitudinale +FlightDataType.TYPE_ROTATIONAL_INERTIA = Moment d'inertie rotatif +FlightDataType.TYPE_CP_LOCATION = Emplacement du CP +FlightDataType.TYPE_CG_LOCATION = Emplacement du CG +FlightDataType.TYPE_STABILITY = Calibres marge de stabilité +FlightDataType.TYPE_MACH_NUMBER = Mach number +FlightDataType.TYPE_REYNOLDS_NUMBER = Nombre de Reynolds +FlightDataType.TYPE_THRUST_FORCE = Poussée +FlightDataType.TYPE_DRAG_FORCE = Force de traînée +FlightDataType.TYPE_DRAG_COEFF = Coefficient de traînée +FlightDataType.TYPE_AXIAL_DRAG_COEFF = Coefficient de trainée axiale +FlightDataType.TYPE_FRICTION_DRAG_COEFF = Coefficient de traînée de friction +FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Coefficient de traînée de pression +FlightDataType.TYPE_BASE_DRAG_COEFF = Coefficient de traînée de base +FlightDataType.TYPE_NORMAL_FORCE_COEFF = Coefficient de force normale +FlightDataType.TYPE_PITCH_MOMENT_COEFF = Coefficient de moment de tangage +FlightDataType.TYPE_YAW_MOMENT_COEFF = Coefficient de moment d'embardée +FlightDataType.TYPE_SIDE_FORCE_COEFF = Coefficient de force latérale +FlightDataType.TYPE_ROLL_MOMENT_COEFF = Coefficient de moment de roulis +FlightDataType.TYPE_ROLL_FORCING_COEFF = Coefficient de forçage de roulis +FlightDataType.TYPE_ROLL_DAMPING_COEFF = Coefficient d'amortissement de roulis +FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Coefficient d'amortissement de tangage +FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Coefficient d'amortissement d'embardée +FlightDataType.TYPE_REFERENCE_LENGTH = Longueur de référence +FlightDataType.TYPE_REFERENCE_AREA = Surface de référence +FlightDataType.TYPE_ORIENTATION_THETA = Orientation verticale (zénith) +FlightDataType.TYPE_ORIENTATION_PHI = Orientation latérale (azimut) +FlightDataType.TYPE_WIND_VELOCITY = Vitesse de vent +FlightDataType.TYPE_AIR_TEMPERATURE = Température de l'air +FlightDataType.TYPE_AIR_PRESSURE = Pression atmosphérique +FlightDataType.TYPE_SPEED_OF_SOUND = Vitesse du son +FlightDataType.TYPE_TIME_STEP = Pas de simulation du temps +FlightDataType.TYPE_COMPUTATION_TIME = Temps de calcul +FlightDataType.TYPE_LATITUDE = Latitude +FlightDataType.TYPE_LONGITUDE = Longitude +FlightDataType.TYPE_CORIOLIS_ACCELERATION = Accélération de Coriolis + +! PlotConfiguration +PlotConfiguration.Verticalmotion = Mouvement vertical par rapport au temps +PlotConfiguration.Totalmotion = Mouvement total par rapport au temps +PlotConfiguration.Flightside = Profil latéral du vol +PlotConfiguration.Stability = Stabilité par rapport au temps +PlotConfiguration.Dragcoef = Coefficients de traînée par rapport au Mach number +PlotConfiguration.Rollcharacteristics = Caractéristiques de roulis +PlotConfiguration.Angleofattack = Angle d'attaque et orientation par rapport au temps +PlotConfiguration.Simulationtime = Pas du temps et temps de calcul + +! Warning +Warning.LargeAOA.str1 = Grand angle d'attaque rencontré. +Warning.LargeAOA.str2 = Grand angle d'attaque rencontré ( +Warning.DISCONTINUITY = Discontinuité dans le diamètre du corps de la fusée. +Warning.THICK_FIN = Les ailerons fin ne seront peut être pas modélisés correctement. +Warning.JAGGED_EDGED_FIN = Des ailerons aux bords irréguliers ne seront pas modélisés correctement. +Warning.LISTENERS_AFFECTED = Listeners modified the flight simulation +Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Le dispositif de récupération s'est ouvert alors que la combustion du moteur n'était pas finie. +Warning.FILE_INVALID_PARAMETER = Paramètre invalide rencontré, ignorer. + + +! Scale dialog +ScaleDialog.lbl.scaleRocket = Fusée entière +ScaleDialog.lbl.scaleSubselection = La sélection et tous ses composants +ScaleDialog.lbl.scaleSelection = Seulement les composants sélectionnés +ScaleDialog.title = Redimensionner le projet +ScaleDialog.lbl.scale = Mise à l'échelle: +ScaleDialog.lbl.scale.ttip = Choisir de redimensionner tout le projet ou seulement la pièce choisie +ScaleDialog.lbl.scaling = Echelle à appliquer: +ScaleDialog.lbl.scaling.ttip = Taille résultante,les valeurs au-dessus de 100% agrandissent et les valeurs en-dessous de 100% réduisent le design. +! