#
# English base translation file
#
+# Should you need to add new logical keys here is the proposed method
+#
+# className.ComponantType.componantName
+#
+
! Set to the name of the current translation file (used for debugging purposes)
debug.currentFile = messages.properties
+! RocketActions
+RocketActions.checkbox.Donotaskmeagain = Do not ask me again
+RocketActions.lbl.Youcanchangedefop = You can change the default operation in the preferences.
+RocketActions.showConfirmDialog.lbl1 = Delete the selected simulations?
+RocketActions.showConfirmDialog.lbl2 = <html><i>This operation cannot be undone.</i>
+RocketActions.showConfirmDialog.title = Delete simulations
+RocketActions.DelCompAct.Delete = Delete
+RocketActions.DelCompAct.ttip.Delete = Delete the selected component.
+RocketActions.DelSimuAct.Delete = Delete
+RocketActions.DelSimuAct.ttip.Delete = Delete the selected simulation.
+RocketActions.DelAct.Delete = Delete
+RocketActions.DelAct.ttip.Delete = Delete the selected component or simulation.
+RocketActions.CutAction.Cut = Cut
+RocketActions.CutAction.ttip.Cut = Cut this component or simulation to the clipboard and remove from this design
+RocketActions.CopyAct.Copy = Copy
+RocketActions.CopyAct.ttip.Copy = Copy this component (and subcomponents) to the clipboard.
+RocketActions.PasteAct.Paste = Paste
+RocketActions.PasteAct.ttip.Paste = Paste the component or simulation on the clipboard to the design.
+RocketActions.EditAct.Edit = Edit
+RocketActions.EditAct.ttip.Edit = Edit the selected component.
+RocketActions.NewStageAct.Newstage = New stage
+RocketActions.NewStageAct.ttip.Newstage = Add a new stage to the rocket design.
+RocketActions.ActBoosterstage = Booster stage
+RocketActions.MoveUpAct.Moveup = Move up
+RocketActions.MoveUpAct.ttip.Moveup = Move this component upwards.
+RocketActions.MoveDownAct.Movedown = Move down
+RocketActions.MoveDownAct.ttip.Movedown = Move this component downwards.
+
+! RocketPanel
+RocketPanel.FigTypeAct.Sideview = Side view
+RocketPanel.FigTypeAct.ttip.Sideview = Side view
+RocketPanel.FigTypeAct.Backview = Back view
+RocketPanel.FigTypeAct.ttip.Backview = Rear view
+RocketPanel.lbl.Motorcfg = Motor configuration:
+RocketPanel.lbl.infoMessage = <html>Click to select Shift+click to select other Double-click to edit Click+drag to move
+
+
+! BasicFrame
+BasicFrame.SimpleFileFilter1 = All rocket designs (*.ork; *.rkt)
+BasicFrame.SimpleFileFilter2 = OpenRocket designs (*.ork)
+BasicFrame.SimpleFileFilter3 = RockSim designs (*.rkt)
+BasicFrame.tab.Rocketdesign = Rocket design
+BasicFrame.tab.Flightsim = Flight simulations
+BasicFrame.title.Addnewcomp = Add new component
+BasicFrame.item.Openrocketdesign = Open a rocket design
+BasicFrame.item.Openexamplerocketdesign = Open an example rocket design
+BasicFrame.item.SavecurRocketdesign = Save the current rocket design
+BasicFrame.item.SavecurRocketdesnewfile = Save the current rocket design to a new file
+BasicFrame.item.Printpart = Print parts list and fin template
+BasicFrame.item.Closedesign = Close the current rocket design
+BasicFrame.item.Quitprogram = Quit the program
+BasicFrame.menu.Rocketedt = Rocket editing
+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
! Labels used in buttons of dialog windows
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.
+
+
+! Bug Report dialog
+bugreport.dlg.title = Bug report
+bugreport.dlg.but.Sendbugreport = Send bug report
+bugreport.dlg.but.Sendbugreport.Ttip = Automatically send the bug report to the OpenRocket developers.
+bugreport.dlg.successmsg1 = Bug report successfully sent.
+bugreport.dlg.successmsg2 = Thank you for helping make OpenRocket better!
+bugreport.dlg.successmsg3 = Bug report sent
+bugreport.dlg.connectedInternet = <html>If connected to the Internet, you can simply click <em>Send bug report</em>.
+bugreport.dlg.otherwise = Otherwise, send the text below to the address:
+bugreport.lbl.Theinformation = The information above may be included in a public bug report. Make sure it does not contain any sensitive information you do not want to be made public.
+bugreport.dlg.failedmsg1 = OpenRocket was unable to send the bug report:
+bugreport.dlg.failedmsg2 = Please send the report manually to
+bugreport.dlg.failedmsg3 = Error sending report
+bugreport.reportDialog.txt = <html><b>You can report a bug in OpenRocket by filling in and submitting the form below.</b><br>You can also report bugs and include attachments on the project web site.
+bugreport.reportDialog.txt2 = <html><b>Please include a short description about what you were doing when the exception occurred.</b>
+
+
+! 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:
+
+
+! Edit Motor configuration dialog
+edtmotorconfdlg.but.removemotor = Remove motor
+edtmotorconfdlg.but.Selectmotor = Select motor
+edtmotorconfdlg.but.Removeconfiguration = Remove configuration
+edtmotorconfdlg.but.Newconfiguration = New configuration
+edtmotorconfdlg.lbl.Motormounts = <html><b>Motor mounts:</b>
+edtmotorconfdlg.title.Editmotorconf = Edit motor configurations
+edtmotorconfdlg.selectcomp = <html>Select which components function as motor mounts:
+edtmotorconfdlg.lbl.Motorconfig = <html><b>Motor configurations:</b>
+edtmotorconfdlg.lbl.Configname = Configuration name:
+edtmotorconfdlg.lbl.Leavenamedefault = Leave name empty for default.
+
+! Example design dialog
+exdesigndlg.but.open = Open
+exdesigndlg.lbl.Selectexample = Select example designs to open:
+exdesigndlg.lbl.Openexampledesign = Open example design
+exdesigndlg.lbl.Exampledesignsnotfound = Example designs could not be found.
+exdesigndlg.lbl.Examplesnotfound = Examples not found
+
+
+! Material edit panel
+matedtpan.but.new = New
+matedtpan.but.edit = Edit
+matedtpan.but.delete = Delete
+matedtpan.but.revertall = Revert all
+matedtpan.col.Material = Material
+matedtpan.col.Type = Type
+matedtpan.col.Density = Density
+matedtpan.col.but.ttip.New = Add a new material
+matedtpan.title.Addcustmaterial = Add a custom material
+matedtpan.but.ttip.edit = Edit an existing material
+matedtpan.title.Editmaterial = Edit material
+matedtpan.title2.Editmaterial = The built-in materials cannot be modified.
+matedtpan.but.ttip.delete = Delete a user-defined material
+matedtpan.but.ttip.revertall = Delete all user-defined materials
+matedtpan.title.Deletealluser-defined = Delete all user-defined materials?
+matedtpan.title.Revertall = Revert all?
