c3cfb2e781
Added l10n message keys for new column in SimulationPanel. Added function MathUtil.interpolate which does linear interpolation of intermediate values. This is used in FlightData for computing Velocity at deployment and Velocity at launch rod clearance.
1549 lines
74 KiB
Properties
1549 lines
74 KiB
Properties
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#
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# English base translation file
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#
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# Should you need to add new logical keys here is the proposed method
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#
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# className.ComponentType.componentName
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#
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#
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# Text tokens within braces should not be translated, e.g.
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# "The file '{filename}' exists."
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# They are pieces that are inserted dynamically.
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#
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! Set to the name of the current translation file (used for debugging purposes)
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debug.currentFile = messages.properties
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! RocketActions
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RocketActions.checkbox.Donotaskmeagain = Do not ask me again
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RocketActions.lbl.Youcanchangedefop = You can change the default operation in the preferences.
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RocketActions.showConfirmDialog.lbl1 = Delete the selected simulations?
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RocketActions.showConfirmDialog.lbl2 = <html><i>This operation cannot be undone.</i>
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RocketActions.showConfirmDialog.title = Delete simulations
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RocketActions.DelCompAct.Delete = Delete
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RocketActions.DelCompAct.ttip.Delete = Delete the selected component.
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RocketActions.DelSimuAct.Delete = Delete
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RocketActions.DelSimuAct.ttip.Delete = Delete the selected simulation.
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RocketActions.DelAct.Delete = Delete
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RocketActions.DelAct.ttip.Delete = Delete the selected component or simulation.
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RocketActions.CutAction.Cut = Cut
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RocketActions.CutAction.ttip.Cut = Cut this component or simulation to the clipboard and remove from this design
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RocketActions.CopyAct.Copy = Copy
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RocketActions.CopyAct.ttip.Copy = Copy this component (and subcomponents) to the clipboard.
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RocketActions.PasteAct.Paste = Paste
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RocketActions.PasteAct.ttip.Paste = Paste the component or simulation on the clipboard to the design.
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RocketActions.EditAct.Edit = Edit
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RocketActions.EditAct.ttip.Edit = Edit the selected component.
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RocketActions.NewStageAct.Newstage = New stage
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RocketActions.NewStageAct.ttip.Newstage = Add a new stage to the rocket design.
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RocketActions.ActBoosterstage = Booster stage
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RocketActions.MoveUpAct.Moveup = Move up
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RocketActions.MoveUpAct.ttip.Moveup = Move this component upwards.
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RocketActions.MoveDownAct.Movedown = Move down
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RocketActions.MoveDownAct.ttip.Movedown = Move this component downwards.
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! RocketPanel
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RocketPanel.FigTypeAct.Sideview = Side view
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RocketPanel.FigTypeAct.ttip.Sideview = Side view
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RocketPanel.FigTypeAct.Backview = Back view
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RocketPanel.FigTypeAct.ttip.Backview = Rear view
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RocketPanel.lbl.Motorcfg = Motor configuration:
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RocketPanel.lbl.infoMessage = <html>Click to select Shift+click to select other Double-click to edit Click+drag to move
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! BasicFrame
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BasicFrame.SimpleFileFilter1 = All rocket designs (*.ork; *.rkt)
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BasicFrame.SimpleFileFilter2 = OpenRocket designs (*.ork)
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BasicFrame.SimpleFileFilter3 = RockSim designs (*.rkt)
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BasicFrame.tab.Rocketdesign = Rocket design
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BasicFrame.tab.Flightsim = Flight simulations
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BasicFrame.title.Addnewcomp = Add new component
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BasicFrame.dlg.lbl1 = Design '
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BasicFrame.dlg.lbl2 = ' has not been saved.
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BasicFrame.dlg.lbl3 = Do you want to save it?
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BasicFrame.dlg.title = Design not saved
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BasicFrame.StageName.Sustainer = Sustainer
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BasicFrame.WarningDialog.txt1 = The following problems were encountered while opening
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BasicFrame.WarningDialog.txt2 = Some design features may not have been loaded correctly.
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BasicFrame.WarningDialog.title = Warnings while opening file
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! General error messages used in multiple contexts
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error.fileExists.title = File exists
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error.fileExists.desc = File '{filename}' exists. Do you want to overwrite it?
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error.writing.title = Error writing file
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error.writing.desc = An error occurred while writing to the file:
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! Labels used in buttons of dialog windows
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# TODO: Rename these to "btn.xxx"
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button.ok = OK
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button.cancel = Cancel
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button.close = Close
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! Common labels used in buttons of dialog windows
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dlg.but.ok = OK
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dlg.but.cancel = Cancel
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dlg.but.close = Close
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! General file type names
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filetypes.pdf = PDF files
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! About Dialog
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AboutDialog.lbl.version = Version
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! The texts below provide additional credits for the translation maintainer
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! - In AboutDialog.lbl.translation replace "English" with the current language.
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! - AboutDialog.lbl.translator is the translator / group name (may be empty)
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! - AboutDialog.lbl.translatorWebsite is a URL to the translator / group (may be empty)
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! - AboutDialog.lbl.translatorIcon is the file name of an icon under pix/translators/ (may be empty)
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AboutDialog.lbl.translation = English translation by:
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AboutDialog.lbl.translator =
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AboutDialog.lbl.translatorWebsite =
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AboutDialog.lbl.translatorIcon =
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! Print dialog
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PrintDialog.title = Print or export
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PrintDialog.but.previewAndPrint = Preview & Print
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PrintDialog.checkbox.showByStage = Show by stage
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PrintDialog.lbl.selectElements = Select elements to include:
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printdlg.but.saveaspdf = Save as PDF
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printdlg.but.preview = Preview
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printdlg.but.settings = Settings
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PrintDialog.error.preview.title = Unable to open preview
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PrintDialog.error.preview.desc1 = Unable to open PDF preview.
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PrintDialog.error.preview.desc2 = Please use the "Save as PDF" option instead.
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!PrintSettingsDialog
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PrintSettingsDialog.title = Print settings
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PrintSettingsDialog.lbl.Templatefillcolor = Template fill color:
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PrintSettingsDialog.lbl.Templatebordercolor = Template border color:
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PrintSettingsDialog.lbl.Papersize = Paper size:
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PrintSettingsDialog.lbl.Paperorientation = Paper orientation:
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PrintSettingsDialog.but.Reset = Reset
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PrintSettingsDialog.but.Close = Close
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! Bug Report dialog
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bugreport.dlg.title = Bug report
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bugreport.dlg.but.Sendbugreport = Send bug report
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bugreport.dlg.but.Sendbugreport.Ttip = Automatically send the bug report to the OpenRocket developers.
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bugreport.dlg.successmsg1 = Bug report successfully sent.
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bugreport.dlg.successmsg2 = Thank you for helping make OpenRocket better!
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bugreport.dlg.successmsg3 = Bug report sent
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bugreport.dlg.connectedInternet = <html>If connected to the Internet, you can simply click <em>Send bug report</em>.
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bugreport.dlg.otherwise = Otherwise, send the text below to the address:
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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.
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bugreport.dlg.failedmsg1 = OpenRocket was unable to send the bug report:
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bugreport.dlg.failedmsg2 = Please send the report manually to
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bugreport.dlg.failedmsg3 = Error sending report
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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.
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bugreport.reportDialog.txt2 = <html><b>Please include a short description about what you were doing when the exception occurred.</b>
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bugreport.dlg.provideDescription = Please provide a description of the bug first.
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bugreport.dlg.provideDescription.title = Bug description missing
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! Debug log dialog
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debuglogdlg.but.clear = Clear
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debuglogdlg.OpenRocketdebuglog = OpenRocket debug log
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debuglogdlg.Displayloglines = Display log lines:
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debuglogdlg.Follow = Follow
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debuglogdlg.col.Time = Time
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debuglogdlg.col.Level = Level
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debuglogdlg.col.Location = Location
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debuglogdlg.col.Message = Message
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debuglogdlg.lbl.Loglinenbr = Log line number:
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debuglogdlg.lbl.Time = Time:
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debuglogdlg.lbl.Level = Level:
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debuglogdlg.lbl.Location = Location:
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debuglogdlg.lbl.Logmessage = Log message:
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debuglogdlg.lbl.Stacktrace = Stack trace:
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! Edit Motor configuration dialog
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edtmotorconfdlg.but.removemotor = Remove motor
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edtmotorconfdlg.but.Selectmotor = Select motor
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edtmotorconfdlg.but.Removeconfiguration = Remove configuration
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edtmotorconfdlg.but.Newconfiguration = New configuration
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edtmotorconfdlg.lbl.Motormounts = <html><b>Motor mounts:</b>
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edtmotorconfdlg.title.Editmotorconf = Edit motor configurations
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edtmotorconfdlg.selectcomp = <html>Select which components function as motor mounts:
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edtmotorconfdlg.lbl.Motorconfig = <html><b>Motor configurations:</b>
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edtmotorconfdlg.lbl.Configname = Configuration name:
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edtmotorconfdlg.lbl.Leavenamedefault = Leave name empty for default.
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! Example design dialog
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exdesigndlg.but.open = Open
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exdesigndlg.lbl.Selectexample = Select example designs to open:
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exdesigndlg.lbl.Openexampledesign = Open example design
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exdesigndlg.lbl.Exampledesignsnotfound = Example designs could not be found.
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exdesigndlg.lbl.Examplesnotfound = Examples not found
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! Material edit panel
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matedtpan.but.new = New
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matedtpan.but.edit = Edit
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matedtpan.but.delete = Delete
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matedtpan.but.revertall = Revert all
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matedtpan.col.Material = Material
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matedtpan.col.Type = Type
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matedtpan.col.Density = Density
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matedtpan.col.but.ttip.New = Add a new material
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matedtpan.title.Addcustmaterial = Add a custom material
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matedtpan.but.ttip.edit = Edit an existing material
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matedtpan.title.Editmaterial = Edit material
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matedtpan.title2.Editmaterial = The built-in materials cannot be modified.
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matedtpan.but.ttip.delete = Delete a user-defined material
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matedtpan.but.ttip.revertall = Delete all user-defined materials
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matedtpan.title.Deletealluser-defined = Delete all user-defined materials?
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matedtpan.title.Revertall = Revert all?
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matedtpan.lbl.edtmaterials = Editing materials will not affect existing rocket designs.
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!MaterialModel
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MaterialModel.title.Material = Material
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MaterialModel.title.Defcustmat = Define custom material
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! Preference dialog
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pref.dlg.but.add = Add
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pref.dlg.but.reset = Reset
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pref.dlg.but.checknow = Check now
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pref.dlg.but.defaultmetric = Default metric
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pref.dlg.but.defaultimperial = Default imperial
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pref.dlg.title.Preferences = Preferences
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pref.dlg.tab.Units = Units
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pref.dlg.tab.Defaultunits = Default units
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pref.dlg.tab.Materials = Materials
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pref.dlg.tab.Custommaterials = Custom materials
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pref.dlg.tab.Options = Options
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pref.dlg.tab.Miscellaneousoptions = Miscellaneous options
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pref.dlg.lbl.Positiontoinsert = Position to insert new body components:
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pref.dlg.lbl.Confirmdeletion = Confirm deletion of simulations:
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pref.dlg.lbl.User-definedthrust = User-defined thrust curves:
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pref.dlg.Allthrustcurvefiles = All thrust curve files (*.eng; *.rse; *.zip; directories)
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pref.dlg.RASPfiles = RASP motor files (*.eng)
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pref.dlg.RockSimfiles = RockSim engine files (*.rse)
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pref.dlg.ZIParchives = ZIP archives (*.zip)
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pref.dlg.checkbox.Checkupdates = Check for software updates at startup
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pref.dlg.ttip.Checkupdatesnow = Check for software updates now
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pref.dlg.lbl.Selectprefunits = Select your preferred units:
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pref.dlg.lbl.Rocketdimensions = Rocket dimensions:
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pref.dlg.lbl.Linedensity = Line density:
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pref.dlg.lbl.Motordimensions = Motor dimensions:
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pref.dlg.lbl.Surfacedensity = Surface density:
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pref.dlg.lbl.Distance = Distance:
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pref.dlg.lbl.Bulkdensity = Bulk density:
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pref.dlg.lbl.Velocity = Velocity:
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pref.dlg.lbl.Surfaceroughness = Surface roughness:
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pref.dlg.lbl.Acceleration = Acceleration:
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pref.dlg.lbl.Area = Area:
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pref.dlg.lbl.Mass = Mass:
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pref.dlg.lbl.Angle = Angle:
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pref.dlg.lbl.Force = Force:
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pref.dlg.lbl.Rollrate = Roll rate:
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pref.dlg.lbl.Totalimpulse = Total impulse:
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pref.dlg.lbl.Temperature = Temperature:
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pref.dlg.lbl.Momentofinertia = Moment of inertia:
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pref.dlg.lbl.Pressure = Pressure:
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pref.dlg.lbl.Stability = Stability:
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pref.dlg.lbl.FlightTime = Flight time:
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pref.dlg.lbl.effect1 = The effects will take place the next time you open a window.
