1547 lines
74 KiB
Properties
1547 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
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simpanel.lbl.defpref = You can change the default operation in the preferences.
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simpanel.dlg.lbl.DeleteSim1 = Delete the selected simulations?
|
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simpanel.dlg.lbl.DeleteSim2 = <html><i>This operation cannot be undone.</i>
|
|
simpanel.dlg.lbl.DeleteSim3 = Delete simulations
|
|
simpanel.col.Name = Name
|
|
simpanel.col.Motors = Motors
|
|
simpanel.col.Apogee = Apogee
|
|
simpanel.col.Maxvelocity = Max. velocity
|
|
simpanel.col.Maxacceleration = Max. acceleration
|
|
simpanel.col.Timetoapogee = Time to apogee
|
|
simpanel.col.Flighttime = Flight time
|
|
simpanel.col.Groundhitvelocity = Ground hit velocity
|
|
|
|
! SimulationRunDialog
|
|
SimuRunDlg.title.RunSim = Running simulations...
|
|
SimuRunDlg.lbl.Running = Running ...
|
|
SimuRunDlg.lbl.Simutime = Simulation time:
|
|
SimuRunDlg.lbl.Altitude = Altitude:
|
|
SimuRunDlg.lbl.Velocity = Velocity:
|
|
SimuRunDlg.msg.Unabletosim = Unable to simulate:
|
|
SimuRunDlg.msg.errorOccurred = An error occurred during the simulation:
|
|
SimuRunDlg.msg.AnException1 = An exception occurred during the simulation:
|
|
SimuRunDlg.msg.AnException2 = Please report this as a bug along with the details below.
|
|
SimuRunDlg.msg.AssertionError1 = A computation error occurred during the simulation.
|
|
SimuRunDlg.msg.AssertionError2 = Please report this as a bug along with the details below.
|
|
SimuRunDlg.msg.unknownerror1 = An unknown error was encountered during the simulation.
|
|
SimuRunDlg.msg.unknownerror2 = The program may be unstable, you should save all your designs and restart OpenRocket now!
|
|
|
|
|
|
RK4SimulationStepper.error.valuesTooLarge = Simulation values exceeded limits. Try selecting a shorter time step.
|
|
|
|
|
|
! SimulationExportPanel
|
|
SimExpPan.desc = Comma Separated Files (*.csv)
|
|
SimExpPan.border.Vartoexport = Variables to export
|
|
SimExpPan.but.Selectall = Select all
|
|
SimExpPan.but.Selectnone = Select none
|
|
SimExpPan.border.Fieldsep = Field separator
|
|
SimExpPan.lbl.Fieldsepstr = Field separator string:
|
|
SimExpPan.lbl.longA1 = <html>The string used to separate the fields in the exported file.<br>
|
|
SimExpPan.lbl.longA2 = Use ',' for a Comma Separated Values (CSV) file.
|
|
SimExpPan.checkbox.Includesimudesc = Include simulation description
|
|
SimExpPan.checkbox.ttip.Includesimudesc = Include a comment at the beginning of the file describing the simulation.
|
|
SimExpPan.border.Comments = Comments
|
|
SimExpPan.checkbox.Includefielddesc = Include field descriptions
|
|
SimExpPan.checkbox.ttip.Includefielddesc = Include a comment line with the descriptions of the exported variables.
|
|
SimExpPan.checkbox.Incflightevents = Include flight events
|
|
SimExpPan.checkbox.ttip.Incflightevents = Include a comment line for every flight event.
|
|
SimExpPan.lbl.Commentchar = Comment character:
|
|
SimExpPan.lbl.ttip.Commentchar = The character(s) that mark a comment line.
|
|
SimExpPan.but.Exporttofile = Export to file...
|
|
SimExpPan.Fileexists.desc1 = File \"
|
|
SimExpPan.Fileexists.desc2 = \" exists. Overwrite?