+matedtpan.lbl.edtmaterials = <html><i>Editing materials will not affect existing rocket designs.</i>
+
+!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.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.
+
+
+! Simulation edit dialog
+simedtdlg.but.runsimulation = Run simulation
+simedtdlg.but.resettodefault = Reset to default
+simedtdlg.but.add = Add
+simedtdlg.but.remove = Remove
+simedtdlg.title.Editsim = Edit simulation
+simedtdlg.lbl.Simname = Simulation name:
+simedtdlg.tab.Launchcond = Launch conditions
+simedtdlg.tab.Simopt = Simulation options
+simedtdlg.tab.Plotdata = Plot data
+simedtdlg.tab.Exportdata = Export data
+simedtdlg.lbl.Motorcfg = Motor configuration:
+simedtdlg.lbl.ttip.Motorcfg = Select the motor configuration to use.
+simedtdlg.combo.ttip.motorconf = Select the motor configuration to use.
+simedtdlg.lbl.Wind = Wind
+simedtdlg.lbl.Averwindspeed = Average windspeed:
+simedtdlg.lbl.ttip.Averwindspeed = The average windspeed relative to the ground.
+simedtdlg.lbl.Stddeviation = Standard deviation:
+simedtdlg.lbl.ttip.Stddeviation = <html>The standard deviation of the windspeed.<br>The windspeed is within twice the standard deviation from the average for 95% of the time.
+simedtdlg.lbl.Turbulenceintensity = Turbulence intensity:
+simedtdlg.lbl.ttip.Turbulenceintensity1 = <html>The turbulence intensity is the standard deviation divided by the average windspeed.<br>
+simedtdlg.lbl.ttip.Turbulenceintensity2 = Typical values range from
+simedtdlg.lbl.ttip.Turbulenceintensity3 = to
+simedtdlg.border.Atmoscond = Atmospheric conditions
+simedtdlg.checkbox.InterStdAtmosphere = Use International Standard Atmosphere
+simedtdlg.checkbox.ttip.InterStdAtmosphere1 = <html>Select to use the International Standard Atmosphere model.<br>This model has a temperature of
+simedtdlg.checkbox.ttip.InterStdAtmosphere2 = and a pressure of
+simedtdlg.checkbox.ttip.InterStdAtmosphere3 = at sea level.
+simedtdlg.lbl.Temperature = Temperature:
+simedtdlg.lbl.ttip.Temperature = The temperature at the launch site.
+simedtdlg.lbl.Pressure = Pressure:
+simedtdlg.lbl.ttip.Pressure = The atmospheric pressure at the launch site.
+simedtdlg.lbl.Launchsite = Launch site
+simedtdlg.lbl.Latitude = Latitude:
+simedtdlg.lbl.ttip.Latitude = <html>The launch site latitude affects the gravitational pull of Earth.<br>Positive values are on the Northern hemisphere, negative values on the Southern hemisphere.
+simedtdlg.lbl.Altitude = Altitude:
+simedtdlg.lbl.ttip.Altitude = <html>The launch altitude above mean sea level.<br>This affects the position of the rocket in the atmospheric model.
+simedtdlg.border.Launchrod = Launch rod
+simedtdlg.lbl.Length = Length:
+simedtdlg.lbl.ttip.Length = The length of the launch rod.
+simedtdlg.lbl.Angle = Angle:
+simedtdlg.lbl.ttip.Angle = The angle of the launch rod from vertical.
+simedtdlg.lbl.Direction = Direction:
+simedtdlg.lbl.ttip.Direction1 = <html>Direction of the launch rod relative to the wind.<br>
+simedtdlg.lbl.ttip.Direction2 = = towards the wind,
+simedtdlg.lbl.ttip.Direction3 = = downwind.
+simedtdlg.border.Simopt = Simulator options
+simedtdlg.lbl.Calcmethod = Calculation method:
+simedtdlg.lbl.ttip.Calcmethod = <html>The Extended Barrowman method calculates aerodynamic forces according <br>to the Barrowman equations extended to accommodate more components.
+simedtdlg.lbl.ExtBarrowman = Extended Barrowman
+simedtdlg.lbl.Simmethod = Simulation method:
+simedtdlg.lbl.ttip.Simmethod1 = <html>The six degree-of-freedom simulator allows the rocket total freedom during flight.<br>
+simedtdlg.lbl.ttip.Simmethod2 = Integration is performed using a 4<sup>th</sup> order Runge-Kutta 4 numerical integration.
+simedtdlg.lbl.Timestep = Time step:
+simedtdlg.lbl.ttip.Timestep1 = <html>The time between simulation steps.<br>A smaller time step results in a more accurate but slower simulation.<br>
+simedtdlg.lbl.ttip.Timestep2 = The 4<sup>th</sup> order simulation method is quite accurate with a time step of
+simedtdlg.but.ttip.resettodefault = Reset the time step to its default value (
+simedtdlg.border.Simlist = Simulator listeners
+simedtdlg.txt.longA1 = <html><i>Simulation listeners</i> is an advanced feature that allows user-written code to listen to and interact with the simulation.
+simedtdlg.txt.longA2 = For details on writing simulation listeners, see the OpenRocket technical documentation.
+simedtdlg.lbl.Curlist = Current listeners:
+simedtdlg.lbl.Addsimlist = Add simulation listener
+simedtdlg.lbl.Noflightdata = No flight data available.
+simedtdlg.lbl.runsimfirst = Please run the simulation first.
+simedtdlg.chart.Simflight = Simulated flight
+simedtdlg.dlg.Simres = Simulation results
+simedtdlg.IntensityDesc.None = None
+simedtdlg.IntensityDesc.Verylow = Very low
+simedtdlg.IntensityDesc.Low = Low
+simedtdlg.IntensityDesc.Medium = Medium
+simedtdlg.IntensityDesc.High = High
+simedtdlg.IntensityDesc.Veryhigh = Very high
+simedtdlg.IntensityDesc.Extreme = Extreme
+
+
+
+! Simulation Panel
+simpanel.but.newsimulation = New simulation
+simpanel.but.editsimulation = Edit simulation
+simpanel.but.runsimulations = Run simulations
+simpanel.but.deletesimulations = Delete simulations
+simpanel.but.plotexport = Plot / export
+simpanel.but.ttip.newsimulation = Add a new simulation
+simpanel.but.ttip.editsim = Edit the selected simulation
+simpanel.but.ttip.runsimu = Re-run the selected simulations
+simpanel.but.ttip.deletesim = Delete the selected simulations
+simpanel.checkbox.donotask = Do not ask me again
+simpanel.lbl.defpref = You can change the default operation in the preferences.
+simpanel.dlg.lbl.DeleteSim1 = Delete the selected simulations?