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pref.dlg.lbl.Checkingupdates = Checking for updates...
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pref.dlg.lbl.msg1 = An error occurred while communicating with the server.
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pref.dlg.lbl.msg2 = Unable to retrieve update information
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pref.dlg.lbl.msg3 = You are running the latest version of OpenRocket.
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pref.dlg.lbl.msg4 = No updates available
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pref.dlg.PrefChoiseSelector1 = Always ask
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pref.dlg.PrefChoiseSelector2 = Insert in middle
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pref.dlg.PrefChoiseSelector3 = Add to end
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pref.dlg.PrefBooleanSelector1 = Delete
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pref.dlg.PrefBooleanSelector2 = Confirm
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pref.dlg.Add = Add
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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.
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PreferencesDialog.lbl.language = Interface language:
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PreferencesDialog.languages.default = System default
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PreferencesDialog.lbl.languageEffect = The language will change the next time you start OpenRocket.
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! Simulation edit dialog
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simedtdlg.but.runsimulation = Run simulation
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simedtdlg.but.resettodefault = Reset to default
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simedtdlg.but.add = Add
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simedtdlg.but.remove = Remove
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simedtdlg.title.Editsim = Edit simulation
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simedtdlg.lbl.Simname = Simulation name:
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simedtdlg.tab.Launchcond = Launch conditions
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simedtdlg.tab.Simopt = Simulation options
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simedtdlg.tab.Plotdata = Plot data
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simedtdlg.tab.Exportdata = Export data
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simedtdlg.lbl.Motorcfg = Motor configuration:
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simedtdlg.lbl.ttip.Motorcfg = Select the motor configuration to use.
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simedtdlg.combo.ttip.motorconf = Select the motor configuration to use.
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simedtdlg.lbl.Wind = Wind
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simedtdlg.lbl.Averwindspeed = Average windspeed:
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simedtdlg.lbl.ttip.Averwindspeed = The average windspeed relative to the ground.
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simedtdlg.lbl.Stddeviation = Standard deviation:
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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.
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simedtdlg.lbl.Turbulenceintensity = Turbulence intensity:
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simedtdlg.lbl.ttip.Turbulenceintensity1 = <html>The turbulence intensity is the standard deviation divided by the average windspeed.<br>
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simedtdlg.lbl.ttip.Turbulenceintensity2 = Typical values range from
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simedtdlg.lbl.ttip.Turbulenceintensity3 = to
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simedtdlg.border.Atmoscond = Atmospheric conditions
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simedtdlg.checkbox.InterStdAtmosphere = Use International Standard Atmosphere
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simedtdlg.checkbox.ttip.InterStdAtmosphere1 = <html>Select to use the International Standard Atmosphere model.<br>This model has a temperature of
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simedtdlg.checkbox.ttip.InterStdAtmosphere2 = and a pressure of
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simedtdlg.checkbox.ttip.InterStdAtmosphere3 = at sea level.
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simedtdlg.lbl.Temperature = Temperature:
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simedtdlg.lbl.ttip.Temperature = The temperature at the launch site.
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simedtdlg.lbl.Pressure = Pressure:
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simedtdlg.lbl.ttip.Pressure = The atmospheric pressure at the launch site.
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simedtdlg.lbl.Launchsite = Launch site
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simedtdlg.lbl.Latitude = Latitude:
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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.
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simedtdlg.lbl.Longitude = Longitude:
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simedtdlg.lbl.ttip.Longitude = <html>Required for weather prediction and elevation models.
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simedtdlg.lbl.Altitude = Altitude:
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simedtdlg.lbl.ttip.Altitude = <html>The launch altitude above mean sea level.<br>This affects the position of the rocket in the atmospheric model.
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simedtdlg.border.Launchrod = Launch rod
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simedtdlg.lbl.Length = Length:
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simedtdlg.lbl.ttip.Length = The length of the launch rod.
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simedtdlg.lbl.Angle = Angle:
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simedtdlg.lbl.ttip.Angle = The angle of the launch rod from vertical.
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simedtdlg.lbl.Direction = Direction:
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simedtdlg.lbl.ttip.Direction1 = <html>Direction of the launch rod relative to the wind.<br>
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simedtdlg.lbl.ttip.Direction2 = = towards the wind,
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simedtdlg.lbl.ttip.Direction3 = = downwind.
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simedtdlg.border.Simopt = Simulator options
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simedtdlg.lbl.Calcmethod = Calculation method:
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simedtdlg.lbl.ttip.Calcmethod = <html>The Extended Barrowman method calculates aerodynamic forces according <br>to the Barrowman equations extended to accommodate more components.
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simedtdlg.lbl.ExtBarrowman = Extended Barrowman
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simedtdlg.lbl.Simmethod = Simulation method:
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simedtdlg.lbl.ttip.Simmethod1 = <html>The six degree-of-freedom simulator allows the rocket total freedom during flight.<br>
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simedtdlg.lbl.ttip.Simmethod2 = Integration is performed using a 4<sup>th</sup> order Runge-Kutta 4 numerical integration.
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simedtdlg.lbl.GeodeticMethod = Geodetic calculations:
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simedtdlg.lbl.ttip.GeodeticMethodTip = Relate to the calculation of coordinates on the earth. This also enables coriolis effect computations.
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simedtdlg.lbl.Timestep = Time step:
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simedtdlg.lbl.ttip.Timestep1 = <html>The time between simulation steps.<br>A smaller time step results in a more accurate but slower simulation.<br>
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simedtdlg.lbl.ttip.Timestep2 = The 4<sup>th</sup> order simulation method is quite accurate with a time step of
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simedtdlg.but.ttip.resettodefault = Reset the time step to its default value (
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simedtdlg.border.Simlist = Simulator listeners
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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.
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simedtdlg.txt.longA2 = For details on writing simulation listeners, see the OpenRocket technical documentation.
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simedtdlg.lbl.Curlist = Current listeners:
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simedtdlg.lbl.Addsimlist = Add simulation listener
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simedtdlg.lbl.Noflightdata = No flight data available.
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simedtdlg.lbl.runsimfirst = Please run the simulation first.
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simedtdlg.chart.Simflight = Simulated flight
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simedtdlg.dlg.Simres = Simulation results
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simedtdlg.IntensityDesc.None = None
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simedtdlg.IntensityDesc.Verylow = Very low
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simedtdlg.IntensityDesc.Low = Low
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simedtdlg.IntensityDesc.Medium = Medium
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simedtdlg.IntensityDesc.High = High
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simedtdlg.IntensityDesc.Veryhigh = Very high
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simedtdlg.IntensityDesc.Extreme = Extreme
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GeodeticComputationStrategy.flat.name = Flat Earth
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GeodeticComputationStrategy.flat.desc = Perform computations with a flat Earth approximation. Sufficient for low-altitude flights.
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GeodeticComputationStrategy.spherical.name = Spherical approximation
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GeodeticComputationStrategy.spherical.desc = <html>Perform geodetic computations assuming a spherical Earth.<br>This is sufficiently accurate for almost all purposes.
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GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid
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GeodeticComputationStrategy.wgs84.desc = <html>Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.<br>Slower and unnecessary in most cases.
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! Simulation Panel
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simpanel.but.newsimulation = New simulation
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simpanel.but.editsimulation = Edit simulation
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simpanel.but.runsimulations = Run simulations
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simpanel.but.deletesimulations = Delete simulations
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simpanel.but.plotexport = Plot / export
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simpanel.but.ttip.newsimulation = Add a new simulation
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simpanel.but.ttip.editsim = Edit the selected simulation
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simpanel.but.ttip.runsimu = Re-run the selected simulations
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simpanel.but.ttip.deletesim = Delete the selected simulations
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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.Velocityoffrod = Velocity off rod
|
|
simpanel.col.Velocityatdeploy = Velocity at deployment
|
|
simpanel.col.Apogee = Apogee
|
|
simpanel.col.Maxvelocity = Max. velocity
|
|
simpanel.col.Maxacceleration = Max. acceleration
|
|
simpanel.col.Timetoapogee = Time to apogee
|
|
simpanel.col.Flighttime = Flight time
|
|
simpanel.col.Groundhitvelocity = Ground hit velocity
|
|
|
|
! SimulationRunDialog
|
|
SimuRunDlg.title.RunSim = Running simulations...
|
|
SimuRunDlg.lbl.Running = Running ...
|
|
SimuRunDlg.lbl.Simutime = Simulation time:
|
|
SimuRunDlg.lbl.Altitude = Altitude:
|
|
SimuRunDlg.lbl.Velocity = Velocity:
|
|
SimuRunDlg.msg.Unabletosim = Unable to simulate:
|
|
SimuRunDlg.msg.errorOccurred = An error occurred during the simulation:
|
|
SimuRunDlg.msg.AnException1 = An exception occurred during the simulation:
|
|
SimuRunDlg.msg.AnException2 = Please report this as a bug along with the details below.
|
|
SimuRunDlg.msg.AssertionError1 = A computation error occurred during the simulation.
|
|
SimuRunDlg.msg.AssertionError2 = Please report this as a bug along with the details below.
|
|
SimuRunDlg.msg.unknownerror1 = An unknown error was encountered during the simulation.
|
|
SimuRunDlg.msg.unknownerror2 = The program may be unstable, you should save all your designs and restart OpenRocket now!
|
|
|
|
|
|
RK4SimulationStepper.error.valuesTooLarge = Simulation values exceeded limits. Try selecting a shorter time step.
|
|
|
|
|
|
! SimulationExportPanel
|
|
SimExpPan.desc = Comma Separated Files (*.csv)
|
|
SimExpPan.border.Vartoexport = Variables to export
|
|
SimExpPan.but.Selectall = Select all
|
|
SimExpPan.but.Selectnone = Select none
|
|
SimExpPan.border.Fieldsep = Field separator
|
|
SimExpPan.lbl.Fieldsepstr = Field separator string:
|
|
SimExpPan.lbl.longA1 = <html>The string used to separate the fields in the exported file.<br>
|
|
SimExpPan.lbl.longA2 = Use ',' for a Comma Separated Values (CSV) file.
|
|
SimExpPan.checkbox.Includesimudesc = Include simulation description
|
|
SimExpPan.checkbox.ttip.Includesimudesc = Include a comment at the beginning of the file describing the simulation.
|
|
SimExpPan.border.Comments = Comments
|
|
SimExpPan.checkbox.Includefielddesc = Include field descriptions
|
|
SimExpPan.checkbox.ttip.Includefielddesc = Include a comment line with the descriptions of the exported variables.
|
|
SimExpPan.checkbox.Incflightevents = Include flight events
|
|
SimExpPan.checkbox.ttip.Incflightevents = Include a comment line for every flight event.
|
|
SimExpPan.lbl.Commentchar = Comment character:
|
|
SimExpPan.lbl.ttip.Commentchar = The character(s) that mark a comment line.
|
|
SimExpPan.but.Exporttofile = Export to file...