|
|
SimExpPan.Fileexists.title = File exists
|
|
SimExpPan.ExportingVar.desc1 = Exporting 1 variable out of
|
|
SimExpPan.ExportingVar.desc2 = Exporting
|
|
SimExpPan.ExportingVar.desc3 = variables out of
|
|
SimExpPan.Col.Variable = Variable
|
|
SimExpPan.Col.Unit = Unit
|
|
|
|
|
|
CsvOptionPanel.separator.space = SPACE
|
|
CsvOptionPanel.separator.tab = TAB
|
|
|
|
|
|
|
|
! MotorPlot
|
|
MotorPlot.title.Motorplot = Motor plot
|
|
MotorPlot.but.Select = Select
|
|
MotorPlot.Chart.Motorthrustcurve = Motor thrust curve
|
|
MotorPlot.Chart.Time = Time / s
|
|
MotorPlot.Chart.Thrust = Thrust / N
|
|
MotorPlot.txt.Designation = Designation:
|
|
MotorPlot.txt.Manufacturer = Manufacturer:
|
|
MotorPlot.txt.Type = Type:
|
|
MotorPlot.txt.Delays = Delays:
|
|
MotorPlot.txt.Comment = Comment:\n
|
|
|
|
|
|
|
|
! Simulation plot panel
|
|
simplotpanel.lbl.Presetplotconf = Preset plot configurations:
|
|
simplotpanel.lbl.Xaxistype = X axis type:
|
|
simplotpanel.lbl.Unit = Unit:
|
|
simplotpanel.lbl.Yaxistypes = Y axis types:
|
|
simplotpanel.lbl.Flightevents = Flight events:
|
|
simplotpanel.but.All = All
|
|
simplotpanel.but.None = None
|
|
simplotpanel.but.NewYaxisplottype = New Y axis plot type
|
|
simplotpanel.but.Plotflight = Plot flight
|
|
simplotpanel.lbl.Axis = Axis:
|
|
simplotpanel.but.ttip.Removethisplot = Remove this plot
|
|
simplotpanel.Desc = The data will be plotted in time order even if the X axis type is not time.
|
|
simplotpanel.OptionPane.lbl1 = A maximum of 15 plots is allowed.
|
|
simplotpanel.OptionPane.lbl2 = Cannot add plot
|
|
simplotpanel.AUTO_NAME = Auto
|
|
simplotpanel.LEFT_NAME = Left
|
|
simplotpanel.RIGHT_NAME = Right
|
|
simplotpanel.CUSTOM = Custom
|
|
SimulationPlotPanel.error.noPlotSelected = Please add one or more variables to plot on the Y-axis.
|
|
SimulationPlotPanel.error.noPlotSelected.title = Nothing to plot
|
|
|
|
|
|
! Component add buttons
|
|
compaddbuttons.Bodycompandfinsets = Body components and fin sets
|
|
compaddbuttons.Nosecone = Nose cone
|
|
compaddbuttons.Bodytube = Body tube
|
|
compaddbuttons.Transition = Transition
|
|
compaddbuttons.Trapezoidal = Trapezoidal
|
|
compaddbuttons.Elliptical = Elliptical
|
|
compaddbuttons.Freeform = Freeform
|
|
compaddbuttons.Launchlug = Launch lug
|
|
compaddbuttons.Innercomponent = Inner component
|
|
compaddbuttons.Innertube = Inner tube
|
|
compaddbuttons.Coupler = Coupler
|
|
compaddbuttons.Centeringring = Centering\nring
|
|
compaddbuttons.Bulkhead = Bulkhead
|
|
compaddbuttons.Engineblock = Engine\nblock
|
|
compaddbuttons.Massobjects = Mass objects
|
|
compaddbuttons.Parachute = Parachute
|
|
compaddbuttons.Streamer = Streamer
|
|
compaddbuttons.Shockcord = Shock cord
|
|
compaddbuttons.Masscomponent = Mass\ncomponent
|
|
compaddbuttons.Donotaskmeagain = Do not ask me again
|
|
compaddbuttons.Selectcomppos = Select component position
|
|
compaddbuttons.lbl.Youcanchange = You can change the default operation in the preferences.
|
|
compaddbuttons.lbl.insertcomp = Insert the component after the current component or as the last component?