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]" +ScaleDialog.lbl.scaleFrom = Mise à l'échelle de +ScaleDialog.lbl.scaleTo = à +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 = Redimensionner +ScaleDialog.undo.scaleRocket = Redimensionner la fusée +ScaleDialog.undo.scaleComponent = Redimensionner une pièce +ScaleDialog.undo.scaleComponents = Redimensionner les pièces + +!icons +Icons.Undo = Undo +Icons.Redo = Redo + +OpenRocketPrintable.Partsdetail = Détail des pièces +OpenRocketPrintable.Fintemplates = Gabaries des ailerons +OpenRocketPrintable.DesignReport = Rapport de conception + +OpenRocketDocument.Redo = Refaire +OpenRocketDocument.Undo = Défaire + +!EllipticalFinSet +EllipticalFinSet.Ellipticalfinset = Ailerons elliptique + +! Optimization + +! Modifiers + +optimization.modifier.nosecone.length = Longueur du cône +optimization.modifier.nosecone.length.desc = Optimise la longueur du cône. +optimization.modifier.nosecone.diameter = Diamètre du cône +optimization.modifier.nosecone.diameter.desc = Optimise le diamètre du cône. +optimization.modifier.nosecone.thickness = Epaisseur du cône +optimization.modifier.nosecone.thickness.desc = Optimise l'épaisseur des parois du cône. +optimization.modifier.nosecone.shapeparameter = Paramètre de la forme +optimization.modifier.nosecone.shapeparameter.desc = Optimise les paramètres de forme du cône. + +optimization.modifier.transition.length = Longueur de la Transition +optimization.modifier.transition.length.desc = Optimise la longueur de la transition. +optimization.modifier.transition.forediameter = Diamètre avant de la Transition +optimization.modifier.transition.forediameter.desc = Optimise le diamètre avant de la transition. +optimization.modifier.transition.aftdiameter = Diamètre arrière de la transition +optimization.modifier.transition.aftdiameter.desc = Optimise le diamètre arrière de la transition. +optimization.modifier.transition.thickness = Epaisseur de la transition +optimization.modifier.transition.thickness.desc = Optimise l'épaisseur des parois de la transition. +optimization.modifier.transition.shapeparameter = Paramètre de la forme +optimization.modifier.transition.shapeparameter.desc = Optimise le paramètre de la forme. + +optimization.modifier.bodytube.length = Longueur du tube du corps +optimization.modifier.bodytube.length.desc = Optimise la longueur du tube du corps. +optimization.modifier.bodytube.outerDiameter = Diamètre externe du tube du corps +optimization.modifier.bodytube.outerDiameter.desc = Optimise le diamètre externe du tube du corps tout en maintenant l'épaisseur des parois. +optimization.modifier.bodytube.innerDiameter = Diamètre interne du tube du corps +optimization.modifier.bodytube.thickness = Epaisseur du tube du corps +optimization.modifier.bodytube.thickness.desc = Optimise l'épaisseur des parois du tube du corps. + +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 = Hauteur +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 = Hauteur +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 = Optimisation de la position du jeux d'ailerons sur le corps de la fusée. + +optimization.modifier.launchlug.length = Longueur +optimization.modifier.launchlug.length.desc = Optimisation de la longueur du tube de guidage. +optimization.modifier.launchlug.outerDiameter = Diamètre externe +optimization.modifier.launchlug.outerDiameter.desc = Optimisation du diamètre externe du tube de guidage. +optimization.modifier.launchlug.thickness = Epaisseur +optimization.modifier.launchlug.thickness.desc = Optimise l'épaisseur de la bague de guide tout en gardant le diamètre extérieur constant. +optimization.modifier.launchlug.position = Position +optimization.modifier.launchlug.position.desc = Optimise la position de la bague de guidage le long du corps de la fusée. + + +optimization.modifier.internalcomponent.position = Position +optimization.modifier.internalcomponent.position.desc = Optimise la position de la pièce par rapport à la pièce parent. + +optimization.modifier.masscomponent.mass = Masse +optimization.modifier.masscomponent.mass.desc = Optimise la masse du composant. + +optimization.modifier.parachute.diameter = Diamètre +optimization.modifier.parachute.diameter.desc = Optimise le diamètre de la coupole du parachute. +optimization.modifier.parachute.coefficient = Coefficient de trainée +optimization.modifier.parachute.coefficient.desc = Optimisation du coefficient de trainée du parachute. Un parachute type à un coefficient de trainée d'environ 0.8. + +optimization.modifier.streamer.length = Longueur +optimization.modifier.streamer.length.desc = Optimisation de la longueur de la banderole (streamer). +optimization.modifier.streamer.width = Largeur +optimization.modifier.streamer.width.desc = Optimisation de la largeur de la banderole (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 = Coefficient de trainée +optimization.modifier.streamer.coefficient.desc = Optimisation du coéfficient de trainée de la banderole (streamer). + +optimization.modifier.recoverydevice.deployDelay = Retard du déploiement +optimization.modifier.recoverydevice.deployDelay.desc = Optimise le délai du déploiement du système du récupération. +optimization.modifier.recoverydevice.deployAltitude = Altitude du déploiement +optimization.modifier.recoverydevice.deployAltitude.desc = Optimise l'altitude de déploiement du dispositif de récupération. + +optimization.modifier.rocketcomponent.overrideMass = Forcer la masse +optimization.modifier.rocketcomponent.overrideMass.desc = Optimise le forçage de la masse du composant. +optimization.modifier.rocketcomponent.overrideCG = forcer le CG +optimization.modifier.rocketcomponent.overrideCG.desc = Optimise le forçage du centre de gravité du composant. + +optimization.modifier.motormount.overhang = Surplomb du moteur +optimization.modifier.motormount.overhang.desc = Optimise le surplomb du moteur. +optimization.modifier.motormount.delay = Retard de l'allumage moteur +optimization.modifier.motormount.delay.desc = Optimisation du retard d'allumage du moteur. + + + + +! General rocket design optimization dialog + +GeneralOptimizationDialog.title = Optimisation de la fusée +GeneralOptimizationDialog.goal.maximize = Maximiser la valeur +GeneralOptimizationDialog.goal.minimize = Minimiser la valeur +GeneralOptimizationDialog.goal.seek = Cherchez la valeur de +GeneralOptimizationDialog.btn.start = Démarrer l'optimisation +GeneralOptimizationDialog.btn.stop = Terminer l'optimisation +GeneralOptimizationDialog.lbl.paramsToOptimize = Paramètres à optimiser: +GeneralOptimizationDialog.btn.add = Ajouter +GeneralOptimizationDialog.btn.add.ttip = Ajouter le paramètre sélectionné aux paramètres à optimiser +GeneralOptimizationDialog.btn.remove = Enlever +GeneralOptimizationDialog.btn.remove.ttip = Enlever le paramètre sélectionné des paramètres à optimiser +GeneralOptimizationDialog.btn.removeAll = Tout enlever +GeneralOptimizationDialog.btn.removeAll.ttip = Enlever tous les paramètres de l'optimisation +GeneralOptimizationDialog.lbl.availableParams = Paramètres disponible: +GeneralOptimizationDialog.lbl.optimizationOpts = Options pour l'optimisation +GeneralOptimizationDialog.lbl.optimizeSim = Optimiser la simulation: +GeneralOptimizationDialog.lbl.optimizeSim.ttip = Choisir la simulation à optimiser +GeneralOptimizationDialog.lbl.optimizeValue = Valeur optimum +GeneralOptimizationDialog.lbl.optimizeValue.ttip = Choisir quelle valeur à optimiser +GeneralOptimizationDialog.lbl.optimizeGoal = But de l'optimisation: +GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Choisir le but de l'optimisation +GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Valeur