|
|
SimExpPan.Fileexists.desc1 = File \"
|
|
SimExpPan.Fileexists.desc2 = \" exists. Overwrite?
|
|
SimExpPan.Fileexists.title = File exists
|
|
SimExpPan.ExportingVar.desc1 = Exporting 1 variable out of
|
|
SimExpPan.ExportingVar.desc2 = Exporting
|
|
SimExpPan.ExportingVar.desc3 = variables out of
|
|
SimExpPan.Col.Variable = Variable
|
|
SimExpPan.Col.Unit = Unit
|
|
|
|
|
|
CsvOptionPanel.separator.space = SPACE
|
|
CsvOptionPanel.separator.tab = TAB
|
|
|
|
|
|
|
|
! MotorPlot
|
|
MotorPlot.title.Motorplot = Motor plot
|
|
MotorPlot.but.Select = Select
|
|
MotorPlot.Chart.Motorthrustcurve = Motor thrust curve
|
|
MotorPlot.Chart.Time = Time / s
|
|
MotorPlot.Chart.Thrust = Thrust / N
|
|
MotorPlot.txt.Designation = Designation:
|
|
MotorPlot.txt.Manufacturer = Manufacturer:
|
|
MotorPlot.txt.Type = Type:
|
|
MotorPlot.txt.Delays = Delays:
|
|
MotorPlot.txt.Comment = Comment:\n
|
|
|
|
|
|
|
|
! Simulation plot panel
|
|
simplotpanel.lbl.Presetplotconf = Preset plot configurations:
|
|
simplotpanel.lbl.Xaxistype = X axis type:
|
|
simplotpanel.lbl.Unit = Unit:
|
|
simplotpanel.lbl.Yaxistypes = Y axis types:
|
|
simplotpanel.lbl.Flightevents = Flight events:
|
|
simplotpanel.but.All = All
|
|
simplotpanel.but.None = None
|
|
simplotpanel.but.NewYaxisplottype = New Y axis plot type
|
|
simplotpanel.but.Plotflight = Plot flight
|
|
simplotpanel.lbl.Axis = Axis:
|
|
simplotpanel.but.ttip.Removethisplot = Remove this plot
|
|
simplotpanel.Desc = The data will be plotted in time order even if the X axis type is not time.
|
|
simplotpanel.OptionPane.lbl1 = A maximum of 15 plots is allowed.
|
|
simplotpanel.OptionPane.lbl2 = Cannot add plot
|
|
simplotpanel.AUTO_NAME = Auto
|
|
simplotpanel.LEFT_NAME = Left
|
|
simplotpanel.RIGHT_NAME = Right
|
|
simplotpanel.CUSTOM = Custom
|
|
SimulationPlotPanel.error.noPlotSelected = Please add one or more variables to plot on the Y-axis.
|
|
SimulationPlotPanel.error.noPlotSelected.title = Nothing to plot
|
|
|
|
|
|
! Component add buttons
|
|
compaddbuttons.Bodycompandfinsets = Body components and fin sets
|
|
compaddbuttons.Nosecone = Nose cone
|
|
compaddbuttons.Bodytube = Body tube
|
|
compaddbuttons.Transition = Transition
|
|
compaddbuttons.Trapezoidal = Trapezoidal
|
|
compaddbuttons.Elliptical = Elliptical
|
|
compaddbuttons.Freeform = Freeform
|
|
compaddbuttons.Launchlug = Launch lug
|
|
compaddbuttons.Innercomponent = Inner component
|
|
compaddbuttons.Innertube = Inner tube
|
|
compaddbuttons.Coupler = Coupler
|
|
compaddbuttons.Centeringring = Centering\nring
|
|
compaddbuttons.Bulkhead = Bulkhead
|
|
compaddbuttons.Engineblock = Engine\nblock
|
|
compaddbuttons.Massobjects = Mass objects
|
|
compaddbuttons.Parachute = Parachute
|
|
compaddbuttons.Streamer = Streamer
|
|
compaddbuttons.Shockcord = Shock cord
|
|
compaddbuttons.Masscomponent = Mass\ncomponent
|
|
compaddbuttons.Donotaskmeagain = Do not ask me again
|
|
compaddbuttons.Selectcomppos = Select component position
|
|
compaddbuttons.lbl.Youcanchange = You can change the default operation in the preferences.
|
|
compaddbuttons.lbl.insertcomp = Insert the component after the current component or as the last component?
|
|
compaddbuttons.askPosition.Inserthere = Insert here
|
|
compaddbuttons.askPosition.Addtotheend = Add to the end
|
|
compaddbuttons.askPosition.Cancel = Cancel
|
|
|
|
! Component Analysis Dialog
|
|
componentanalysisdlg.componentanalysis = Component analysis
|
|
componentanalysisdlg.lbl.winddir = Wind direction:
|
|
componentanalysisdlg.TitledBorder.warnings = Warnings:
|
|
componentanalysisdlg.ToggleBut.worst = Worst
|
|
componentanalysisdlg.lbl.angleofattack = Angle of attack:
|
|
componentanalysisdlg.lbl.machnumber = Mach number:
|
|
componentanalysisdlg.lbl.rollrate = Roll rate:
|
|
componentanalysisdlg.lbl.activestages = Active stages:
|
|
componentanalysisdlg.lbl.motorconf = Motor configuration:
|
|
componentanalysisdlg.TabStability.Col = Component
|
|
componentanalysisdlg.TabStability = Stability
|
|
componentanalysisdlg.TabStability.ttip = Stability information
|
|
componentanalysisdlg.dragTableModel.Col.Component = Component
|
|
componentanalysisdlg.dragTableModel.Col.Pressure = <html>Pressure C<sub>D</sub>
|
|
componentanalysisdlg.dragTableModel.Col.Base = <html>Base C<sub>D</sub>
|
|
componentanalysisdlg.dragTableModel.Col.friction = <html>Friction C<sub>D</sub>
|
|
componentanalysisdlg.dragTableModel.Col.total = <html>Total C<sub>D</sub>
|
|
componentanalysisdlg.dragTabchar = Drag characteristics
|
|
componentanalysisdlg.dragTabchar.ttip = Drag characteristics
|
|
componentanalysisdlg.rollTableModel.Col.component = Component
|
|
componentanalysisdlg.rollTableModel.Col.rollforc = Roll forcing coefficient
|
|
componentanalysisdlg.rollTableModel.Col.rolldamp = Roll damping coefficient
|
|
componentanalysisdlg.rollTableModel.Col.total = <html>Total C<sub>l</sub>
|
|
componentanalysisdlg.rollTableModel = Roll dynamics
|
|
componentanalysisdlg.rollTableModel.ttip = Roll dynamics
|
|
componentanalysisdlg.println.closingmethod = Closing method called:
|
|
componentanalysisdlg.println.settingnam = SETTING NAN VALUES
|
|
componentanalysisdlg.lbl.reflenght = Reference length:
|
|
componentanalysisdlg.lbl.refarea = Reference area:
|
|
!componentanalysisdlg.But.close =Close
|
|
componentanalysisdlg.TabStability.Col.Component = Component
|
|
|
|
! Custom Material dialog
|
|
custmatdlg.title.Custommaterial = Custom material
|
|
custmatdlg.lbl.Materialname = Material name:
|
|
custmatdlg.lbl.Materialtype = Material type:
|
|
custmatdlg.lbl.Materialdensity = Material density:
|
|
custmatdlg.checkbox.Addmaterial = Add material to database
|
|
|
|
|
|
! Ring Component Config
|
|
ringcompcfg.OuterRadius = OuterRadius
|
|
ringcompcfg.Automatic = Automatic
|
|
ringcompcfg.InnerRadius = InnerRadius
|
|
ringcompcfg.Thickness = Thickness
|
|
ringcompcfg.Length = Length
|
|
ringcompcfg.Positionrelativeto = Position relative to:
|
|
ringcompcfg.plus = plus
|
|
ringcompcfg.PositionValue = PositionValue
|
|
ringcompcfg.Radialdistance = Radial distance:
|
|
ringcompcfg.Distancefrom = Distance from the rocket centerline
|
|
ringcompcfg.Radialdirection = Radial direction:
|
|
ringcompcfg.radialdirectionfrom = The radial direction from the rocket centerline
|
|
ringcompcfg.but.Reset = Reset
|
|
ringcompcfg.but.Resetcomponant = Reset the component to the rocket centerline
|
|
ringcompcfg.EngineBlock.desc = <html>An <b>engine block</b> stops the motor from moving forwards in the motor mount tube.<br><br>In order to add a motor, create a <b>body tube</b> or <b>inner tube</b> and mark it as a motor mount in the <em>Motor</em> tab.
|
|
ringcompcfg.note.desc = Note: An inner tube will not affect the aerodynamics of the rocket even if it is located outside of the body tube.
|
|
|
|
|
|
! Body Tube Config
|
|
BodyTubecfg.lbl.Bodytubelength = Body tube length:
|
|
BodyTubecfg.lbl.Outerdiameter = Outer diameter:
|
|
BodyTubecfg.lbl.Innerdiameter = Inner diameter:
|
|
BodyTubecfg.lbl.Wallthickness = Wall thickness:
|
|
BodyTubecfg.tab.General = General
|
|
BodyTubecfg.tab.Generalproperties = General properties
|
|
BodyTubecfg.tab.Motor = Motor
|
|
BodyTubecfg.tab.Motormountconf = Motor mount configuration
|
|
BodyTubecfg.checkbox.Automatic = Automatic
|
|
BodyTubecfg.checkbox.Filled = Filled
|
|
|
|
! FinSetConfig
|
|
FinSetConfig.tab.Fintabs = Fin tabs
|
|
FinSetConfig.tab.Through-the-wall = Through-the-wall fin tabs
|
|
FinSetConfig.but.Converttofreeform = Convert to freeform
|
|
FinSetConfig.but.Converttofreeform.ttip = Convert this fin set into a freeform fin set
|
|
FinSetConfig.Convertfinset = Convert fin set
|
|
FinSetConfig.but.Splitfins = Split fins
|
|
FinSetConfig.but.Splitfins.ttip = Split the fin set into separate fins
|
|
FinSetConfig.but.AutoCalc = Calculate automatically
|
|
FinSetConfig.lbl.Through-the-wall = Through-the-wall fin tabs:
|
|
FinSetConfig.lbl.Tablength = Tab length:
|
|
FinSetConfig.ttip.Tablength = The length of the fin tab.
|
|
FinSetConfig.lbl.Tabheight = Tab height:
|
|
FinSetConfig.ttip.Tabheight = The spanwise height of the fin tab.
|
|
FinSetConfig.lbl.Tabposition = Tab position:
|
|
FinSetConfig.ttip.Tabposition = The position of the fin tab.
|
|
FinSetConfig.lbl.relativeto = relative to
|
|
|
|
!FinMarkingGuide
|
|
FinMarkingGuide.lbl.Front = Front
|
|
|
|
! MotorDatabaseLoadingDialog
|
|
MotorDbLoadDlg.title = Loading motors
|
|
MotorDbLoadDlg.Loadingmotors = Loading motors...
|
|
|
|
! RocketConfig
|
|
RocketCfg.lbl.Designname = Design name:
|
|
RocketCfg.lbl.Designer = Designer:
|
|
RocketCfg.lbl.Comments = Comments:
|
|
RocketCfg.lbl.Revisionhistory = Revision history:
|
|
RocketCfg.lbl.Material = Material:
|
|
|
|
! ShockCordConfig
|
|
ShockCordCfg.lbl.Shockcordlength = Shock cord length:
|
|
|
|
! RocketComponentConfig
|
|
RocketCompCfg.lbl.Componentname = Component name:
|
|
RocketCompCfg.ttip.Thecomponentname = The component name.