|
|
compaddbuttons.askPosition.Inserthere = Insert here
|
|
compaddbuttons.askPosition.Addtotheend = Add to the end
|
|
compaddbuttons.askPosition.Cancel = Cancel
|
|
|
|
! Component Analysis Dialog
|
|
componentanalysisdlg.componentanalysis = Component analysis
|
|
componentanalysisdlg.lbl.winddir = Wind direction:
|
|
componentanalysisdlg.TitledBorder.warnings = Warnings:
|
|
componentanalysisdlg.ToggleBut.worst = Worst
|
|
componentanalysisdlg.lbl.angleofattack = Angle of attack:
|
|
componentanalysisdlg.lbl.machnumber = Mach number:
|
|
componentanalysisdlg.lbl.rollrate = Roll rate:
|
|
componentanalysisdlg.lbl.activestages = Active stages:
|
|
componentanalysisdlg.lbl.motorconf = Motor configuration:
|
|
componentanalysisdlg.TabStability.Col = Component
|
|
componentanalysisdlg.TabStability = Stability
|
|
componentanalysisdlg.TabStability.ttip = Stability information
|
|
componentanalysisdlg.dragTableModel.Col.Component = Component
|
|
componentanalysisdlg.dragTableModel.Col.Pressure = <html>Pressure C<sub>D</sub>
|
|
componentanalysisdlg.dragTableModel.Col.Base = <html>Base C<sub>D</sub>
|
|
componentanalysisdlg.dragTableModel.Col.friction = <html>Friction C<sub>D</sub>
|
|
componentanalysisdlg.dragTableModel.Col.total = <html>Total C<sub>D</sub>
|
|
componentanalysisdlg.dragTabchar = Drag characteristics
|
|
componentanalysisdlg.dragTabchar.ttip = Drag characteristics
|
|
componentanalysisdlg.rollTableModel.Col.component = Component
|
|
componentanalysisdlg.rollTableModel.Col.rollforc = Roll forcing coefficient
|
|
componentanalysisdlg.rollTableModel.Col.rolldamp = Roll damping coefficient
|
|
componentanalysisdlg.rollTableModel.Col.total = <html>Total C<sub>l</sub>
|
|
componentanalysisdlg.rollTableModel = Roll dynamics
|
|
componentanalysisdlg.rollTableModel.ttip = Roll dynamics
|
|
componentanalysisdlg.println.closingmethod = Closing method called:
|
|
componentanalysisdlg.println.settingnam = SETTING NAN VALUES
|
|
componentanalysisdlg.lbl.reflenght = Reference length:
|
|
componentanalysisdlg.lbl.refarea = Reference area:
|
|
!componentanalysisdlg.But.close =Close
|
|
componentanalysisdlg.TabStability.Col.Component = Component
|
|
|
|
! Custom Material dialog
|
|
custmatdlg.title.Custommaterial = Custom material
|
|
custmatdlg.lbl.Materialname = Material name:
|
|
custmatdlg.lbl.Materialtype = Material type:
|
|
custmatdlg.lbl.Materialdensity = Material density:
|
|
custmatdlg.checkbox.Addmaterial = Add material to database
|
|
|
|
|
|
! Ring Component Config
|
|
ringcompcfg.OuterRadius = OuterRadius
|
|
ringcompcfg.Automatic = Automatic
|
|
ringcompcfg.InnerRadius = InnerRadius
|
|
ringcompcfg.Thickness = Thickness
|
|
ringcompcfg.Length = Length
|
|
ringcompcfg.Positionrelativeto = Position relative to:
|
|
ringcompcfg.plus = plus
|
|
ringcompcfg.PositionValue = PositionValue
|
|
ringcompcfg.Radialdistance = Radial distance:
|
|
ringcompcfg.Distancefrom = Distance from the rocket centerline
|
|
ringcompcfg.Radialdirection = Radial direction:
|
|
ringcompcfg.radialdirectionfrom = The radial direction from the rocket centerline
|
|
ringcompcfg.but.Reset = Reset
|
|
ringcompcfg.but.Resetcomponant = Reset the component to the rocket centerline
|
|
ringcompcfg.EngineBlock.desc = <html>An <b>engine block</b> stops the motor from moving forwards in the motor mount tube.<br><br>In order to add a motor, create a <b>body tube</b> or <b>inner tube</b> and mark it as a motor mount in the <em>Motor</em> tab.
|
|
ringcompcfg.note.desc = Note: An inner tube will not affect the aerodynamics of the rocket even if it is located outside of the body tube.