+simpanel.dlg.lbl.DeleteSim2 = <html><i>This operation cannot be undone.</i>
+simpanel.dlg.lbl.DeleteSim3 = Delete simulations
+simpanel.col.Name = Name
+simpanel.col.Motors = Motors
+simpanel.col.Apogee = Apogee
+simpanel.col.Maxvelocity = Max. velocity
+simpanel.col.Maxacceleration = Max. acceleration
+simpanel.col.Timetoapogee = Time to apogee
+simpanel.col.Flighttime = Flight time
+simpanel.col.Groundhitvelocity = Ground hit velocity
+
+! SimulationRunDialog
+SimuRunDlg.title.RunSim = Running simulations...
+SimuRunDlg.lbl.Running = Running ...
+SimuRunDlg.lbl.Simutime = Simulation time:
+SimuRunDlg.lbl.Altitude = Altitude:
+SimuRunDlg.lbl.Velocity = Velocity:
+SimuRunDlg.msg.Unabletosim = Unable to simulate:
+SimuRunDlg.msg.errorOccurred = An error occurred during the simulation:
+SimuRunDlg.msg.AnException1 = An exception occurred during the simulation:
+SimuRunDlg.msg.AnException2 = Please report this as a bug along with the details below.
+SimuRunDlg.msg.AssertionError1 = A computation error occurred during the simulation.
+SimuRunDlg.msg.AssertionError2 = Please report this as a bug along with the details below.
+SimuRunDlg.msg.unknownerror1 = An unknown error was encountered during the simulation.
+SimuRunDlg.msg.unknownerror2 = The program may be unstable, you should save all your designs and restart OpenRocket now!
+
+
+
+! SimulationExportPanel
+SimExpPan.desc = Comma Separated Files (*.csv)
+SimExpPan.border.Vartoexport = Variables to export
+SimExpPan.but.Selectall = Select all
+SimExpPan.but.Selectnone = Select none
+SimExpPan.border.Fieldsep = Field separator
+SimExpPan.lbl.Fieldsepstr = Field separator string:
+SimExpPan.lbl.longA1 = <html>The string used to separate the fields in the exported file.<br>
+SimExpPan.lbl.longA2 = Use ',' for a Comma Separated Values (CSV) file.
+SimExpPan.checkbox.Includesimudesc = Include simulation description
+SimExpPan.checkbox.ttip.Includesimudesc = Include a comment at the beginning of the file describing the simulation.
+SimExpPan.border.Comments = Comments
+SimExpPan.checkbox.Includefielddesc = Include field descriptions
+SimExpPan.checkbox.ttip.Includefielddesc = Include a comment line with the descriptions of the exported variables.
+SimExpPan.checkbox.Incflightevents = Include flight events
+SimExpPan.checkbox.ttip.Incflightevents = Include a comment line for every flight event.
+SimExpPan.lbl.Commentchar = Comment character:
+SimExpPan.lbl.ttip.Commentchar = The character(s) that mark a comment line.
+SimExpPan.but.Exporttofile = Export to file...
+SimExpPan.Fileexists.desc1 = File \"
+SimExpPan.Fileexists.desc2 = \" exists. Overwrite?
+SimExpPan.Fileexists.title = File exists
+SimExpPan.ExportingVar.desc1 = Exporting 1 variable out of
+SimExpPan.ExportingVar.desc2 = Exporting
+SimExpPan.ExportingVar.desc3 = variables out of
+SimExpPan.Col.Variable = Variable
+SimExpPan.Col.Unit = Unit
+
+! 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
+
+! Component add buttons
+compaddbuttons.Bodycompandfinsets = Body components and fin sets
+compaddbuttons.Nosecone = Nose cone
+compaddbuttons.Bodytube = Body tube
+compaddbuttons.Transition = Transition
+compaddbuttons.Trapezoidal = Trapezoidal
+compaddbuttons.Elliptical = Elliptical
+compaddbuttons.Freeform = Freeform
+compaddbuttons.Launchlug = Launch lug
+compaddbuttons.Innercomponent = Inner component
+compaddbuttons.Innertube = Inner tube
+compaddbuttons.Coupler = Coupler
+compaddbuttons.Centeringring = Centering\nring
+compaddbuttons.Bulkhead = Bulkhead
+compaddbuttons.Engineblock = Engine\nblock
+compaddbuttons.Massobjects = Mass objects
+compaddbuttons.Parachute = Parachute
+compaddbuttons.Streamer = Streamer
+compaddbuttons.Shockcord = Shock cord
+compaddbuttons.Masscomponent = Mass\ncomponent
+compaddbuttons.Donotaskmeagain = Do not ask me again
+compaddbuttons.Selectcomppos = Select component position
+compaddbuttons.lbl.Youcanchange = You can change the default operation in the preferences.
+compaddbuttons.lbl.insertcomp = Insert the component after the current component or as the last component?
+compaddbuttons.askPosition.Inserthere = Insert here
+compaddbuttons.askPosition.Addtotheend = Add to the end
+compaddbuttons.askPosition.Cancel = Cancel
+
+! Component Analysis Dialog
+componentanalysisdlg.componentanalysis = Component analysis
+componentanalysisdlg.lbl.winddir = Wind direction:
+componentanalysisdlg.TitledBorder.warnings = Warnings:
+componentanalysisdlg.ToggleBut.worst = Worst
+componentanalysisdlg.lbl.angleofattack = Angle of attack:
+componentanalysisdlg.lbl.machnumber = Mach number:
+componentanalysisdlg.lbl.rollrate = Roll rate:
+componentanalysisdlg.lbl.activestages = Active stages:
+componentanalysisdlg.lbl.motorconf = Motor configuration:
+componentanalysisdlg.TabStability.Col = Component
+componentanalysisdlg.TabStability = Stability
+componentanalysisdlg.TabStability.ttip = Stability information
+componentanalysisdlg.dragTableModel.Col.Component = Component
+componentanalysisdlg.dragTableModel.Col.Pressure = <html>Pressure C<sub>D</sub>
+componentanalysisdlg.dragTableModel.Col.Base = <html>Base C<sub>D</sub>
+componentanalysisdlg.dragTableModel.Col.friction = <html>Friction C<sub>D</sub>
+componentanalysisdlg.dragTableModel.Col.total = <html>Total C<sub>D</sub>
+componentanalysisdlg.dragTabchar = Drag characteristics
+componentanalysisdlg.dragTabchar.ttip = Drag characteristics
+componentanalysisdlg.rollTableModel.Col.component = Component
+componentanalysisdlg.rollTableModel.Col.rollforc = Roll forcing coefficient
+componentanalysisdlg.rollTableModel.Col.rolldamp = Roll damping coefficient
+componentanalysisdlg.rollTableModel.Col.total = <html>Total C<sub>l</sub>
+componentanalysisdlg.rollTableModel = Roll dynamics
+componentanalysisdlg.rollTableModel.ttip = Roll dynamics
+componentanalysisdlg.println.closingmethod = Closing method called:
+componentanalysisdlg.println.settingnam = SETTING NAN VALUES
+componentanalysisdlg.lbl.reflenght = Reference length:
+componentanalysisdlg.lbl.refarea = Reference area:
+!componentanalysisdlg.But.close =Close
+
+! Custom Material dialog
+custmatdlg.title.Custommaterial = Custom material
+custmatdlg.lbl.Materialname = Material name:
+custmatdlg.lbl.Materialtype = Material type:
+custmatdlg.lbl.Materialdensity = Material density:
+custmatdlg.checkbox.Addmaterial = Add material to database
+
+
+! Ring Component Config
+ringcompcfg.OuterRadius = OuterRadius
+ringcompcfg.Automatic = Automatic
+ringcompcfg.InnerRadius = InnerRadius
+ringcompcfg.Thickness = Thickness
+ringcompcfg.Length = Length
+ringcompcfg.Positionrelativeto = Position relative to:
+ringcompcfg.plus = plus
+ringcompcfg.PositionValue = PositionValue
+ringcompcfg.Radialdistance = Radial distance:
+ringcompcfg.Distancefrom = Distance from the rocket centerline
+ringcompcfg.Radialdirection = Radial direction
+ringcompcfg.radialdirectionfrom = The radial direction from the rocket centerline
+ringcompcfg.but.Reset = Reset
+ringcompcfg.but.Resetcomponant = Reset the component to the rocket centerline
+ringcompcfg.EngineBlock.desc = <html>An <b>engine block</b> stops the motor from moving forwards in the motor mount tube.<br><br>In order to add a motor, create a <b>body tube</b> or <b>inner tube</b> and mark it as a motor mount in the <em>Motor</em> tab.