|
|
RocketCompCfg.tab.Override = Override
|
|
RocketCompCfg.tab.MassandCGoverride = Mass and CG override options
|
|
RocketCompCfg.tab.Figure = Figure
|
|
RocketCompCfg.tab.Figstyleopt = Figure style options
|
|
RocketCompCfg.tab.Comment = Comment
|
|
RocketCompCfg.tab.Specifyacomment = Specify a comment for the component
|
|
RocketCompCfg.lbl.Mass = Mass:
|
|
RocketCompCfg.lbl.Componentmass = Component mass:
|
|
RocketCompCfg.lbl.overriddento = (overridden to
|
|
RocketCompCfg.lbl.overriddenby = (overridden by
|
|
RocketCompCfg.lbl.Componentmaterial = Component material:
|
|
RocketCompCfg.lbl.Componentfinish = Component finish:
|
|
RocketCompCfg.lbl.ttip.componentmaterialaffects = The component material affects the weight of the component.
|
|
RocketCompCfg.combo.ttip.componentmaterialaffects = The component material affects the weight of the component.
|
|
RocketCompCfg.lbl.longA1 = <html>The component finish affects the aerodynamic drag of the component.<br>
|
|
RocketCompCfg.lbl.longA2 = The value indicated is the average roughness height of the surface.
|
|
RocketCompCfg.but.Setforall = Set for all
|
|
RocketCompCfg.but.ttip.Setforall = Set this finish for all components of the rocket.
|
|
RocketCompCfg.lbl.Overridemassorcenter = Override the mass or center of gravity of the
|
|
RocketCompCfg.checkbox.Overridemass = Override mass:
|
|
RocketCompCfg.checkbox.Overridecenterofgrav = Override center of gravity:
|
|
RocketCompCfg.checkbox.OverridemassandCG = Override mass and CG of all subcomponents
|
|
RocketCompCfg.lbl.longB1 = <html>The overridden mass does not include motors.<br>
|
|
RocketCompCfg.lbl.longB2 = The center of gravity is measured from the front end of the
|
|
RocketCompCfg.lbl.Commentsonthe = Comments on the
|
|
RocketCompCfg.lbl.Figurestyle = Figure style:
|
|
RocketCompCfg.lbl.Componentcolor = Component color:
|
|
RocketCompCfg.lbl.Choosecolor = Choose color
|
|
RocketCompCfg.checkbox.Usedefaultcolor = Use default color
|
|
RocketCompCfg.lbl.Complinestyle = Component line style:
|
|
RocketCompCfg.but.Saveasdefstyle = Save as default style
|
|
RocketCompCfg.lbl.Diameter = Diameter:
|
|
RocketCompCfg.lbl.Length = Length:
|
|
RocketCompCfg.lbl.Thickness = Thickness:
|
|
RocketCompCfg.checkbox.Endcapped = End capped
|
|
RocketCompCfg.ttip.Endcapped = Whether the end of the shoulder is capped.
|
|
RocketCompCfg.title.Noseconeshoulder = Nose cone shoulder
|
|
RocketCompCfg.title.Aftshoulder = Aft shoulder
|
|
RocketCompCfg.border.Foreshoulder = Fore shoulder
|
|
!RocketCompCfg.lbl.Length = Length:
|
|
|
|
! BulkheadConfig
|
|
BulkheadCfg.tab.Diameter = Diameter:
|
|
BulkheadCfg.tab.Thickness = Thickness:
|
|
BulkheadCfg.tab.General = General
|
|
BulkheadCfg.tab.Generalproperties = General properties
|
|
|
|
!CenteringRingConfig
|
|
CenteringRingCfg.tab.Outerdiam = Outer diameter:
|
|
CenteringRingCfg.tab.Innerdiam = Inner diameter:
|
|
CenteringRingCfg.tab.Thickness = Thickness:
|
|
CenteringRingCfg.tab.General = General
|
|
CenteringRingCfg.tab.Generalproperties = General properties
|
|
|
|
!ComponentConfigDialog
|
|
ComponentCfgDlg.configuration = configuration
|
|
ComponentCfgDlg.configuration1 =
|
|
ComponentCfgDlg.Modify = Modify
|
|
|
|
!EllipticalFinSetConfig
|
|
EllipticalFinSetCfg.Nbroffins = Number of fins:
|
|
EllipticalFinSetCfg.Rotation = Rotation:
|
|
EllipticalFinSetCfg.Fincant = Fin cant:
|
|
EllipticalFinSetCfg.Rootchord = Root chord:
|
|
EllipticalFinSetCfg.Height = Height:
|
|
EllipticalFinSetCfg.Positionrelativeto = Position relative to:
|
|
EllipticalFinSetCfg.plus = plus
|
|
EllipticalFinSetCfg.FincrossSection = Fin cross section:
|
|
EllipticalFinSetCfg.Thickness = Thickness:
|
|
EllipticalFinSetCfg.General = General
|
|
EllipticalFinSetCfg.Generalproperties = General properties
|
|
EllipticalFinSetCfg.ttip.Fincant = The angle that the fins are canted with respect to the rocket body.
|
|
|
|
!FreeformFinSetConfig
|
|
FreeformFinSetCfg.tab.General = General
|
|
FreeformFinSetCfg.tab.ttip.General = General properties
|
|
FreeformFinSetCfg.tab.Shape = Shape
|
|
FreeformFinSetCfg.tab.ttip.Finshape = Fin shape
|
|
FreeformFinSetCfg.lbl.Numberoffins = Number of fins:
|
|
FreeformFinSetCfg.lbl.Finrotation = Fin rotation:
|
|
FreeformFinSetCfg.lbl.Fincant = Fin cant:
|
|
FreeformFinSetCfg.lbl.ttip.Fincant = The angle that the fins are canted with respect to the rocket body.
|
|
FreeformFinSetCfg.lbl.Posrelativeto = Position relative to:
|
|
FreeformFinSetCfg.lbl.plus = plus
|
|
FreeformFinSetCfg.lbl.FincrossSection = Fin cross section:
|
|
FreeformFinSetCfg.lbl.Thickness = Thickness:
|
|
! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle
|
|
FreeformFinSetConfig.lbl.doubleClick1 = Double-click
|
|
FreeformFinSetConfig.lbl.doubleClick2 = to edit
|
|
FreeformFinSetConfig.lbl.clickDrag = Click+drag: Add and move points
|
|
FreeformFinSetConfig.lbl.ctrlClick = Ctrl+click: Remove point
|
|
|
|
|
|
!InnerTubeConfig
|
|
InnerTubeCfg.tab.Motor = Motor
|
|
InnerTubeCfg.tab.ttip.Motor = Motor mount configuration
|
|
InnerTubeCfg.tab.Cluster = Cluster
|
|
InnerTubeCfg.tab.ttip.Cluster = Cluster configuration
|
|
InnerTubeCfg.tab.Radialpos = Radial position
|
|
InnerTubeCfg.tab.ttip.Radialpos = Radial position
|
|
InnerTubeCfg.lbl.Selectclustercfg = Select cluster configuration:
|
|
InnerTubeCfg.lbl.TubeSep = Tube separation:
|
|
InnerTubeCfg.lbl.ttip.TubeSep = The separation of the tubes, 1.0 = touching each other
|
|
InnerTubeCfg.lbl.Rotation = Rotation:
|
|
InnerTubeCfg.lbl.ttip.Rotation = Rotation angle of the cluster configuration
|
|
InnerTubeCfg.lbl.Rotangle = Rotation angle of the cluster configuration
|
|
InnerTubeCfg.but.Splitcluster = Split cluster
|
|
InnerTubeCfg.lbl.longA1 = <html>Split the cluster into separate components.<br>
|
|
InnerTubeCfg.lbl.longA2 = This also duplicates all components attached to this inner tube.
|
|
InnerTubeCfg.but.Resetsettings = Reset settings
|
|
InnerTubeCfg.but.ttip.Resetsettings = Reset the separation and rotation to the default values
|
|
|
|
! LaunchLugConfig
|
|
LaunchLugCfg.lbl.Length = Length:
|
|
LaunchLugCfg.lbl.Outerdiam = Outer diameter:
|
|
LaunchLugCfg.lbl.Innerdiam = Inner diameter:
|
|
LaunchLugCfg.lbl.Thickness = Thickness:
|
|
LaunchLugCfg.lbl.Radialpos = Radial position:
|
|
LaunchLugCfg.lbl.Posrelativeto = Position relative to:
|
|
LaunchLugCfg.lbl.plus = plus
|
|
LaunchLugCfg.tab.General = General
|
|
LaunchLugCfg.tab.Generalprop = General properties
|
|
|
|
! MassComponentConfig
|
|
MassComponentCfg.lbl.Mass = Mass:
|
|
MassComponentCfg.lbl.Length = Length:
|
|
MassComponentCfg.lbl.Diameter = Diameter:
|
|
MassComponentCfg.lbl.PosRelativeto = Position relative to:
|
|
MassComponentCfg.lbl.plus = plus
|
|
MassComponentCfg.tab.General = General
|
|
MassComponentCfg.tab.ttip.General = General properties
|
|
MassComponentCfg.tab.Radialpos = Radial position
|
|
MassComponentCfg.tab.ttip.Radialpos = Radial position configuration
|
|
MassComponentCfg.lbl.Radialdistance = Radial distance:
|
|
MassComponentCfg.lbl.Radialdirection = Radial direction:
|
|
MassComponentCfg.but.Reset = Reset
|
|
|
|
! MotorConfig
|
|
MotorCfg.checkbox.compmotormount = This component is a motor mount
|
|
MotorCfg.lbl.Motorcfg = Motor configuration:
|
|
MotorCfg.but.New = New
|
|
MotorCfg.lbl.Currentmotor = Current motor:
|
|
MotorCfg.lbl.Motoroverhang = Motor overhang:
|
|
MotorCfg.lbl.Ignitionat = Ignition at:
|
|
MotorCfg.lbl.plus = plus
|
|
MotorCfg.lbl.seconds = seconds
|
|
MotorCfg.lbl.longA1 = The current design has only one stage.
|
|
MotorCfg.lbl.longA2 = Stages can be added by clicking \"New stage\".
|
|
MotorCfg.lbl.longB1 = The current design has
|
|
MotorCfg.lbl.longB2 = stages.
|
|
MotorCfg.but.Selectmotor = Select motor
|
|
MotorCfg.but.Removemotor = Remove motor
|
|
MotorCfg.lbl.motorLabel = None
|
|
|
|
! NoseConeConfig
|
|
NoseConeCfg.lbl.Noseconeshape = Nose cone shape:
|
|
NoseConeCfg.lbl.Shapeparam = Shape parameter:
|
|
NoseConeCfg.lbl.Noseconelength = Nose cone length:
|
|
NoseConeCfg.lbl.Basediam = Base diameter:
|
|
NoseConeCfg.checkbox.Automatic = Automatic
|
|
NoseConeCfg.lbl.Wallthickness = Wall thickness:
|
|
NoseConeCfg.checkbox.Filled = Filled
|
|
NoseConeCfg.tab.General = General
|
|
NoseConeCfg.tab.ttip.General = General properties
|
|
NoseConeCfg.tab.Shoulder = Shoulder
|
|
NoseConeCfg.tab.ttip.Shoulder = Shoulder properties
|
|
|
|
! ParachuteConfig
|
|
ParachuteCfg.lbl.Canopy = Canopy:
|
|
ParachuteCfg.lbl.Diameter = Diameter:
|
|
ParachuteCfg.lbl.Material = Material:
|
|
ParachuteCfg.combo.MaterialModel = The component material affects the weight of the component.
|
|
ParachuteCfg.lbl.longA1 = <html>Drag coefficient C<sub>D</sub>:
|
|
ParachuteCfg.lbl.longB1 = <html>The drag coefficient relative to the total area of the parachute.<br>
|
|
ParachuteCfg.lbl.longB2 = A larger drag coefficient yields a slowed descent rate.
|
|
ParachuteCfg.lbl.longB3 = A typical value for parachutes is 0.8.