|
|
|
|
|
|
! Body Tube Config
|
|
BodyTubecfg.lbl.Bodytubelength = Body tube length:
|
|
BodyTubecfg.lbl.Outerdiameter = Outer diameter:
|
|
BodyTubecfg.lbl.Innerdiameter = Inner diameter:
|
|
BodyTubecfg.lbl.Wallthickness = Wall thickness:
|
|
BodyTubecfg.tab.General = General
|
|
BodyTubecfg.tab.Generalproperties = General properties
|
|
BodyTubecfg.tab.Motor = Motor
|
|
BodyTubecfg.tab.Motormountconf = Motor mount configuration
|
|
BodyTubecfg.checkbox.Automatic = Automatic
|
|
BodyTubecfg.checkbox.Filled = Filled
|
|
|
|
! FinSetConfig
|
|
FinSetConfig.tab.Fintabs = Fin tabs
|
|
FinSetConfig.tab.Through-the-wall = Through-the-wall fin tabs
|
|
FinSetConfig.but.Converttofreeform = Convert to freeform
|
|
FinSetConfig.but.Converttofreeform.ttip = Convert this fin set into a freeform fin set
|
|
FinSetConfig.Convertfinset = Convert fin set
|
|
FinSetConfig.but.Splitfins = Split fins
|
|
FinSetConfig.but.Splitfins.ttip = Split the fin set into separate fins
|
|
FinSetConfig.but.AutoCalc = Calculate automatically
|
|
FinSetConfig.lbl.Through-the-wall = Through-the-wall fin tabs:
|
|
FinSetConfig.lbl.Tablength = Tab length:
|
|
FinSetConfig.ttip.Tablength = The length of the fin tab.
|
|
FinSetConfig.lbl.Tabheight = Tab height:
|
|
FinSetConfig.ttip.Tabheight = The spanwise height of the fin tab.
|
|
FinSetConfig.lbl.Tabposition = Tab position:
|
|
FinSetConfig.ttip.Tabposition = The position of the fin tab.
|
|
FinSetConfig.lbl.relativeto = relative to
|
|
|
|
!FinMarkingGuide
|
|
FinMarkingGuide.lbl.Front = Front
|
|
|
|
! MotorDatabaseLoadingDialog
|
|
MotorDbLoadDlg.title = Loading motors
|
|
MotorDbLoadDlg.Loadingmotors = Loading motors...
|
|
|
|
! RocketConfig
|
|
RocketCfg.lbl.Designname = Design name:
|
|
RocketCfg.lbl.Designer = Designer:
|
|
RocketCfg.lbl.Comments = Comments:
|
|
RocketCfg.lbl.Revisionhistory = Revision history:
|
|
RocketCfg.lbl.Material = Material:
|
|
|
|
! ShockCordConfig
|
|
ShockCordCfg.lbl.Shockcordlength = Shock cord length:
|
|
|
|
! RocketComponentConfig
|
|
RocketCompCfg.lbl.Componentname = Component name:
|
|
RocketCompCfg.ttip.Thecomponentname = The component name.
|
|
RocketCompCfg.tab.Override = Override
|
|
RocketCompCfg.tab.MassandCGoverride = Mass and CG override options
|
|
RocketCompCfg.tab.Figure = Figure
|
|
RocketCompCfg.tab.Figstyleopt = Figure style options
|
|
RocketCompCfg.tab.Comment = Comment
|
|
RocketCompCfg.tab.Specifyacomment = Specify a comment for the component
|
|
RocketCompCfg.lbl.Mass = Mass:
|
|
RocketCompCfg.lbl.Componentmass = Component mass:
|
|
RocketCompCfg.lbl.overriddento = (overridden to
|
|
RocketCompCfg.lbl.overriddenby = (overridden by
|
|
RocketCompCfg.lbl.Componentmaterial = Component material:
|
|
RocketCompCfg.lbl.Componentfinish = Component finish:
|
|
RocketCompCfg.lbl.ttip.componentmaterialaffects = The component material affects the weight of the component.
|
|
RocketCompCfg.combo.ttip.componentmaterialaffects = The component material affects the weight of the component.
|
|
RocketCompCfg.lbl.longA1 = <html>The component finish affects the aerodynamic drag of the component.<br>
|
|
RocketCompCfg.lbl.longA2 = The value indicated is the average roughness height of the surface.
|
|
RocketCompCfg.but.Setforall = Set for all
|
|
RocketCompCfg.but.ttip.Setforall = Set this finish for all components of the rocket.