+ringcompcfg.note.desc = Note: An inner tube will not affect the aerodynamics of the rocket even if it is located outside of the body tube.
+
+
+! Body Tube Config
+BodyTubecfg.lbl.Bodytubelength = Body tube length:
+BodyTubecfg.lbl.Outerdiameter = Outer diameter:
+BodyTubecfg.lbl.Innerdiameter = Inner diameter:
+BodyTubecfg.lbl.Wallthickness = Wall thickness:
+BodyTubecfg.tab.General = General
+BodyTubecfg.tab.Generalproperties = General properties
+BodyTubecfg.tab.Motor = Motor
+BodyTubecfg.tab.Motormountconf = Motor mount configuration
+BodyTubecfg.checkbox.Automatic = Automatic
+BodyTubecfg.checkbox.Filled = Filled
+
+! FinSetConfig
+FinSetConfig.tab.Fintabs = Fin tabs
+FinSetConfig.tab.Through-the-wall = Through-the-wall fin tabs
+FinSetConfig.but.Converttofreeform = Convert to freeform
+FinSetConfig.but.Converttofreeform.ttip = Convert this fin set into a freeform fin set
+FinSetConfig.Convertfinset = Convert fin set
+FinSetConfig.but.Splitfins = Split fins
+FinSetConfig.but.Splitfins.ttip = Split the fin set into separate fins
+FinSetConfig.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
+
+! MotorDatabaseLoadingDialog
+MotorDbLoadDlg.title = Loading motors
+MotorDbLoadDlg.Loadingmotors = Loading motors...
+
+! RocketConfig
+RocketCfg.lbl.Designname = Design name:
+RocketCfg.lbl.Designer = Designer:
+RocketCfg.lbl.Comments = Comments:
+RocketCfg.lbl.Revisionhistory = Revision history:
+RocketCfg.lbl.Material = Material:
+
+! ShockCordConfig
+ShockCordCfg.lbl.Shockcordlength = Shock cord length
+
+! RocketComponentConfig
+RocketCompCfg.lbl.Componentname = Component name:
+RocketCompCfg.ttip.Thecomponentname = The component name.
+RocketCompCfg.tab.Override = Override
+RocketCompCfg.tab.MassandCGoverride = Mass and CG override options
+RocketCompCfg.tab.Figure = Figure
+RocketCompCfg.tab.Figstyleopt = Figure style options
+RocketCompCfg.tab.Comment = Comment
+RocketCompCfg.tab.Specifyacomment = Specify a comment for the component
+RocketCompCfg.lbl.Mass = Mass:
+RocketCompCfg.lbl.Componentmass = Component mass:
+RocketCompCfg.lbl.overriddento = (overridden to
+RocketCompCfg.lbl.overriddenby = (overridden by
+RocketCompCfg.lbl.Componentmaterial = Component material:
+RocketCompCfg.lbl.Componentfinish = Component finish:
+RocketCompCfg.lbl.ttip.componentmaterialaffects = The component material affects the weight of the component.
+RocketCompCfg.combo.ttip.componentmaterialaffects = The component material affects the weight of the component.
+RocketCompCfg.lbl.longA1 = <html>The component finish affects the aerodynamic drag of the component.<br>
+RocketCompCfg.lbl.longA2 = The value indicated is the average roughness height of the surface.
+RocketCompCfg.but.Setforall = Set for all
+RocketCompCfg.but.ttip.Setforall = Set this finish for all components of the rocket.
+RocketCompCfg.lbl.Overridemassorcenter = Override the mass or center of gravity of the
+RocketCompCfg.checkbox.Overridemass = Override mass:
+RocketCompCfg.checkbox.Overridecenterofgrav = Override center of gravity:
+RocketCompCfg.checkbox.OverridemassandCG = Override mass and CG of all subcomponents
+RocketCompCfg.lbl.longB1 = <html>The overridden mass does not include motors.<br>
+RocketCompCfg.lbl.longB2 = The center of gravity is measured from the front end of the
+RocketCompCfg.lbl.Commentsonthe = Comments on the
+RocketCompCfg.lbl.Figurestyle = Figure style:
+RocketCompCfg.lbl.Componentcolor = Component color:
+RocketCompCfg.lbl.Choosecolor = Choose color
+RocketCompCfg.checkbox.Usedefaultcolor = Use default color
+RocketCompCfg.lbl.Complinestyle = Component line style:
+RocketCompCfg.but.Saveasdefstyle = Save as default style
+RocketCompCfg.lbl.Diameter = Diameter:
+RocketCompCfg.lbl.Length = Length:
+RocketCompCfg.lbl.Thickness = Thickness:
+RocketCompCfg.checkbox.Endcapped = End capped
+RocketCompCfg.ttip.Endcapped = Whether the end of the shoulder is capped.
+RocketCompCfg.title.Noseconeshoulder = Nose cone shoulder
+RocketCompCfg.title.Aftshoulder = Aft shoulder
+RocketCompCfg.border.Foreshoulder = Fore shoulder
+!RocketCompCfg.lbl.Length = Length:
+
+! BulkheadConfig
+BulkheadCfg.tab.Radius = Radius:
+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.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:
+
+!InnerTubeConfig
+InnerTubeCfg.tab.Motor = Motor
+InnerTubeCfg.tab.ttip.Motor = Motor mount configuration
+InnerTubeCfg.tab.Cluster = Cluster
+InnerTubeCfg.tab.ttip.Cluster = Cluster configuration
+InnerTubeCfg.tab.Radialpos = Radial position
+InnerTubeCfg.tab.ttip.Radialpos = Radial position
+InnerTubeCfg.lbl.Selectclustercfg = Select cluster configuration:
+InnerTubeCfg.lbl.TubeSep = Tube separation:
+InnerTubeCfg.lbl.ttip.TubeSep = The separation of the tubes, 1.0 = touching each other
+InnerTubeCfg.lbl.Rotation = Rotation:
+InnerTubeCfg.lbl.ttip.Rotation = Rotation angle of the cluster configuration
+InnerTubeCfg.lbl.Rotangle = Rotation angle of the cluster configuration
+InnerTubeCfg.but.Splitcluster = Split cluster
+InnerTubeCfg.lbl.longA1 = <html>Split the cluster into separate components.<br>
+InnerTubeCfg.lbl.longA2 = This also duplicates all components attached to this inner tube.