|
|
ParachuteCfg.but.Reset = Reset
|
|
ParachuteCfg.lbl.Shroudlines = Shroud lines:
|
|
ParachuteCfg.lbl.Numberoflines = Number of lines:
|
|
ParachuteCfg.lbl.Linelength = Line length:
|
|
ParachuteCfg.lbl.Material = Material:
|
|
ParachuteCfg.lbl.Posrelativeto = Position relative to:
|
|
ParachuteCfg.lbl.plus = plus
|
|
ParachuteCfg.lbl.Packedlength = Packed length:
|
|
ParachuteCfg.lbl.Packeddiam = Packed diameter:
|
|
ParachuteCfg.lbl.Deploysat = Deploys at:
|
|
ParachuteCfg.lbl.seconds = seconds
|
|
ParachuteCfg.lbl.Altitude = Altitude:
|
|
ParachuteCfg.tab.General = General
|
|
ParachuteCfg.tab.ttip.General = General properties
|
|
ParachuteCfg.tab.Radialpos = Radial position
|
|
ParachuteCfg.tab.ttip.Radialpos = Radial position configuration
|
|
ParachuteCfg.lbl.Radialdistance = Radial distance:
|
|
ParachuteCfg.lbl.Radialdirection = Radial direction:
|
|
ParachuteCfg.but.Reset = Reset
|
|
ParachuteCfg.lbl.plusdelay = plus
|
|
|
|
! ShockCordConfig
|
|
ShockCordCfg.lbl.Shockcordlength = Shock cord length:
|
|
ShockCordCfg.lbl.Shockcordmaterial = Shock cord material:
|
|
ShockCordCfg.lbl.Posrelativeto = Position relative to:
|
|
ShockCordCfg.lbl.plus = plus
|
|
ShockCordCfg.lbl.Packedlength = Packed length:
|
|
ShockCordCfg.lbl.Packeddiam = Packed diameter:
|
|
ShockCordCfg.tab.General = General
|
|
ShockCordCfg.tab.ttip.General = General properties
|
|
|
|
!SleeveConfig
|
|
SleeveCfg.tab.Outerdiam = Outer diameter:
|
|
SleeveCfg.tab.Innerdiam = Inner diameter:
|
|
SleeveCfg.tab.Wallthickness = Wall thickness:
|
|
SleeveCfg.tab.Length = Length:
|
|
SleeveCfg.tab.General = General
|
|
SleeveCfg.tab.Generalproperties = General properties
|
|
|
|
! StreamerConfig
|
|
StreamerCfg.lbl.Striplength = Strip length:
|
|
StreamerCfg.lbl.Stripwidth = Strip width:
|
|
StreamerCfg.lbl.Striparea = Strip area:
|
|
StreamerCfg.lbl.Aspectratio = Aspect ratio:
|
|
StreamerCfg.lbl.Material = Material:
|
|
StreamerCfg.combo.ttip.MaterialModel = The component material affects the weight of the component.
|
|
StreamerCfg.lbl.longA1 = <html>Drag coefficient C<sub>D</sub>:
|
|
StreamerCfg.lbl.longB1 = <html>The drag coefficient relative to the total area of the streamer.<br>
|
|
StreamerCfg.lbl.longB2 = A larger drag coefficient yields a slowed descent rate.
|
|
StreamerCfg.lbl.Automatic = Automatic
|
|
StreamerCfg.lbl.longC1 = The drag coefficient is relative to the area of the streamer.
|
|
StreamerCfg.lbl.Posrelativeto = Position relative to:
|
|
StreamerCfg.lbl.plus = plus
|
|
StreamerCfg.lbl.Packedlength = Packed length:
|
|
StreamerCfg.lbl.Packeddiam = Packed diameter:
|
|
StreamerCfg.lbl.Deploysat = Deploys at:
|
|
StreamerCfg.lbl.seconds = seconds
|
|
StreamerCfg.lbl.Altitude = Altitude:
|
|
StreamerCfg.tab.General = General
|
|
StreamerCfg.tab.ttip.General = General properties
|
|
StreamerCfg.tab.Radialpos = Radial position
|
|
StreamerCfg.tab.ttip.Radialpos = Radial position configuration
|
|
StreamerCfg.lbl.Radialdistance = Radial distance:
|
|
StreamerCfg.lbl.Radialdirection = Radial direction:
|
|
StreamerCfg.but.Reset = Reset
|
|
StreamerCfg.lbl.plusdelay = plus
|
|
|
|
! ThicknessRingComponentConfig
|
|
ThicknessRingCompCfg.tab.Outerdiam = Outer diameter:
|
|
ThicknessRingCompCfg.tab.Innerdiam = Inner diameter:
|
|
ThicknessRingCompCfg.tab.Wallthickness = Wall thickness:
|
|
ThicknessRingCompCfg.tab.Length = Length:
|
|
ThicknessRingCompCfg.tab.General = General
|
|
ThicknessRingCompCfg.tab.Generalprop = General properties
|
|
|
|
! TransitionConfig
|
|
TransitionCfg.lbl.Transitionshape = Transition shape:
|
|
TransitionCfg.checkbox.Clipped = Clipped
|
|
TransitionCfg.lbl.Shapeparam = Shape parameter:
|
|
TransitionCfg.lbl.Transitionlength = Transition length:
|
|
TransitionCfg.lbl.Forediam = Fore diameter:
|
|
TransitionCfg.checkbox.Automatic = Automatic
|
|
TransitionCfg.lbl.Aftdiam = Aft diameter:
|
|
TransitionCfg.lbl.Wallthickness = Wall thickness:
|
|
TransitionCfg.checkbox.Filled = Filled
|
|
TransitionCfg.tab.General = General
|
|
TransitionCfg.tab.Generalproperties = General properties
|
|
TransitionCfg.tab.Shoulder = Shoulder
|
|
TransitionCfg.tab.Shoulderproperties = Shoulder properties
|
|
|
|
! TrapezoidFinSetConfig
|
|
TrapezoidFinSetCfg.lbl.Nbroffins = Number of fins:
|
|
TrapezoidFinSetCfg.lbl.ttip.Nbroffins = The number of fins in the fin set.
|
|
TrapezoidFinSetCfg.lbl.Finrotation = Fin rotation:
|
|
TrapezoidFinSetCfg.lbl.ttip.Finrotation = The angle of the first fin in the fin set.
|
|
TrapezoidFinSetCfg.lbl.Fincant = Fin cant:
|
|
TrapezoidFinSetCfg.lbl.ttip.Fincant =The angle that the fins are canted with respect to the rocket body.
|
|
TrapezoidFinSetCfg.lbl.Rootchord = Root chord:
|
|
TrapezoidFinSetCfg.lbl.Tipchord = Tip chord:
|
|
TrapezoidFinSetCfg.lbl.Height = Height:
|
|
TrapezoidFinSetCfg.lbl.Sweeplength = Sweep length:
|
|
TrapezoidFinSetCfg.lbl.Sweepangle = Sweep angle:
|
|
TrapezoidFinSetCfg.lbl.FincrossSection = Fin cross section:
|
|
TrapezoidFinSetCfg.lbl.Thickness = Thickness:
|
|
TrapezoidFinSetCfg.lbl.Posrelativeto = Position relative to:
|
|
TrapezoidFinSetCfg.lbl.plus = plus
|
|
TrapezoidFinSetCfg.tab.General = General
|
|
TrapezoidFinSetCfg.tab.Generalproperties = General properties
|
|
|
|
!MotorConfigurationModel
|
|
MotorCfgModel.Editcfg = Edit configurations
|
|
|
|
! StorageOptionChooser
|
|
StorageOptChooser.lbl.Simdatatostore = Simulated data to store:
|
|
StorageOptChooser.rdbut.Allsimdata = All simulated data
|
|
StorageOptChooser.lbl.longA1 = <html>Store all simulated data.<br>
|
|
StorageOptChooser.lbl.longA2 = This can result in very large files!
|
|
StorageOptChooser.rdbut.Every = Every
|
|
StorageOptChooser.lbl.longB1 = <html>Store plottable values approximately this far apart.<br>
|
|
StorageOptChooser.lbl.longB2 = Larger values result in smaller files.
|
|
StorageOptChooser.lbl.seconds = seconds
|
|
StorageOptChooser.rdbut.Onlyprimfig = Only primary figures
|
|
StorageOptChooser.lbl.longC1 = <html>Store only the values shown in the summary table.<br>
|
|
StorageOptChooser.lbl.longC2 = This results in the smallest files.
|
|
StorageOptChooser.checkbox.Compfile = Compress file
|
|
StorageOptChooser.lbl.UsingComp = Using compression reduces the file size significantly.
|
|
StorageOptChooser.lbl.longD1 = An estimate on how large the resulting file would be with the present options.
|
|
StorageOptChooser.ttip.Saveopt = Save options
|
|
StorageOptChooser.lbl.Estfilesize = Estimated file size:
|
|
StorageOptChooser.lbl.Saveopt = Save options
|
|
|
|
! ThrustCurveMotorSelectionPanel
|
|
TCMotorSelPan.lbl.Selrocketmotor = Select rocket motor:
|
|
TCMotorSelPan.checkbox.hideSimilar = Hide very similar thrust curves
|
|
TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Show all motors
|
|
TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Show motors with diameter less than that of the motor mount
|
|
TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Show motors with diameter equal to that of the motor mount
|
|
TCMotorSelPan.lbl.Motormountdia = Motor mount diameter:
|
|
TCMotorSelPan.lbl.Search = Search:
|
|
TCMotorSelPan.lbl.Selectthrustcurve = Select thrust curve:
|
|
TCMotorSelPan.lbl.Ejectionchargedelay = Ejection charge delay:
|
|
TCMotorSelPan.equalsIgnoreCase.None = None
|
|
TCMotorSelPan.lbl.NumberofsecondsorNone = (Number of seconds or \"None\")
|
|
TCMotorSelPan.lbl.Totalimpulse = Total impulse:
|
|
TCMotorSelPan.lbl.Avgthrust = Avg. thrust:
|
|
TCMotorSelPan.lbl.Maxthrust = Max. thrust:
|
|
TCMotorSelPan.lbl.Burntime = Burn time:
|
|
TCMotorSelPan.lbl.Launchmass = Launch mass:
|
|
TCMotorSelPan.lbl.Emptymass = Empty mass:
|
|
TCMotorSelPan.lbl.Datapoints = Data points:
|
|
TCMotorSelPan.lbl.Digest = Digest:
|
|
TCMotorSelPan.title.Thrustcurve = Thrust curve:
|
|
TCMotorSelPan.title.Thrust = Thrust
|
|
TCMotorSelPan.delayBox.None = None
|
|
|
|
|
|
! PlotDialog
|
|
PlotDialog.title.Flightdataplot = Flight data plot
|
|
PlotDialog.Chart.Simulatedflight = Simulated flight
|
|
PlotDialog.CheckBox.Showdatapoints = Show data points
|
|
PlotDialog.lbl.Chart = Click and drag down+right to zoom in, up+left to zoom out
|
|
|
|
|
|
! "main" prefix is used for the main application dialog
|
|
|
|
# FIXME: Rename the description keys
|
|
|
|
main.menu.file = File
|
|
main.menu.file.desc = File-handling related tasks
|
|
main.menu.file.new = New
|
|
main.menu.file.new.desc = Create a new rocket design
|
|
main.menu.file.open = Open...
|
|
BasicFrame.item.Openrocketdesign = Open a rocket design
|
|
main.menu.file.openExample = Open example...
|
|
BasicFrame.item.Openexamplerocketdesign = Open an example rocket design
|
|
main.menu.file.save = Save
|
|
BasicFrame.item.SavecurRocketdesign = Save the current rocket design
|
|
main.menu.file.saveAs = Save as...
|
|
BasicFrame.item.SavecurRocketdesnewfile = Save the current rocket design to a new file
|
|
main.menu.file.print = Print / Export PDF...