|
|
RocketCompCfg.lbl.Overridemassorcenter = Override the mass or center of gravity of the
|
|
RocketCompCfg.checkbox.Overridemass = Override mass:
|
|
RocketCompCfg.checkbox.Overridecenterofgrav = Override center of gravity:
|
|
RocketCompCfg.checkbox.OverridemassandCG = Override mass and CG of all subcomponents
|
|
RocketCompCfg.lbl.longB1 = <html>The overridden mass does not include motors.<br>
|
|
RocketCompCfg.lbl.longB2 = The center of gravity is measured from the front end of the
|
|
RocketCompCfg.lbl.Commentsonthe = Comments on the
|
|
RocketCompCfg.lbl.Figurestyle = Figure style:
|
|
RocketCompCfg.lbl.Componentcolor = Component color:
|
|
RocketCompCfg.lbl.Choosecolor = Choose color
|
|
RocketCompCfg.checkbox.Usedefaultcolor = Use default color
|
|
RocketCompCfg.lbl.Complinestyle = Component line style:
|
|
RocketCompCfg.but.Saveasdefstyle = Save as default style
|
|
RocketCompCfg.lbl.Diameter = Diameter:
|
|
RocketCompCfg.lbl.Length = Length:
|
|
RocketCompCfg.lbl.Thickness = Thickness:
|
|
RocketCompCfg.checkbox.Endcapped = End capped
|
|
RocketCompCfg.ttip.Endcapped = Whether the end of the shoulder is capped.
|
|
RocketCompCfg.title.Noseconeshoulder = Nose cone shoulder
|
|
RocketCompCfg.title.Aftshoulder = Aft shoulder
|
|
RocketCompCfg.border.Foreshoulder = Fore shoulder
|
|
!RocketCompCfg.lbl.Length = Length:
|
|
|
|
! BulkheadConfig
|
|
BulkheadCfg.tab.Diameter = Diameter:
|
|
BulkheadCfg.tab.Thickness = Thickness:
|
|
BulkheadCfg.tab.General = General
|
|
BulkheadCfg.tab.Generalproperties = General properties
|
|
|
|
!CenteringRingConfig
|
|
CenteringRingCfg.tab.Outerdiam = Outer diameter:
|
|
CenteringRingCfg.tab.Innerdiam = Inner diameter:
|
|
CenteringRingCfg.tab.Thickness = Thickness:
|
|
CenteringRingCfg.tab.General = General
|
|
CenteringRingCfg.tab.Generalproperties = General properties
|
|
|
|
!ComponentConfigDialog
|
|
ComponentCfgDlg.configuration = configuration
|
|
ComponentCfgDlg.configuration1 =
|
|
ComponentCfgDlg.Modify = Modify
|
|
|
|
!EllipticalFinSetConfig
|
|
EllipticalFinSetCfg.Nbroffins = Number of fins:
|
|
EllipticalFinSetCfg.Rotation = Rotation:
|
|
EllipticalFinSetCfg.Fincant = Fin cant:
|
|
EllipticalFinSetCfg.Rootchord = Root chord:
|
|
EllipticalFinSetCfg.Height = Height:
|
|
EllipticalFinSetCfg.Positionrelativeto = Position relative to:
|
|
EllipticalFinSetCfg.plus = plus
|
|
EllipticalFinSetCfg.FincrossSection = Fin cross section:
|
|
EllipticalFinSetCfg.Thickness = Thickness:
|
|
EllipticalFinSetCfg.General = General
|
|
EllipticalFinSetCfg.Generalproperties = General properties
|
|
EllipticalFinSetCfg.ttip.Fincant = The angle that the fins are canted with respect to the rocket body.
|
|
|
|
!FreeformFinSetConfig
|
|
FreeformFinSetCfg.tab.General = General
|
|
FreeformFinSetCfg.tab.ttip.General = General properties
|
|
FreeformFinSetCfg.tab.Shape = Shape
|
|
FreeformFinSetCfg.tab.ttip.Finshape = Fin shape
|
|
FreeformFinSetCfg.lbl.Numberoffins = Number of fins:
|
|
FreeformFinSetCfg.lbl.Finrotation = Fin rotation:
|
|
FreeformFinSetCfg.lbl.Fincant = Fin cant:
|
|
FreeformFinSetCfg.lbl.ttip.Fincant = The angle that the fins are canted with respect to the rocket body.