+InnerTubeCfg.but.Resetsettings = Reset settings
+InnerTubeCfg.but.ttip.Resetsettings = Reset the separation and rotation to the default values
+
+! LaunchLugConfig
+LaunchLugCfg.lbl.Length = Length:
+LaunchLugCfg.lbl.Outerdiam = Outer diameter:
+LaunchLugCfg.lbl.Innerdiam = Inner diameter:
+LaunchLugCfg.lbl.Thickness = Thickness:
+LaunchLugCfg.lbl.Radialpos = Radial position:
+LaunchLugCfg.lbl.Posrelativeto = Position relative to:
+LaunchLugCfg.lbl.plus = plus
+LaunchLugCfg.tab.General = General
+LaunchLugCfg.tab.Generalprop = General properties
+
+! MassComponentConfig
+MassComponentCfg.lbl.Mass = Mass
+MassComponentCfg.lbl.Length = Length
+MassComponentCfg.lbl.Diameter = Diameter
+MassComponentCfg.lbl.PosRelativeto = Position relative to:
+MassComponentCfg.lbl.plus = plus
+MassComponentCfg.tab.General = General
+MassComponentCfg.tab.ttip.General = General properties
+MassComponentCfg.tab.Radialpos = Radial position
+MassComponentCfg.tab.ttip.Radialpos = Radial position configuration
+MassComponentCfg.lbl.Radialdistance = Radial distance:
+MassComponentCfg.lbl.Radialdirection = Radial direction:
+MassComponentCfg.but.Reset = Reset
+
+! MotorConfig
+MotorCfg.checkbox.compmotormount = This component is a motor mount
+MotorCfg.lbl.Motorcfg = Motor configuration:
+MotorCfg.but.New = New
+MotorCfg.lbl.Currentmotor = Current motor:
+MotorCfg.lbl.Motoroverhang = Motor overhang:
+MotorCfg.lbl.Ignitionat = Ignition at:
+MotorCfg.lbl.plus = plus
+MotorCfg.lbl.seconds = seconds
+MotorCfg.lbl.longA1 = The current design has only one stage.
+MotorCfg.lbl.longA2 = Stages can be added by clicking \"New stage\".
+MotorCfg.lbl.longB1 = The current design has
+MotorCfg.lbl.longB2 = stages.
+MotorCfg.but.Selectmotor = Select motor
+MotorCfg.but.Removemotor = Remove motor
+MotorCfg.lbl.motorLabel = None
+
+! NoseConeConfig
+NoseConeCfg.lbl.Noseconeshape = Nose cone shape:
+NoseConeCfg.lbl.Shapeparam = Shape parameter:
+NoseConeCfg.lbl.Noseconelength = Nose cone length:
+NoseConeCfg.lbl.Basediam = Base diameter:
+NoseConeCfg.checkbox.Automatic = Automatic
+NoseConeCfg.lbl.Wallthickness = Wall thickness:
+NoseConeCfg.checkbox.Filled = Filled
+NoseConeCfg.tab.General = General
+NoseConeCfg.tab.ttip.General = General properties
+NoseConeCfg.tab.Shoulder = Shoulder
+NoseConeCfg.tab.ttip.Shoulder = Shoulder properties
+
+! ParachuteConfig
+ParachuteCfg.lbl.Canopy = Canopy:
+ParachuteCfg.lbl.Diameter = Diameter:
+ParachuteCfg.lbl.Material = Material:
+ParachuteCfg.combo.MaterialModel = The component material affects the weight of the component.
+ParachuteCfg.lbl.longA1 = <html>Drag coefficient C<sub>D</sub>:
+ParachuteCfg.lbl.longB1 = <html>The drag coefficient relative to the total area of the parachute.<br>
+ParachuteCfg.lbl.longB2 = A larger drag coefficient yields a slowed descent rate.
+ParachuteCfg.lbl.longB3 = A typical value for parachutes is 0.8.
+ParachuteCfg.but.Reset = Reset
+ParachuteCfg.lbl.Shroudlines = Shroud lines:
+ParachuteCfg.lbl.Numberoflines = Number of lines:
+ParachuteCfg.lbl.Linelength = Line length:
+ParachuteCfg.lbl.Material = Material:
+ParachuteCfg.lbl.Posrelativeto = Position relative to:
+ParachuteCfg.lbl.plus = plus
+ParachuteCfg.lbl.Packedlength = Packed length:
+ParachuteCfg.lbl.Packeddiam = Packed diameter:
+ParachuteCfg.lbl.Deploysat = Deploys at:
+ParachuteCfg.lbl.seconds = seconds
+ParachuteCfg.lbl.Altitude = Altitude:
+ParachuteCfg.tab.General = General
+ParachuteCfg.tab.ttip.General = General properties
+ParachuteCfg.tab.Radialpos = Radial position
+ParachuteCfg.tab.ttip.Radialpos = Radial position configuration
+ParachuteCfg.lbl.Radialdistance = Radial distance:
+ParachuteCfg.lbl.Radialdirection = Radial direction:
+ParachuteCfg.but.Reset = Reset
+
+! ShockCordConfig
+ShockCordCfg.lbl.Shockcordlength = Shock cord length
+ShockCordCfg.lbl.Shockcordmaterial = Shock cord material:
+ShockCordCfg.lbl.Posrelativeto = Position relative to:
+ShockCordCfg.lbl.plus = plus
+ShockCordCfg.lbl.Packedlength = Packed length:
+ShockCordCfg.lbl.Packeddiam = Packed diameter:
+ShockCordCfg.tab.General = General
+ShockCordCfg.tab.ttip.General = General properties
+
+!SleeveConfig
+SleeveCfg.tab.Outerdiam = Outer diameter:
+SleeveCfg.tab.Innerdiam = Inner diameter:
+SleeveCfg.tab.Wallthickness = Wall thickness:
+SleeveCfg.tab.Length = Length:
+SleeveCfg.tab.General = General
+SleeveCfg.tab.Generalproperties = General properties
+
+! StreamerConfig
+StreamerCfg.lbl.Striplength = Strip length:
+StreamerCfg.lbl.Stripwidth = Strip width:
+StreamerCfg.lbl.Striparea = Strip area:
+StreamerCfg.lbl.Aspectratio = Aspect ratio:
+StreamerCfg.lbl.Material = Material:
+StreamerCfg.combo.ttip.MaterialModel = The component material affects the weight of the component.
+StreamerCfg.lbl.longA1 = <html>Drag coefficient C<sub>D</sub>:
+StreamerCfg.lbl.longB1 = <html>The drag coefficient relative to the total area of the streamer.<br>
+StreamerCfg.lbl.longB2 = A larger drag coefficient yields a slowed descent rate.