personnalisée à rechercher +GeneralOptimizationDialog.lbl.requireStability = Stabilité désirée +GeneralOptimizationDialog.lbl.requireMinStability = Stabilité minimum: +GeneralOptimizationDialog.lbl.requireMinStability.ttip = Exiger une marge de stabilité statique minimale pour le design +GeneralOptimizationDialog.lbl.requireMaxStability = Stabilité maximum: +GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Exiger une marge de stabilité statique maximale pour le design +GeneralOptimizationDialog.status.bestValue = Meilleure valeur: +GeneralOptimizationDialog.status.bestValue.ttip = Meilleure valeur optimum trouvé jusqu'à présent. +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 = Appliquer l'optimisation +GeneralOptimizationDialog.btn.apply.ttip = Appliquer les résultats de l'optimisation au design de la fusée +GeneralOptimizationDialog.btn.reset = Re-Réinitialiser +GeneralOptimizationDialog.btn.reset.ttip = Réinitialiser le design de la fusée au design actuel de la fusée +GeneralOptimizationDialog.btn.close = Fermer +GeneralOptimizationDialog.btn.close.ttip = Fermer la fenêtre de dialogue sans modifier la fusée +GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters. +GeneralOptimizationDialog.error.selectParams.title = Choisir les paramètres de l'optimisation +GeneralOptimizationDialog.error.optimizationFailure.text = L'optimisation n'a pas fonctionnée: +GeneralOptimizationDialog.error.optimizationFailure.title = L'optimisation n'a pas réussie +GeneralOptimizationDialog.undoText = Appliquer l'optimisation +GeneralOptimizationDialog.basicSimulationName = Simulation simple +GeneralOptimizationDialog.noSimulationName = Pas de simulation +GeneralOptimizationDialog.table.col.parameter = Paramètre +GeneralOptimizationDialog.table.col.current = Courant +GeneralOptimizationDialog.table.col.min = Minimum +GeneralOptimizationDialog.table.col.max = Maximum +GeneralOptimizationDialog.export.header = Inclure la ligne d'en tête +GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions. +GeneralOptimizationDialog.export.stability = Stabilité + + +! Dialog for plotting optimization results +OptimizationPlotDialog.title = Résultats de l'optimisation +OptimizationPlotDialog.lbl.zoomInstructions = Click et glisser en bas et à droite pour zoomer plus, en haut et à gauche pour zoomer moins +OptimizationPlotDialog.plot1d.title = Résultat de l'optimisation +OptimizationPlotDialog.plot1d.series = Résultat de l'optimisation +OptimizationPlotDialog.plot2d.title = Optimization path +OptimizationPlotDialog.plot2d.path = Chemin pour l'optimisation +OptimizationPlotDialog.plot2d.evals = Evaluations +OptimizationPlotDialog.plot.ttip.stability = Stabilité: +OptimizationPlotDialog.plot.label.optimum = Optimum + +! Optimization parameters +MaximumAltitudeParameter.name = Altitude de l'apogée +MaximumVelocityParameter.name = Vitesse maximum +MaximumAccelerationParameter.name = Accélération maximum +StabilityParameter.name = Stabilité +GroundHitVelocityParameter.name = Vitesse à l'atterrissage +LandingDistanceParameter.name = Distance à l'atterrissage +TotalFlightTimeParameter.name = Durée totale du vol +DeploymentVelocityParameter.name = Vitesse lors de l'ouverture du parachute + + +! Compass directions drawn on a compass rose. +CompassRose.lbl.north = N +CompassRose.lbl.east = E +CompassRose.lbl.south = S +CompassRose.lbl.west = O + +! 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 = SO +CompassSelectionButton.lbl.W = O +CompassSelectionButton.lbl.NW = NO + + +SlideShowDialog.btn.next = Suivant +SlideShowDialog.btn.prev = Précédent + +GuidedTourSelectionDialog.title = Tours d'horizon +GuidedTourSelectionDialog.lbl.selectTour = Choisir un tour d'horizon: +GuidedTourSelectionDialog.lbl.description = Description du tour d'horizon: +GuidedTourSelectionDialog.lbl.length = Nombre de diapositives: +GuidedTourSelectionDialog.btn.start = Commencer le tour d'horizon!