|
|
FreeformFinSetCfg.lbl.Posrelativeto = Position relative to:
|
|
FreeformFinSetCfg.lbl.plus = plus
|
|
FreeformFinSetCfg.lbl.FincrossSection = Fin cross section:
|
|
FreeformFinSetCfg.lbl.Thickness = Thickness:
|
|
! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle
|
|
FreeformFinSetConfig.lbl.doubleClick1 = Double-click
|
|
FreeformFinSetConfig.lbl.doubleClick2 = to edit
|
|
FreeformFinSetConfig.lbl.clickDrag = Click+drag: Add and move points
|
|
FreeformFinSetConfig.lbl.ctrlClick = Ctrl+click: Remove point
|
|
|
|
|
|
!InnerTubeConfig
|
|
InnerTubeCfg.tab.Motor = Motor
|
|
InnerTubeCfg.tab.ttip.Motor = Motor mount configuration
|
|
InnerTubeCfg.tab.Cluster = Cluster
|
|
InnerTubeCfg.tab.ttip.Cluster = Cluster configuration
|
|
InnerTubeCfg.tab.Radialpos = Radial position
|
|
InnerTubeCfg.tab.ttip.Radialpos = Radial position
|
|
InnerTubeCfg.lbl.Selectclustercfg = Select cluster configuration:
|
|
InnerTubeCfg.lbl.TubeSep = Tube separation:
|
|
InnerTubeCfg.lbl.ttip.TubeSep = The separation of the tubes, 1.0 = touching each other
|
|
InnerTubeCfg.lbl.Rotation = Rotation:
|
|
InnerTubeCfg.lbl.ttip.Rotation = Rotation angle of the cluster configuration
|
|
InnerTubeCfg.lbl.Rotangle = Rotation angle of the cluster configuration
|
|
InnerTubeCfg.but.Splitcluster = Split cluster
|
|
InnerTubeCfg.lbl.longA1 = <html>Split the cluster into separate components.<br>
|
|
InnerTubeCfg.lbl.longA2 = This also duplicates all components attached to this inner tube.
|
|
InnerTubeCfg.but.Resetsettings = Reset settings
|
|
InnerTubeCfg.but.ttip.Resetsettings = Reset the separation and rotation to the default values
|
|
|
|
! LaunchLugConfig
|
|
LaunchLugCfg.lbl.Length = Length:
|
|
LaunchLugCfg.lbl.Outerdiam = Outer diameter:
|
|
LaunchLugCfg.lbl.Innerdiam = Inner diameter:
|
|
LaunchLugCfg.lbl.Thickness = Thickness:
|
|
LaunchLugCfg.lbl.Radialpos = Radial position:
|
|
LaunchLugCfg.lbl.Posrelativeto = Position relative to:
|
|
LaunchLugCfg.lbl.plus = plus
|
|
LaunchLugCfg.tab.General = General
|
|
LaunchLugCfg.tab.Generalprop = General properties
|
|
|
|
! MassComponentConfig
|
|
MassComponentCfg.lbl.Mass = Mass:
|
|
MassComponentCfg.lbl.Length = Length:
|
|
MassComponentCfg.lbl.Diameter = Diameter:
|
|
MassComponentCfg.lbl.PosRelativeto = Position relative to:
|
|
MassComponentCfg.lbl.plus = plus
|
|
MassComponentCfg.tab.General = General
|
|
MassComponentCfg.tab.ttip.General = General properties
|
|
MassComponentCfg.tab.Radialpos = Radial position
|
|
MassComponentCfg.tab.ttip.Radialpos = Radial position configuration
|
|
MassComponentCfg.lbl.Radialdistance = Radial distance:
|
|
MassComponentCfg.lbl.Radialdirection = Radial direction:
|
|
MassComponentCfg.but.Reset = Reset
|
|
|
|
! MotorConfig
|
|
MotorCfg.checkbox.compmotormount = This component is a motor mount
|
|
MotorCfg.lbl.Motorcfg = Motor configuration:
|
|
MotorCfg.but.New = New
|
|
MotorCfg.lbl.Currentmotor = Current motor:
|
|
MotorCfg.lbl.Motoroverhang = Motor overhang:
|
|
MotorCfg.lbl.Ignitionat = Ignition at:
|
|
MotorCfg.lbl.plus = plus
|
|
MotorCfg.lbl.seconds = seconds
|
|
MotorCfg.lbl.longA1 = The current design has only one stage.
|
|
MotorCfg.lbl.longA2 = Stages can be added by clicking \"New stage\".
|
|
MotorCfg.lbl.longB1 = The current design has
|
|
MotorCfg.lbl.longB2 = stages.