+StreamerCfg.lbl.Automatic = Automatic
+StreamerCfg.lbl.longC1 = The drag coefficient is relative to the area of the streamer.
+StreamerCfg.lbl.Posrelativeto = Position relative to:
+StreamerCfg.lbl.plus = plus
+StreamerCfg.lbl.Packedlength = Packed length:
+StreamerCfg.lbl.Packeddiam = Packed diameter:
+StreamerCfg.lbl.Deploysat = Deploys at:
+StreamerCfg.lbl.seconds = seconds
+StreamerCfg.lbl.Altitude = Altitude:
+StreamerCfg.tab.General = General
+StreamerCfg.tab.ttip.General = General properties
+StreamerCfg.tab.Radialpos = Radial position
+StreamerCfg.tab.ttip.Radialpos = Radial position configuration
+StreamerCfg.lbl.Radialdistance = Radial distance:
+StreamerCfg.lbl.Radialdirection = Radial direction:
+StreamerCfg.but.Reset = Reset
+
+! ThicknessRingComponentConfig
+ThicknessRingCompCfg.tab.Outerdiam = Outer diameter:
+ThicknessRingCompCfg.tab.Innerdiam = Inner diameter:
+ThicknessRingCompCfg.tab.Wallthickness = Wall thickness:
+ThicknessRingCompCfg.tab.Length = Length:
+ThicknessRingCompCfg.tab.General = General
+ThicknessRingCompCfg.tab.Generalprop = General properties
+
+! TransitionConfig
+TransitionCfg.lbl.Transitionshape = Transition shape:
+TransitionCfg.checkbox.Clipped = Clipped
+TransitionCfg.lbl.Shapeparam = Shape parameter:
+TransitionCfg.lbl.Transitionlength = Transition length:
+TransitionCfg.lbl.Forediam = Fore diameter:
+TransitionCfg.checkbox.Automatic = Automatic
+TransitionCfg.lbl.Aftdiam = Aft diameter:
+TransitionCfg.lbl.Wallthickness = Wall thickness:
+TransitionCfg.checkbox.Filled = Filled
+TransitionCfg.tab.General = General
+TransitionCfg.tab.Generalproperties = General properties
+TransitionCfg.tab.Shoulder = Shoulder
+TransitionCfg.tab.Shoulderproperties = Shoulder properties
+
+! TrapezoidFinSetConfig
+TrapezoidFinSetCfg.lbl.Nbroffins = Number of fins:
+TrapezoidFinSetCfg.lbl.ttip.Nbroffins = The number of fins in the fin set.
+TrapezoidFinSetCfg.lbl.Finrotation = Fin rotation:
+TrapezoidFinSetCfg.lbl.ttip.Finrotation = The angle of the first fin in the fin set.
+TrapezoidFinSetCfg.lbl.Fincant = Fin cant:
+TrapezoidFinSetCfg.lbl.ttip.Fincant =The angle that the fins are canted with respect to the rocket body.
+TrapezoidFinSetCfg.lbl.Rootchord = Root chord:
+TrapezoidFinSetCfg.lbl.Tipchord = Tip chord:
+TrapezoidFinSetCfg.lbl.Height = Height:
+TrapezoidFinSetCfg.lbl.Sweeplength = Sweep length:
+TrapezoidFinSetCfg.lbl.Sweepangle = Sweep angle:
+TrapezoidFinSetCfg.lbl.FincrossSection = Fin cross section:
+TrapezoidFinSetCfg.lbl.Thickness = Thickness:
+TrapezoidFinSetCfg.lbl.Posrelativeto = Position relative to:
+TrapezoidFinSetCfg.lbl.plus = plus
+TrapezoidFinSetCfg.tab.General = General
+TrapezoidFinSetCfg.tab.Generalproperties = General properties
+
+!MotorConfigurationModel
+MotorCfgModel.Editcfg = Edit configurations
+
+! StorageOptionChooser
+StorageOptChooser.lbl.Simdatatostore = Simulated data to store:
+StorageOptChooser.rdbut.Allsimdata = All simulated data
+StorageOptChooser.lbl.longA1 = <html>Store all simulated data.<br>
+StorageOptChooser.lbl.longA2 = This can result in very large files!
+StorageOptChooser.rdbut.Every = Every
+StorageOptChooser.lbl.longB1 = <html>Store plottable values approximately this far apart.<br>
+StorageOptChooser.lbl.longB2 = Larger values result in smaller files.
+StorageOptChooser.lbl.seconds = seconds
+StorageOptChooser.rdbut.Onlyprimfig = Only primary figures
+StorageOptChooser.lbl.longC1 = <html>Store only the values shown in the summary table.<br>
+StorageOptChooser.lbl.longC2 = This results in the smallest files.
+StorageOptChooser.checkbox.Compfile = Compress file
+StorageOptChooser.lbl.UsingComp = Using compression reduces the file size significantly.
+StorageOptChooser.lbl.longD1 = An estimate on how large the resulting file would be with the present options.
+StorageOptChooser.ttip.Saveopt = Save options
+StorageOptChooser.lbl.Estfilesize = Estimated file size:
+StorageOptChooser.lbl.Saveopt = Save options
+
+! ThrustCurveMotorSelectionPanel
+TCMotorSelPan.lbl.Selrocketmotor = Select rocket motor:
+TCMotorSelPan.checkbox.hideSimilar = Hide very similar thrust curves
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Show all motors
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Show motors with diameter less than that of the motor mount
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Show motors with diameter equal to that of the motor mount
+TCMotorSelPan.lbl.Motormountdia = Motor mount diameter:
+TCMotorSelPan.lbl.Search = Search:
+TCMotorSelPan.lbl.Selectthrustcurve = Select thrust curve:
+TCMotorSelPan.lbl.Ejectionchargedelay = Ejection charge delay:
+TCMotorSelPan.equalsIgnoreCase.None = None
+TCMotorSelPan.lbl.NumberofsecondsorNone = (Number of seconds or \"None\")
+TCMotorSelPan.lbl.Totalimpulse = Total impulse:
+TCMotorSelPan.lbl.Avgthrust = Avg. thrust:
+TCMotorSelPan.lbl.Maxthrust = Max. thrust:
+TCMotorSelPan.lbl.Burntime = Burn time:
+TCMotorSelPan.lbl.Launchmass = Launch mass:
+TCMotorSelPan.lbl.Emptymass = Empty mass:
+TCMotorSelPan.lbl.Datapoints = Data points:
+TCMotorSelPan.lbl.Digest = Digest:
+TCMotorSelPan.title.Thrustcurve = Thrust curve:
+TCMotorSelPan.title.Thrust = Thrust
+TCMotorSelPan.delayBox.None = None
+
+
+! PlotDialog
+PlotDialog.title.Flightdataplot = Flight data plot
+PlotDialog.Chart.Simulatedflight = Simulated flight
+PlotDialog.CheckBox.Showdatapoints = Show data points
+PlotDialog.lbl.Chart = Click+drag down+right to zoom in, up+left to zoom out
+
! "main" prefix is used for the main application dialog
main.menu.file.openExample = Open example...
main.menu.file.save = Save
main.menu.file.saveAs = Save as...