|
|
main.menu.file.print.desc = Print or save as PDF the parts list and fin templates
|
|
main.menu.file.close = Close
|
|
BasicFrame.item.Closedesign = Close the current rocket design
|
|
main.menu.file.quit = Quit
|
|
BasicFrame.item.Quitprogram = Quit the program
|
|
|
|
main.menu.edit = Edit
|
|
BasicFrame.menu.Rocketedt = Rocket editing
|
|
main.menu.edit.undo = Undo
|
|
main.menu.edit.undo.desc = Undo the previous operation
|
|
main.menu.edit.redo = Redo
|
|
main.menu.edit.redo.desc = Redo the previously undone operation
|
|
main.menu.edit.cut = Cut
|
|
main.menu.edit.copy = Copy
|
|
main.menu.edit.paste = Paste
|
|
main.menu.edit.delete = Delete
|
|
main.menu.edit.resize = Scale...
|
|
main.menu.edit.resize.desc = Scale parts of the rocket design
|
|
main.menu.edit.preferences = Preferences
|
|
main.menu.edit.preferences.desc = Setup the application preferences
|
|
|
|
main.menu.analyze = Analyze
|
|
main.menu.analyze.desc = Rocket analysis
|
|
main.menu.analyze.componentAnalysis = Component analysis
|
|
main.menu.analyze.componentAnalysis.desc = Analyze the rocket components separately
|
|
main.menu.analyze.optimization = Rocket optimization
|
|
main.menu.analyze.optimization.desc = General rocket design optimization
|
|
|
|
main.menu.help = Help
|
|
main.menu.help.desc = Information about OpenRocket
|
|
main.menu.help.tours = Guided tours
|
|
main.menu.help.tours.desc = Take guided tours on OpenRocket
|
|
main.menu.help.license = License
|
|
main.menu.help.license.desc = OpenRocket license information
|
|
main.menu.help.bugReport = Bug report
|
|
main.menu.help.bugReport.desc = Information about reporting bugs in OpenRocket
|
|
main.menu.help.debugLog = Debug log
|
|
main.menu.help.debugLog.desc = View the OpenRocket debug log
|
|
main.menu.help.about = About
|
|
main.menu.help.about.desc = Copyright details about OpenRocket
|
|
|
|
main.menu.debug = Debug
|
|
main.menu.debug.whatisthismenu = What is this menu?
|
|
main.menu.debug.createtestrocket = Create test rocket
|
|
|
|
! database
|
|
! Translate here all material database
|
|
!
|
|
|
|
! Material database
|
|
! BULK_MATERIAL
|
|
Databases.materials.Acrylic = Acrylic
|
|
Databases.materials.Balsa = Balsa
|
|
Databases.materials.Basswood = Basswood
|
|
Databases.materials.Birch = Birch
|
|
Databases.materials.Cardboard = Cardboard
|
|
Databases.materials.Carbonfiber = Carbon fiber
|
|
Databases.materials.Cork = Cork
|
|
Databases.materials.DepronXPS = Depron (XPS)
|
|
Databases.materials.Fiberglass = Fiberglass
|
|
Databases.materials.Kraftphenolic = Kraft phenolic
|
|
Databases.materials.Maple = Maple
|
|
Databases.materials.Paperoffice = Paper (office)
|
|
Databases.materials.Pine = Pine
|
|
Databases.materials.Plywoodbirch = Plywood (birch)
|
|
Databases.materials.PolycarbonateLexan = Polycarbonate (Lexan)
|
|
Databases.materials.Polystyrene = Polystyrene
|
|
Databases.materials.PVC = PVC
|
|
Databases.materials.Spruce = Spruce
|
|
Databases.materials.StyrofoamgenericEPS = Styrofoam (generic EPS)
|
|
Databases.materials.StyrofoamBluefoamXPS = Styrofoam \"Blue foam\" (XPS)
|
|
Databases.materials.Quantumtubing = Quantum tubing
|
|
Databases.materials.BlueTube = Blue tube
|
|
!SURFACE_MATERIAL
|
|
Databases.materials.Ripstopnylon = Ripstop nylon
|
|
Databases.materials.Mylar = Mylar
|
|
Databases.materials.Polyethylenethin = Polyethylene (thin)
|
|
Databases.materials.Polyethyleneheavy = Polyethylene (heavy)
|
|
Databases.materials.Silk = Silk
|
|
Databases.materials.Paperoffice = Paper (office)
|
|
Databases.materials.Cellophane = Cellophane
|
|
Databases.materials.Crepepaper = Cr\u00eape paper
|
|
! LINE_MATERIAL
|
|
Databases.materials.Threadheavy-duty = Thread (heavy-duty)
|
|
Databases.materials.Elasticcordround2mm = Elastic cord (round 2mm, 1/16 in)
|
|
Databases.materials.Elasticcordflat6mm = Elastic cord (flat 6mm, 1/4 in)
|
|
Databases.materials.Elasticcordflat12mm = Elastic cord (flat 12mm, 1/2 in)
|
|
Databases.materials.Elasticcordflat19mm = Elastic cord (flat 19mm, 3/4 in)
|
|
Databases.materials.Elasticcordflat25mm = Elastic cord (flat 25mm, 1 in)
|
|
Databases.materials.Braidednylon2mm = Braided nylon (2 mm, 1/16 in)
|
|
Databases.materials.Braidednylon3mm = Braided nylon (3 mm, 1/8 in)
|
|
Databases.materials.Tubularnylon11mm = Tubular nylon (11 mm, 7/16 in)
|
|
Databases.materials.Tubularnylon14mm = Tubular nylon (14 mm, 9/16 in)
|
|
Databases.materials.Tubularnylon25mm = Tubular nylon (25 mm, 1 in)
|
|
|
|
! ExternalComponent
|
|
ExternalComponent.Rough = Rough
|
|
ExternalComponent.Unfinished = Unfinished
|
|
ExternalComponent.Regularpaint = Regular paint
|
|
ExternalComponent.Smoothpaint = Smooth paint
|
|
ExternalComponent.Polished = Polished
|
|
|
|
! LineStyle
|
|
LineStyle.Solid = Solid
|
|
LineStyle.Dashed = Dashed
|
|
LineStyle.Dotted = Dotted
|
|
LineStyle.Dash-dotted = Dash-dotted
|
|
LineStyle.Defaultstyle = Default style
|
|
|
|
! Shape
|
|
Shape.Conical = Conical
|
|
Shape.Conical.desc1 = A conical nose cone has a profile of a triangle.
|
|
Shape.Conical.desc2 = A conical transition has straight sides.
|
|
Shape.Ogive = Ogive
|
|
Shape.Ogive.desc1 = An ogive nose cone has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube, values less than 1 produce <b>secant ogives</b>.
|
|
Shape.Ogive.desc2 = An ogive transition has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube at the aft end, values less than 1 produce <b>secant ogives</b>.
|
|
Shape.Ellipsoid = Ellipsoid
|
|
Shape.Ellipsoid.desc1 = An ellipsoidal nose cone has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>.
|
|
Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>. If the transition is not clipped, then the profile is extended at the center by the corresponding radius.
|
|
Shape.Powerseries = Power series
|
|
Shape.Powerseries.desc1 = A power series nose cone has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 this is a <b>\u00BD-power</b> or <b>parabolic</b> nose cone, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 a <b>conical</b> nose cone.
|
|
Shape.Powerseries.desc2 = A power series transition has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 the transition is <b>\u00BD-power</b> or <b>parabolic</b>, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 <b>conical</b>.
|
|
Shape.Parabolicseries = Parabolic series
|
|
Shape.Parabolicseries.desc1 = A parabolic series nose cone has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> nose cone.
|
|
Shape.Parabolicseries.desc2 = A parabolic series transition has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube at the aft end, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> transition.
|
|
Shape.Haackseries = Haack series
|
|
Shape.Haackseries.desc1 = The Haack series nose cones are designed to minimize drag. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> nose cone, which minimizes drag for fixed length and diameter, while a value of 0.333 produces an <b>LV-Haack</b> nose cone, which minimizes drag for fixed length and volume.
|
|
Shape.Haackseries.desc2 = The Haack series <i>nose cones</i> are designed to minimize drag. These transition shapes are their equivalents, but do not necessarily produce optimal drag for transitions. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> shape, while a value of 0.333 produces an <b>LV-Haack</b> shape.
|
|
|
|
|
|
! RocketComponent
|
|
RocketComponent.Position.TOP = Top of the parent component
|
|
RocketComponent.Position.MIDDLE = Middle of the parent component
|
|
RocketComponent.Position.BOTTOM = Bottom of the parent component
|
|
RocketComponent.Position.AFTER = After the parent component
|
|
RocketComponent.Position.ABSOLUTE = Tip of the nose cone
|
|
|
|
! LaunchLug
|
|
LaunchLug.Launchlug = Launch lug
|
|
! NoseCone
|
|
NoseCone.NoseCone = Nose cone
|
|
! Transition
|
|
Transition.Transition = Transition
|
|
!Stage
|
|
Stage.Stage = Stage
|
|
! BodyTube
|
|
BodyTube.BodyTube = Body tube
|
|
! TubeCoupler
|
|
TubeCoupler.TubeCoupler = Tube coupler
|
|
!InnerTube
|
|
InnerTube.InnerTube = Inner Tube
|
|
! TrapezoidFinSet
|
|
TrapezoidFinSet.TrapezoidFinSet = Trapezoidal fin set
|
|
! FreeformFinSet
|
|
FreeformFinSet.FreeformFinSet = Freeform fin set
|
|
!MassComponent
|
|
MassComponent.MassComponent = Mass component
|
|
! Parachute
|
|
Parachute.Parachute = Parachute
|
|
! ShockCord
|
|
ShockCord.ShockCord = Shock cord
|
|
! Bulkhead
|
|
Bulkhead.Bulkhead = Bulkhead
|
|
|
|
!Rocket
|
|
Rocket.motorCount.Nomotor = [No motors]
|
|
Rocket.compname.Rocket = Rocket
|
|
|
|
!MotorMount
|
|
MotorMount.IgnitionEvent.AUTOMATIC = Automatic (launch or ejection charge)
|
|
MotorMount.IgnitionEvent.LAUNCH = Launch
|
|
MotorMount.IgnitionEvent.EJECTION_CHARGE = First ejection charge of previous stage
|
|
MotorMount.IgnitionEvent.BURNOUT = First burnout of previous stage
|
|
MotorMount.IgnitionEvent.NEVER = Never
|
|
|
|
!ComponentIcons
|
|
ComponentIcons.Nosecone = Nose cone
|
|
ComponentIcons.Bodytube = Body tube
|
|
ComponentIcons.Transition = Transition
|
|
ComponentIcons.Trapezoidalfinset = Trapezoidal fin set
|
|
ComponentIcons.Ellipticalfinset = Elliptical fin set
|
|
ComponentIcons.Freeformfinset = Freeform fin set
|
|
ComponentIcons.Launchlug = Launch lug
|
|
ComponentIcons.Innertube = Inner tube
|
|
ComponentIcons.Tubecoupler = Tube coupler
|
|
ComponentIcons.Centeringring = Centering ring
|
|
ComponentIcons.Bulkhead = Bulk head
|
|
ComponentIcons.Engineblock = Engine block
|
|
ComponentIcons.Parachute = Parachute
|
|
ComponentIcons.Streamer = Streamer
|
|
ComponentIcons.Shockcord = Shock cord
|
|
ComponentIcons.Masscomponent = Mass component
|
|
ComponentIcons.disabled = (disabled)
|
|
|
|
! StageAction
|
|
StageAction.Stage = Stage
|
|
|
|
! RecoveryDevice
|
|
RecoveryDevice.DeployEvent.LAUNCH = Launch (plus NN seconds)
|
|
RecoveryDevice.DeployEvent.EJECTION = First ejection charge of this stage
|
|
RecoveryDevice.DeployEvent.APOGEE = Apogee
|
|
RecoveryDevice.DeployEvent.ALTITUDE = Specific altitude during descent
|
|
RecoveryDevice.DeployEvent.NEVER = Never
|
|
|
|
! FlightEvent
|
|
FlightEvent.Type.LAUNCH = Launch
|
|
FlightEvent.Type.IGNITION = Motor ignition
|
|
FlightEvent.Type.LIFTOFF = Lift-off
|
|
FlightEvent.Type.LAUNCHROD = Launch rod clearance
|
|
FlightEvent.Type.BURNOUT = Motor burnout
|
|
FlightEvent.Type.EJECTION_CHARGE = Ejection charge
|
|
FlightEvent.Type.STAGE_SEPARATION = Stage separation
|
|
FlightEvent.Type.APOGEE = Apogee
|
|
FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Recovery device deployment
|
|
FlightEvent.Type.GROUND_HIT = Ground hit
|
|
FlightEvent.Type.SIMULATION_END = Simulation end
|
|
FlightEvent.Type.ALTITUDE = Altitude change
|
|
|
|
! ThrustCurveMotorColumns
|
|
TCurveMotorCol.MANUFACTURER = Manufacturer
|
|
TCurveMotorCol.DESIGNATION = Designation
|
|
TCurveMotorCol.TYPE = Type
|
|
TCurveMotorCol.DIAMETER = Diameter
|
|
TCurveMotorCol.LENGTH = Length
|
|
|
|
! RocketInfo
|
|
RocketInfo.lengthLine.Length = Length
|
|
RocketInfo.lengthLine.maxdiameter = , max. diameter
|
|
RocketInfo.massText1 = Mass with motors
|
|
RocketInfo.massText2 = Mass with no motors
|
|
RocketInfo.at = at M=
|
|
RocketInfo.cgText = CG:
|
|
RocketInfo.cpText = CP:
|
|
RocketInfo.stabText = Stability:
|
|
RocketInfo.Warning = Warning:
|
|
RocketInfo.Calculating = Calculating...