|
|
MotorCfg.but.Selectmotor = Select motor
|
|
MotorCfg.but.Removemotor = Remove motor
|
|
MotorCfg.lbl.motorLabel = None
|
|
|
|
! NoseConeConfig
|
|
NoseConeCfg.lbl.Noseconeshape = Nose cone shape:
|
|
NoseConeCfg.lbl.Shapeparam = Shape parameter:
|
|
NoseConeCfg.lbl.Noseconelength = Nose cone length:
|
|
NoseConeCfg.lbl.Basediam = Base diameter:
|
|
NoseConeCfg.checkbox.Automatic = Automatic
|
|
NoseConeCfg.lbl.Wallthickness = Wall thickness:
|
|
NoseConeCfg.checkbox.Filled = Filled
|
|
NoseConeCfg.tab.General = General
|
|
NoseConeCfg.tab.ttip.General = General properties
|
|
NoseConeCfg.tab.Shoulder = Shoulder
|
|
NoseConeCfg.tab.ttip.Shoulder = Shoulder properties
|
|
|
|
! ParachuteConfig
|
|
ParachuteCfg.lbl.Canopy = Canopy:
|
|
ParachuteCfg.lbl.Diameter = Diameter:
|
|
ParachuteCfg.lbl.Material = Material:
|
|
ParachuteCfg.combo.MaterialModel = The component material affects the weight of the component.
|
|
ParachuteCfg.lbl.longA1 = <html>Drag coefficient C<sub>D</sub>:
|
|
ParachuteCfg.lbl.longB1 = <html>The drag coefficient relative to the total area of the parachute.<br>
|
|
ParachuteCfg.lbl.longB2 = A larger drag coefficient yields a slowed descent rate.
|
|
ParachuteCfg.lbl.longB3 = A typical value for parachutes is 0.8.
|
|
ParachuteCfg.but.Reset = Reset
|
|
ParachuteCfg.lbl.Shroudlines = Shroud lines:
|
|
ParachuteCfg.lbl.Numberoflines = Number of lines:
|
|
ParachuteCfg.lbl.Linelength = Line length:
|
|
ParachuteCfg.lbl.Material = Material:
|
|
ParachuteCfg.lbl.Posrelativeto = Position relative to:
|
|
ParachuteCfg.lbl.plus = plus
|
|
ParachuteCfg.lbl.Packedlength = Packed length:
|
|
ParachuteCfg.lbl.Packeddiam = Packed diameter:
|
|
ParachuteCfg.lbl.Deploysat = Deploys at:
|
|
ParachuteCfg.lbl.seconds = seconds
|
|
ParachuteCfg.lbl.Altitude = Altitude:
|
|
ParachuteCfg.tab.General = General
|
|
ParachuteCfg.tab.ttip.General = General properties
|
|
ParachuteCfg.tab.Radialpos = Radial position
|
|
ParachuteCfg.tab.ttip.Radialpos = Radial position configuration
|
|
ParachuteCfg.lbl.Radialdistance = Radial distance:
|
|
ParachuteCfg.lbl.Radialdirection = Radial direction:
|
|
ParachuteCfg.but.Reset = Reset
|
|
ParachuteCfg.lbl.plusdelay = plus
|
|
|
|
! ShockCordConfig
|
|
ShockCordCfg.lbl.Shockcordlength = Shock cord length:
|
|
ShockCordCfg.lbl.Shockcordmaterial = Shock cord material:
|
|
ShockCordCfg.lbl.Posrelativeto = Position relative to:
|
|
ShockCordCfg.lbl.plus = plus
|
|
ShockCordCfg.lbl.Packedlength = Packed length:
|
|
ShockCordCfg.lbl.Packeddiam = Packed diameter:
|
|
ShockCordCfg.tab.General = General
|
|
ShockCordCfg.tab.ttip.General = General properties
|
|
|
|
!SleeveConfig
|
|
SleeveCfg.tab.Outerdiam = Outer diameter:
|
|
SleeveCfg.tab.Innerdiam = Inner diameter:
|
|
SleeveCfg.tab.Wallthickness = Wall thickness:
|
|
SleeveCfg.tab.Length = Length:
|
|
SleeveCfg.tab.General = General
|
|
SleeveCfg.tab.Generalproperties = General properties
|
|
|
|
! StreamerConfig
|
|
StreamerCfg.lbl.Striplength = Strip length:
|
|
StreamerCfg.lbl.Stripwidth = Strip width:
|
|
StreamerCfg.lbl.Striparea = Strip area:
|
|
StreamerCfg.lbl.Aspectratio = Aspect ratio:
|
|
StreamerCfg.lbl.Material = Material:
|
|
StreamerCfg.combo.ttip.MaterialModel = The component material affects the weight of the component.