+main.menu.file.print = Print / Export PDF...
main.menu.file.close = Close
main.menu.file.quit = Quit
main.menu.help.license = License
main.menu.help.bugReport = Bug report
main.menu.help.debugLog = Debug log
-main.menu.help. = About
+main.menu.help.about = About
+
+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.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
+!SURFACE_MATERIAL
+Databases.materials.Ripstopnylon = Ripstop nylon
+Databases.materials.Mylar = Mylar
+Databases.materials.Polyethylenethin = Polyethylene (thin)
+Databases.materials.Polyethyleneheavy = Polyethylene (heavy)
+Databases.materials.Silk = Silk
+Databases.materials.Paperoffice = Paper (office)
+Databases.materials.Cellophane = Cellophane
+Databases.materials.Crepepaper = Cr\u00eape paper
+! LINE_MATERIAL
+Databases.materials.Threadheavy-duty = Thread (heavy-duty)
+Databases.materials.Elasticcordround2mm = Elastic cord (round 2mm, 1/16 in)
+Databases.materials.Elasticcordflat6mm = Elastic cord (flat 6mm, 1/4 in)
+Databases.materials.Elasticcordflat12mm = Elastic cord (flat 12mm, 1/2 in)
+Databases.materials.Elasticcordflat19mm = Elastic cord (flat 19mm, 3/4 in)
+Databases.materials.Elasticcordflat25mm = Elastic cord (flat 25mm, 1 in)
+Databases.materials.Braidednylon2mm = Braided nylon (2 mm, 1/16 in)
+Databases.materials.Braidednylon3mm = Braided nylon (3 mm, 1/8 in)
+Databases.materials.Tubularnylon11mm = Tubular nylon (11 mm, 7/16 in)
+Databases.materials.Tubularnylon14mm = Tubular nylon (14 mm, 9/16 in)
+Databases.materials.Tubularnylon25mm = Tubular nylon (25 mm, 1 in)
+
+! ExternalComponent
+ExternalComponent.Rough = Rough
+ExternalComponent.Unfinished = Unfinished
+ExternalComponent.Regularpaint = Regular paint
+ExternalComponent.Smoothpaint = Smooth paint
+ExternalComponent.Polished = Polished
+
+! LineStyle
+LineStyle.Solid = Solid
+LineStyle.Dashed = Dashed
+LineStyle.Dotted = Dotted
+LineStyle.Dash-dotted = Dash-dotted
+LineStyle.Defaultstyle = Default style
+
+! Shape
+Shape.Conical = Conical
+Shape.Conical.desc1 = A conical nose cone has a profile of a triangle.
+Shape.Conical.desc2 = A conical transition has straight sides.
+Shape.Ogive = Ogive
+Shape.Ogive.desc1 = An ogive nose cone has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube, values less than 1 produce <b>secant ogives</b>.
+Shape.Ogive.desc2 = An ogive transition has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube at the aft end, values less than 1 produce <b>secant ogives</b>.
+Shape.Ellipsoid = Ellipsoid
+Shape.Ellipsoid.desc1 = An ellipsoidal nose cone has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>.
+Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>. If the transition is not clipped, then the profile is extended at the center by the corresponding radius.
+Shape.Powerseries = Power series
+Shape.Powerseries.desc1 = A power series nose cone has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 this is a <b>\u00BD-power</b> or <b>parabolic</b> nose cone, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 a <b>conical</b> nose cone.
+Shape.Powerseries.desc2 = A power series transition has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 the transition is <b>\u00BD-power</b> or <b>parabolic</b>, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 <b>conical</b>.
+Shape.Parabolicseries = Parabolic series
+Shape.Parabolicseries.desc1 = A parabolic series nose cone has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> nose cone.
+Shape.Parabolicseries.desc2 = A parabolic series transition has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube at the aft end, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> transition.
+Shape.Haackseries = Haack series
+Shape.Haackseries.desc1 = The Haack series nose cones are designed to minimize drag. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> nose cone, which minimizes drag for fixed length and diameter, while a value of 0.333 produces an <b>LV-Haack</b> nose cone, which minimizes drag for fixed length and volume.
+Shape.Haackseries.desc2 = The Haack series <i>nose cones</i> are designed to minimize drag. These transition shapes are their equivalents, but do not necessarily produce optimal drag for transitions. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> shape, while a value of 0.333 produces an <b>LV-Haack</b> shape.
+
+
+! RocketComponent
+RocketComponent.Position.TOP = Top of the parent component
+RocketComponent.Position.MIDDLE = Middle of the parent component
+RocketComponent.Position.BOTTOM = Bottom of the parent component
+RocketComponent.Position.AFTER = After the parent component
+RocketComponent.Position.ABSOLUTE = Tip of the nose cone
+
+! LaunchLug
+LaunchLug.Launchlug = Launch lug
+! NoseCone
+NoseCone.NoseCone = Nose cone
+! Transition
+Transition.Transition = Transition
+!Stage
+Stage.Stage = Stage
+! BodyTube
+BodyTube.BodyTube = Body tube
+! TubeCoupler
+TubeCoupler.TubeCoupler = Tube coupler
+!InnerTube
+InnerTube.InnerTube = Inner Tube
+! TrapezoidFinSet
+TrapezoidFinSet.TrapezoidFinSet = Trapezoidal fin set
+! FreeformFinSet
+FreeformFinSet.FreeformFinSet = Freeform fin set
+!MassComponent
+MassComponent.MassComponent = Mass component
+! Parachute
+Parachute.Parachute = Parachute
+! ShockCord
+ShockCord.ShockCord = Shock cord
+! Bulkhead
+Bulkhead.Bulkhead = Bulkhead
+
+!Rocket
+Rocket.motorCount.Nomotor = [No motors]
+Rocket.compname.Rocket = Rocket
+
+!MotorMount
+MotorMount.IgnitionEvent.AUTOMATIC = Automatic (launch or ejection charge)
+MotorMount.IgnitionEvent.LAUNCH = Launch
+MotorMount.IgnitionEvent.EJECTION_CHARGE = First ejection charge of previous stage
+MotorMount.IgnitionEvent.BURNOUT = First burnout of previous stage
+MotorMount.IgnitionEvent.NEVER = Never
+