|
|
RocketInfo.Apogee = Apogee:
|
|
RocketInfo.Maxvelocity = Max. velocity:
|
|
RocketInfo.Maxacceleration = Max. acceleration:
|
|
RocketInfo.apogeeValue = N/A
|
|
RocketInfo.Mach = (Mach
|
|
RocketInfo.velocityValue = N/A
|
|
RocketInfo.accelerationValue = N/A
|
|
|
|
! FinSet
|
|
FinSet.CrossSection.SQUARE = Square
|
|
FinSet.CrossSection.ROUNDED = Rounded
|
|
FinSet.CrossSection.AIRFOIL = Airfoil
|
|
FinSet.TabRelativePosition.FRONT = Root chord leading edge
|
|
FinSet.TabRelativePosition.CENTER = Root chord midpoint
|
|
FinSet.TabRelativePosition.END = Root chord trailing edge
|
|
|
|
! FlightDataType
|
|
FlightDataType.TYPE_TIME = Time
|
|
FlightDataType.TYPE_ALTITUDE = Altitude
|
|
FlightDataType.TYPE_VELOCITY_Z = Vertical velocity
|
|
FlightDataType.TYPE_ACCELERATION_Z = Vertical acceleration
|
|
FlightDataType.TYPE_VELOCITY_TOTAL = Total velocity
|
|
FlightDataType.TYPE_ACCELERATION_TOTAL = Total acceleration
|
|
FlightDataType.TYPE_POSITION_X = Position upwind
|
|
FlightDataType.TYPE_POSITION_Y = Position parallel to wind
|
|
FlightDataType.TYPE_POSITION_XY = Lateral distance
|
|
FlightDataType.TYPE_POSITION_DIRECTION = Lateral direction
|
|
FlightDataType.TYPE_VELOCITY_XY = Lateral velocity
|
|
FlightDataType.TYPE_ACCELERATION_XY = Lateral acceleration
|
|
FlightDataType.TYPE_AOA = Angle of attack
|
|
FlightDataType.TYPE_ROLL_RATE = Roll rate
|
|
FlightDataType.TYPE_PITCH_RATE = Pitch rate
|
|
FlightDataType.TYPE_YAW_RATE = Yaw rate
|
|
FlightDataType.TYPE_MASS = Mass
|
|
FlightDataType.TYPE_LONGITUDINAL_INERTIA = Longitudinal moment of inertia
|
|
FlightDataType.TYPE_ROTATIONAL_INERTIA = Rotational moment of inertia
|
|
FlightDataType.TYPE_CP_LOCATION = CP location
|
|
FlightDataType.TYPE_CG_LOCATION = CG location
|
|
FlightDataType.TYPE_STABILITY = Stability margin calibers
|
|
FlightDataType.TYPE_MACH_NUMBER = Mach number
|
|
FlightDataType.TYPE_REYNOLDS_NUMBER = Reynolds number
|
|
FlightDataType.TYPE_THRUST_FORCE = Thrust
|
|
FlightDataType.TYPE_DRAG_FORCE = Drag force
|
|
FlightDataType.TYPE_DRAG_COEFF = Drag coefficient
|
|
FlightDataType.TYPE_AXIAL_DRAG_COEFF = Axial drag coefficient
|
|
FlightDataType.TYPE_FRICTION_DRAG_COEFF = Friction drag coefficient
|
|
FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Pressure drag coefficient
|
|
FlightDataType.TYPE_BASE_DRAG_COEFF = Base drag coefficient
|
|
FlightDataType.TYPE_NORMAL_FORCE_COEFF = Normal force coefficient
|
|
FlightDataType.TYPE_PITCH_MOMENT_COEFF = Pitch moment coefficient
|
|
FlightDataType.TYPE_YAW_MOMENT_COEFF = Yaw moment coefficient
|
|
FlightDataType.TYPE_SIDE_FORCE_COEFF = Side force coefficient
|
|
FlightDataType.TYPE_ROLL_MOMENT_COEFF = Roll moment coefficient
|
|
FlightDataType.TYPE_ROLL_FORCING_COEFF = Roll forcing coefficient
|
|
FlightDataType.TYPE_ROLL_DAMPING_COEFF = Roll damping coefficient
|
|
FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Pitch damping coefficient
|
|
FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Yaw damping coefficient
|
|
FlightDataType.TYPE_REFERENCE_LENGTH = Reference lenght
|
|
FlightDataType.TYPE_REFERENCE_AREA = Reference area
|
|
FlightDataType.TYPE_ORIENTATION_THETA = Vertical orientation (zenith)
|
|
FlightDataType.TYPE_ORIENTATION_PHI = Lateral orientation (azimuth)
|
|
FlightDataType.TYPE_WIND_VELOCITY = Wind velocity
|
|
FlightDataType.TYPE_AIR_TEMPERATURE = Air temperature
|
|
FlightDataType.TYPE_AIR_PRESSURE = Air pressure
|
|
FlightDataType.TYPE_SPEED_OF_SOUND = Speed of sound
|
|
FlightDataType.TYPE_TIME_STEP = Simulation time step
|
|
FlightDataType.TYPE_COMPUTATION_TIME = Computation time
|
|
FlightDataType.TYPE_LATITUDE = Latitude
|
|
FlightDataType.TYPE_LONGITUDE = Longitude
|
|
FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration
|
|
|
|
! PlotConfiguration
|
|
PlotConfiguration.Verticalmotion = Vertical motion vs. time
|
|
PlotConfiguration.Totalmotion = Total motion vs. time
|
|
PlotConfiguration.Flightside = Flight side profile
|
|
PlotConfiguration.Stability = Stability vs. time
|
|
PlotConfiguration.Dragcoef = Drag coefficients vs. Mach number
|
|
PlotConfiguration.Rollcharacteristics = Roll characteristics
|
|
PlotConfiguration.Angleofattack = Angle of attack and orientation vs. time
|
|
PlotConfiguration.Simulationtime = Simulation time step and computation time
|
|
|
|
! Warning
|
|
Warning.LargeAOA.str1 = Large angle of attack encountered.
|
|
Warning.LargeAOA.str2 = Large angle of attack encountered (
|
|
Warning.DISCONTINUITY = Discontinuity in rocket body diameter.
|
|
Warning.THICK_FIN = Thick fins may not be modeled accurately.
|
|
Warning.JAGGED_EDGED_FIN = Jagged-edged fin predictions may be inaccurate.
|
|
Warning.LISTENERS_AFFECTED = Listeners modified the flight simulation
|
|
Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Recovery device opened while motor still burning.
|
|
Warning.FILE_INVALID_PARAMETER = Invalid parameter encountered, ignoring.
|
|
|
|
|
|
! Scale dialog
|
|
ScaleDialog.lbl.scaleRocket = Entire rocket
|
|
ScaleDialog.lbl.scaleSubselection = Selection and all subcomponents
|
|
ScaleDialog.lbl.scaleSelection = Only selected component
|
|
ScaleDialog.title = Scale design
|
|
ScaleDialog.lbl.scale = Scale:
|
|
ScaleDialog.lbl.scale.ttip = Select whether to scale the entire design or only the selected component
|
|
ScaleDialog.lbl.scaling = Scaling to apply:
|
|
ScaleDialog.lbl.scaling.ttip = Resulting size, values above 100% grow and values below 100% shrink the design.
|
|
! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"
|
|
ScaleDialog.lbl.scaleFrom = Scale from
|
|
ScaleDialog.lbl.scaleTo = to
|
|
ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and resulting length.
|
|
ScaleDialog.checkbox.scaleMass = Update explicit mass values
|
|
ScaleDialog.checkbox.scaleMass.ttip = Scale mass component and override mass values by the cube of the scaling factor
|
|
ScaleDialog.button.scale = Scale
|
|
ScaleDialog.undo.scaleRocket = Scale rocket
|
|
ScaleDialog.undo.scaleComponent = Scale component
|
|
ScaleDialog.undo.scaleComponents = Scale components
|
|
|
|
!icons
|
|
Icons.Undo = Undo
|
|
Icons.Redo = Redo
|
|
|
|
OpenRocketPrintable.Partsdetail = Parts detail
|
|
OpenRocketPrintable.Fintemplates = Fin templates
|
|
OpenRocketPrintable.Transitiontemplates = Transition templates
|
|
OpenRocketPrintable.Noseconetemplates = Nose Cone templates
|
|
OpenRocketPrintable.Finmarkingguide = Fin marking guide
|
|
OpenRocketPrintable.DesignReport = Design Report
|
|
|
|
OpenRocketDocument.Redo = Redo
|
|
OpenRocketDocument.Undo = Undo
|
|
|
|
!EllipticalFinSet
|
|
EllipticalFinSet.Ellipticalfinset = Elliptical fin set
|
|
|
|
! Optimization
|
|
|
|
! Modifiers
|
|
|
|
optimization.modifier.nosecone.length = Length
|
|
optimization.modifier.nosecone.length.desc = Optimize the nose cone length.
|
|
optimization.modifier.nosecone.diameter = Diameter
|
|
optimization.modifier.nosecone.diameter.desc = Optimize the nose cone base diameter.
|
|
optimization.modifier.nosecone.thickness = Thickness
|
|
optimization.modifier.nosecone.thickness.desc = Optimize the nose cone wall thickness.
|
|
optimization.modifier.nosecone.shapeparameter = Shape parameter
|
|
optimization.modifier.nosecone.shapeparameter.desc = Optimize the nose cone shape parameter.
|
|
|
|
optimization.modifier.transition.length = Length
|
|
optimization.modifier.transition.length.desc = Optimize the transition length.
|
|
optimization.modifier.transition.forediameter = Fore diameter
|
|
optimization.modifier.transition.forediameter.desc = Optimize the transition fore diameter.
|
|
optimization.modifier.transition.aftdiameter = Aft diameter
|
|
optimization.modifier.transition.aftdiameter.desc = Optimize the transition aft diameter.
|
|
optimization.modifier.transition.thickness = Thickness
|
|
optimization.modifier.transition.thickness.desc = Optimize the transition wall thickness.
|
|
optimization.modifier.transition.shapeparameter = Shape parameter
|
|
optimization.modifier.transition.shapeparameter.desc = Optimize the transition shape parameter.
|
|
|
|
optimization.modifier.bodytube.length = Length
|
|
optimization.modifier.bodytube.length.desc = Optimize the body tube length.
|
|
optimization.modifier.bodytube.outerDiameter = Outer diameter
|
|
optimization.modifier.bodytube.outerDiameter.desc = Optimize the body tube outer diameter while maintaining the wall thickness.
|
|
optimization.modifier.bodytube.thickness = Thickness
|
|
optimization.modifier.bodytube.thickness.desc = Optimize the body tube wall thickness.
|
|
|
|
optimization.modifier.trapezoidfinset.rootChord = Root chord
|
|
optimization.modifier.trapezoidfinset.rootChord.desc = Optimize the root chord length of the fin set (length of fin at the rocket body).
|
|
optimization.modifier.trapezoidfinset.tipChord = Tip chord
|
|
optimization.modifier.trapezoidfinset.tipChord.desc = Optimize the tip chord length of the fin set (length of fin at outer edge).
|
|
optimization.modifier.trapezoidfinset.sweep = Sweep
|
|
optimization.modifier.trapezoidfinset.sweep.desc = Optimize the sweep of the fin set (distance that the leading edge sweeps backwards).
|
|
optimization.modifier.trapezoidfinset.height = Height
|
|
optimization.modifier.trapezoidfinset.height.desc = Optimize the height (semi-span) of the fin set.
|
|
|
|
optimization.modifier.ellipticalfinset.length = Root chord
|
|
optimization.modifier.ellipticalfinset.length.desc = Optimize the root chord length of the fin set.
|
|
optimization.modifier.ellipticalfinset.height = Height
|
|
optimization.modifier.ellipticalfinset.height.desc = Optimize the height (semi-span) of the fin set.
|
|
|
|
optimization.modifier.finset.cant = Cant angle
|
|
optimization.modifier.finset.cant.desc = Optimize the cant angle of the fin set.
|
|
optimization.modifier.finset.position = Position
|
|
optimization.modifier.finset.position.desc = Optimize the fin set position along the rocket body.
|
|
|
|
optimization.modifier.launchlug.length = Length
|
|
optimization.modifier.launchlug.length.desc = Optimize the launch lug length.
|
|
optimization.modifier.launchlug.outerDiameter = Outer diameter
|
|
optimization.modifier.launchlug.outerDiameter.desc = Optimize the outer diameter of the launch lug.
|
|
optimization.modifier.launchlug.thickness = Thickness
|
|
optimization.modifier.launchlug.thickness.desc = Optimize the launch lug thickness while keeping the outer diameter constant.
|
|
optimization.modifier.launchlug.position = Position
|
|
optimization.modifier.launchlug.position.desc = Optimize the launch lug position along the rocket body.
|
|
|
|
|
|
optimization.modifier.internalcomponent.position = Position
|
|
optimization.modifier.internalcomponent.position.desc = Optimize the position of the component relative to the parent component.
|
|
|
|
optimization.modifier.masscomponent.mass = Mass
|
|
optimization.modifier.masscomponent.mass.desc = Optimize the mass of the mass component.
|
|
|
|
optimization.modifier.parachute.diameter = Diameter
|
|
optimization.modifier.parachute.diameter.desc = Optimize the parachute canopy diameter.
|
|
optimization.modifier.parachute.coefficient = Drag coefficient
|
|
optimization.modifier.parachute.coefficient.desc = Optimize the drag coefficient of the parachute. Typical parachutes have a drag coefficient of about 0.8.
|
|
|
|
optimization.modifier.streamer.length = Length
|
|
optimization.modifier.streamer.length.desc = Optimize the length of the streamer.
|
|
optimization.modifier.streamer.width = Width
|
|
optimization.modifier.streamer.width.desc = Optimize the width of the streamer.
|
|
optimization.modifier.streamer.aspectRatio = Aspect ratio
|
|
optimization.modifier.streamer.aspectRatio.desc = Optimize the aspect ratio of the streamer (length/width). You should NOT select streamer length or width at the same time with the aspect ratio.
|
|
optimization.modifier.streamer.coefficient = Drag coefficient
|
|
optimization.modifier.streamer.coefficient.desc = Optimize the drag coefficient of the streamer.
|
|
|
|
optimization.modifier.recoverydevice.deployDelay = Deployment delay
|
|
optimization.modifier.recoverydevice.deployDelay.desc = Optimize the deployment delay of the recovery device.
|
|
optimization.modifier.recoverydevice.deployAltitude = Deployment altitude
|
|
optimization.modifier.recoverydevice.deployAltitude.desc = Optimize the deployment altitude of the recovery device.
|
|
|
|
optimization.modifier.rocketcomponent.overrideMass = Override mass
|
|
optimization.modifier.rocketcomponent.overrideMass.desc = Optimize the overridden mass of the component.
|
|
optimization.modifier.rocketcomponent.overrideCG = Override CG
|
|
optimization.modifier.rocketcomponent.overrideCG.desc = Optimize the overridden center of gravity of the component.
|
|
|
|
optimization.modifier.motormount.overhang = Motor overhang
|
|
optimization.modifier.motormount.overhang.desc = Optimize the motor overhang.
|
|
optimization.modifier.motormount.delay = Motor ignition delay
|
|
optimization.modifier.motormount.delay.desc = Optimize the motor ignition delay.
|
|
|
|
|
|
|
|
|
|
! General rocket design optimization dialog
|
|
|
|
GeneralOptimizationDialog.title = Rocket optimization
|
|
GeneralOptimizationDialog.goal.maximize = Maximize value
|
|
GeneralOptimizationDialog.goal.minimize = Minimize value
|
|
GeneralOptimizationDialog.goal.seek = Seek value of
|
|
GeneralOptimizationDialog.btn.start = Start optimization
|
|
GeneralOptimizationDialog.btn.stop = Stop optimization
|
|
GeneralOptimizationDialog.lbl.paramsToOptimize = Parameters to optimize:
|
|
GeneralOptimizationDialog.btn.add = Add
|
|
GeneralOptimizationDialog.btn.add.ttip = Add the selected parameter to the optimization
|
|
GeneralOptimizationDialog.btn.remove = Remove
|
|
GeneralOptimizationDialog.btn.remove.ttip = Remove the selected parameter from the optimization
|
|
GeneralOptimizationDialog.btn.removeAll = Remove all
|
|
GeneralOptimizationDialog.btn.removeAll.ttip = Remove all parameters from the optimization
|
|
GeneralOptimizationDialog.lbl.availableParams = Available parameters:
|
|
GeneralOptimizationDialog.lbl.optimizationOpts = Optimization options
|
|
GeneralOptimizationDialog.lbl.optimizeSim = Optimize simulation:
|
|
GeneralOptimizationDialog.lbl.optimizeSim.ttip = Select which simulation to optimize
|
|
GeneralOptimizationDialog.lbl.optimizeValue = Optimized value:
|
|
GeneralOptimizationDialog.lbl.optimizeValue.ttip = Select what value is to be optimized
|
|
GeneralOptimizationDialog.lbl.optimizeGoal = Optimization goal:
|
|
GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Select the goal of the optimization
|
|
GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Custom value to seek
|
|
GeneralOptimizationDialog.lbl.requireStability = Required stability
|
|
GeneralOptimizationDialog.lbl.requireMinStability = Minimum stability:
|
|
GeneralOptimizationDialog.lbl.requireMinStability.ttip = Require a minimum static stability margin for the design
|
|
GeneralOptimizationDialog.lbl.requireMaxStability = Maximum stability:
|
|
GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Require a maximum static stability margin for the design
|
|
GeneralOptimizationDialog.status.bestValue = Best value:
|
|
GeneralOptimizationDialog.status.bestValue.ttip = Best optimization value found so far.
|
|
GeneralOptimizationDialog.status.stepCount = Step count:
|
|
GeneralOptimizationDialog.status.stepCount.ttip = Number of optimization steps that have been performed.
|
|
GeneralOptimizationDialog.status.evalCount = Evaluations:
|
|
GeneralOptimizationDialog.status.evalCount.ttip = Total number of function evaluations (simulations) that have been performed.
|
|
GeneralOptimizationDialog.status.stepSize = Step size:
|
|
GeneralOptimizationDialog.status.stepSize.ttip = Current optimization step size (relative to the optimization parameter ranges)
|
|
GeneralOptimizationDialog.btn.plotPath = Plot path
|
|
GeneralOptimizationDialog.btn.plotPath.ttip = Plot the optimization path (one and two dimensional optimization only)
|
|
GeneralOptimizationDialog.btn.save = Save path
|
|
GeneralOptimizationDialog.btn.save.ttip = Save the results of the function evaluations (simulations) as a CSV file.
|
|
GeneralOptimizationDialog.btn.apply = Apply optimization
|
|
GeneralOptimizationDialog.btn.apply.ttip = Apply the optimization results to the rocket design
|
|
GeneralOptimizationDialog.btn.reset = Reset
|
|
GeneralOptimizationDialog.btn.reset.ttip = Reset the rocket design to the current rocket design
|
|
GeneralOptimizationDialog.btn.close = Close
|
|
GeneralOptimizationDialog.btn.close.ttip = Close the dialog without modifying the rocket design
|
|
GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters.
|
|
GeneralOptimizationDialog.error.selectParams.title = Select optimization parameters
|
|
GeneralOptimizationDialog.error.optimizationFailure.text = The optimization failed to run:
|
|
GeneralOptimizationDialog.error.optimizationFailure.title = Optimization failed
|
|
GeneralOptimizationDialog.undoText = Apply optimization
|
|
GeneralOptimizationDialog.basicSimulationName = Basic simulation
|
|
GeneralOptimizationDialog.noSimulationName = No simulation
|
|
GeneralOptimizationDialog.table.col.parameter = Parameter
|
|
GeneralOptimizationDialog.table.col.current = Current
|
|
GeneralOptimizationDialog.table.col.min = Minimum
|
|
GeneralOptimizationDialog.table.col.max = Maximum
|
|
GeneralOptimizationDialog.export.header = Include header line
|
|
GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions.
|
|
GeneralOptimizationDialog.export.stability = Stability
|
|
|
|
|
|
! Dialog for plotting optimization results
|
|
OptimizationPlotDialog.title = Optimization results
|
|
OptimizationPlotDialog.lbl.zoomInstructions = Click and drag down+right to zoom in, up+left to zoom out
|
|
OptimizationPlotDialog.plot1d.title = Optimization result
|
|
OptimizationPlotDialog.plot1d.series = Optimization result
|
|
OptimizationPlotDialog.plot2d.title = Optimization path
|
|
OptimizationPlotDialog.plot2d.path = Optimization path
|
|
OptimizationPlotDialog.plot2d.evals = Evaluations
|
|
OptimizationPlotDialog.plot.ttip.stability = Stability:
|
|
OptimizationPlotDialog.plot.label.optimum = Optimum
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! Optimization parameters
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MaximumAltitudeParameter.name = Apogee altitude
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MaximumVelocityParameter.name = Maximum velocity
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MaximumAccelerationParameter.name = Maximum acceleration
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StabilityParameter.name = Stability
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GroundHitVelocityParameter.name = Ground hit speed
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LandingDistanceParameter.name = Landing distance
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TotalFlightTimeParameter.name = Total flight time
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DeploymentVelocityParameter.name = Velocity at parachute deployment
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! Compass directions drawn on a compass rose.
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CompassRose.lbl.north = N
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CompassRose.lbl.east = E
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CompassRose.lbl.south = S
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CompassRose.lbl.west = W
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! Compass directions with subdirections. These might not be localized even if the directions on the compass rose are.
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CompassSelectionButton.lbl.N = N
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CompassSelectionButton.lbl.NE = NE
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CompassSelectionButton.lbl.E = E
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CompassSelectionButton.lbl.SE = SE
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CompassSelectionButton.lbl.S = S
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CompassSelectionButton.lbl.SW = SW
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CompassSelectionButton.lbl.W = W
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CompassSelectionButton.lbl.NW = NW
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SlideShowDialog.btn.next = Next
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SlideShowDialog.btn.prev = Previous
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GuidedTourSelectionDialog.title = Guided tours
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GuidedTourSelectionDialog.lbl.selectTour = Select guided tour:
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GuidedTourSelectionDialog.lbl.description = Tour description:
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GuidedTourSelectionDialog.lbl.length = Number of slides:
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GuidedTourSelectionDialog.btn.start = Start tour!
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