+!ComponentIcons
+ComponentIcons.Nosecone = Nose cone
+ComponentIcons.Bodytube = Body tube
+ComponentIcons.Transition = Transition
+ComponentIcons.Trapezoidalfinset = Trapezoidal fin set
+ComponentIcons.Ellipticalfinset = Elliptical fin set
+ComponentIcons.Freeformfinset = Freeform fin set
+ComponentIcons.Launchlug = Launch lug
+ComponentIcons.Innertube = Inner tube
+ComponentIcons.Tubecoupler = Tube coupler
+ComponentIcons.Centeringring = Centering ring
+ComponentIcons.Bulkhead = Bulk head
+ComponentIcons.Engineblock = Engine block
+ComponentIcons.Parachute = Parachute
+ComponentIcons.Streamer = Streamer
+ComponentIcons.Shockcord = Shock cord
+ComponentIcons.Masscomponent = Mass component
+ComponentIcons.disabled = (disabled)
+
+! StageAction
+StageAction.Stage = Stage
+
+! RecoveryDevice
+RecoveryDevice.DeployEvent.LAUNCH = Launch (plus NN seconds)
+RecoveryDevice.DeployEvent.EJECTION = First ejection charge of this stage
+RecoveryDevice.DeployEvent.APOGEE = Apogee
+RecoveryDevice.DeployEvent.ALTITUDE = Specific altitude during descent
+RecoveryDevice.DeployEvent.NEVER = Never
+
+! FlightEvent
+FlightEvent.Type.LAUNCH = Launch
+FlightEvent.Type.IGNITION = Motor ignition
+FlightEvent.Type.LIFTOFF = Lift-off
+FlightEvent.Type.LAUNCHROD = Launch rod clearance
+FlightEvent.Type.BURNOUT = Motor burnout
+FlightEvent.Type.EJECTION_CHARGE = Ejection charge
+FlightEvent.Type.STAGE_SEPARATION = Stage separation
+FlightEvent.Type.APOGEE = Apogee
+FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Recovery device deployment
+FlightEvent.Type.GROUND_HIT = Ground hit
+FlightEvent.Type.SIMULATION_END = Simulation end
+FlightEvent.Type.ALTITUDE = Altitude change
+
+! ThrustCurveMotorColumns
+TCurveMotorCol.MANUFACTURER = Manufacturer
+TCurveMotorCol.DESIGNATION = Designation
+TCurveMotorCol.TYPE = Type
+TCurveMotorCol.DIAMETER = Diameter
+TCurveMotorCol.LENGTH = Length
+
+! RocketInfo
+RocketInfo.lengthLine.Length = Length
+RocketInfo.lengthLine.maxdiameter = , max. diameter
+RocketInfo.massText1 = Mass with motors
+RocketInfo.massText2 = Mass with no motors
+RocketInfo.at = at M=
+RocketInfo.cgText = CG:
+RocketInfo.cpText = CP:
+RocketInfo.stabText = Stability:
+RocketInfo.Warning = Warning:
+RocketInfo.Calculating = Calculating...
+RocketInfo.Apogee = Apogee:
+RocketInfo.Maxvelocity = Max. velocity:
+RocketInfo.Maxacceleration = Max. acceleration:
+RocketInfo.apogeeValue = N/A
+RocketInfo.Mach = (Mach
+RocketInfo.velocityValue = N/A
+RocketInfo.accelerationValue = N/A
+
+! FinSet
+FinSet.CrossSection.SQUARE = Square
+FinSet.CrossSection.ROUNDED = Rounded
+FinSet.CrossSection.AIRFOIL = Airfoil
+FinSet.TabRelativePosition.FRONT = Root chord leading edge
+FinSet.TabRelativePosition.CENTER = Root chord midpoint
+FinSet.TabRelativePosition.END = Root chord trailing edge
+! FlightDataType
+FlightDataType.TYPE_TIME = Time
+FlightDataType.TYPE_ALTITUDE = Altitude
+FlightDataType.TYPE_VELOCITY_Z = Vertical velocity
+FlightDataType.TYPE_ACCELERATION_Z = Vertical acceleration
+FlightDataType.TYPE_VELOCITY_TOTAL = Total velocity
+FlightDataType.TYPE_ACCELERATION_TOTAL = Total acceleration
+FlightDataType.TYPE_POSITION_X = Position upwind
+FlightDataType.TYPE_POSITION_Y = Position parallel to wind
+FlightDataType.TYPE_POSITION_XY = Lateral distance
+FlightDataType.TYPE_POSITION_DIRECTION = Lateral direction
+FlightDataType.TYPE_VELOCITY_XY = Lateral velocity
+FlightDataType.TYPE_ACCELERATION_XY = Lateral acceleration
+FlightDataType.TYPE_AOA = Angle of attack
+FlightDataType.TYPE_ROLL_RATE = Roll rate
+FlightDataType.TYPE_PITCH_RATE = Pitch rate
+FlightDataType.TYPE_YAW_RATE = Yaw rate
+FlightDataType.TYPE_MASS = Mass
+FlightDataType.TYPE_LONGITUDINAL_INERTIA = Longitudinal moment of inertia
+FlightDataType.TYPE_ROTATIONAL_INERTIA = Rotational moment of inertia
+FlightDataType.TYPE_CP_LOCATION = CP location
+FlightDataType.TYPE_CG_LOCATION = CG location
+FlightDataType.TYPE_STABILITY = Stability margin calibers
+FlightDataType.TYPE_MACH_NUMBER = Mach number
+FlightDataType.TYPE_REYNOLDS_NUMBER = Reynolds number
+FlightDataType.TYPE_THRUST_FORCE = Thrust
+FlightDataType.TYPE_DRAG_FORCE = Drag force
+FlightDataType.TYPE_DRAG_COEFF = Drag coefficient
+FlightDataType.TYPE_AXIAL_DRAG_COEFF = Axial drag coefficient
+FlightDataType.TYPE_FRICTION_DRAG_COEFF = Friction drag coefficient
+FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Pressure drag coefficient
+FlightDataType.TYPE_BASE_DRAG_COEFF = Base drag coefficient
+FlightDataType.TYPE_NORMAL_FORCE_COEFF = Normal force coefficient
+FlightDataType.TYPE_PITCH_MOMENT_COEFF = Pitch moment coefficient
+FlightDataType.TYPE_YAW_MOMENT_COEFF = Yaw moment coefficient
+FlightDataType.TYPE_SIDE_FORCE_COEFF = Side force coefficient
+FlightDataType.TYPE_ROLL_MOMENT_COEFF = Roll moment coefficient
+FlightDataType.TYPE_ROLL_FORCING_COEFF = Roll forcing coefficient
+FlightDataType.TYPE_ROLL_DAMPING_COEFF = Roll damping coefficient
+FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Pitch damping coefficient
+FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Yaw damping coefficient
+FlightDataType.TYPE_REFERENCE_LENGTH = Reference lenght
+FlightDataType.TYPE_REFERENCE_AREA = Reference area
+FlightDataType.TYPE_ORIENTATION_THETA = Vertical orientation (zenith)
+FlightDataType.TYPE_ORIENTATION_PHI = Lateral orientation (azimuth)
+FlightDataType.TYPE_WIND_VELOCITY = Wind velocity
+FlightDataType.TYPE_AIR_TEMPERATURE = Air temperature
+FlightDataType.TYPE_AIR_PRESSURE = Air pressure
+FlightDataType.TYPE_SPEED_OF_SOUND = Speed of sound
+FlightDataType.TYPE_TIME_STEP = Simulation time step
+FlightDataType.TYPE_COMPUTATION_TIME = Computation time
+! 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.
projects / debian / openrocket / blobdiff