|
|
StreamerCfg.lbl.longA1 = <html>Drag coefficient C<sub>D</sub>:
|
|
StreamerCfg.lbl.longB1 = <html>The drag coefficient relative to the total area of the streamer.<br>
|
|
StreamerCfg.lbl.longB2 = A larger drag coefficient yields a slowed descent rate.
|
|
StreamerCfg.lbl.Automatic = Automatic
|
|
StreamerCfg.lbl.longC1 = The drag coefficient is relative to the area of the streamer.
|
|
StreamerCfg.lbl.Posrelativeto = Position relative to:
|
|
StreamerCfg.lbl.plus = plus
|
|
StreamerCfg.lbl.Packedlength = Packed length:
|
|
StreamerCfg.lbl.Packeddiam = Packed diameter:
|
|
StreamerCfg.lbl.Deploysat = Deploys at:
|
|
StreamerCfg.lbl.seconds = seconds
|
|
StreamerCfg.lbl.Altitude = Altitude:
|
|
StreamerCfg.tab.General = General
|
|
StreamerCfg.tab.ttip.General = General properties
|
|
StreamerCfg.tab.Radialpos = Radial position
|
|
StreamerCfg.tab.ttip.Radialpos = Radial position configuration
|
|
StreamerCfg.lbl.Radialdistance = Radial distance:
|
|
StreamerCfg.lbl.Radialdirection = Radial direction:
|
|
StreamerCfg.but.Reset = Reset
|
|
StreamerCfg.lbl.plusdelay = plus
|
|
|
|
! ThicknessRingComponentConfig
|
|
ThicknessRingCompCfg.tab.Outerdiam = Outer diameter:
|
|
ThicknessRingCompCfg.tab.Innerdiam = Inner diameter:
|
|
ThicknessRingCompCfg.tab.Wallthickness = Wall thickness:
|
|
ThicknessRingCompCfg.tab.Length = Length:
|
|
ThicknessRingCompCfg.tab.General = General
|
|
ThicknessRingCompCfg.tab.Generalprop = General properties
|
|
|
|
! TransitionConfig
|
|
TransitionCfg.lbl.Transitionshape = Transition shape:
|
|
TransitionCfg.checkbox.Clipped = Clipped
|
|
TransitionCfg.lbl.Shapeparam = Shape parameter:
|
|
TransitionCfg.lbl.Transitionlength = Transition length:
|
|
TransitionCfg.lbl.Forediam = Fore diameter:
|
|
TransitionCfg.checkbox.Automatic = Automatic
|
|
TransitionCfg.lbl.Aftdiam = Aft diameter:
|
|
TransitionCfg.lbl.Wallthickness = Wall thickness:
|
|
TransitionCfg.checkbox.Filled = Filled
|
|
TransitionCfg.tab.General = General
|
|
TransitionCfg.tab.Generalproperties = General properties
|
|
TransitionCfg.tab.Shoulder = Shoulder
|
|
TransitionCfg.tab.Shoulderproperties = Shoulder properties
|
|
|
|
! TrapezoidFinSetConfig
|
|
TrapezoidFinSetCfg.lbl.Nbroffins = Number of fins:
|
|
TrapezoidFinSetCfg.lbl.ttip.Nbroffins = The number of fins in the fin set.
|
|
TrapezoidFinSetCfg.lbl.Finrotation = Fin rotation:
|
|
TrapezoidFinSetCfg.lbl.ttip.Finrotation = The angle of the first fin in the fin set.
|
|
TrapezoidFinSetCfg.lbl.Fincant = Fin cant:
|
|
TrapezoidFinSetCfg.lbl.ttip.Fincant =The angle that the fins are canted with respect to the rocket body.
|
|
TrapezoidFinSetCfg.lbl.Rootchord = Root chord:
|
|
TrapezoidFinSetCfg.lbl.Tipchord = Tip chord:
|
|
TrapezoidFinSetCfg.lbl.Height = Height:
|
|
TrapezoidFinSetCfg.lbl.Sweeplength = Sweep length:
|
|
TrapezoidFinSetCfg.lbl.Sweepangle = Sweep angle:
|
|
TrapezoidFinSetCfg.lbl.FincrossSection = Fin cross section:
|
|
TrapezoidFinSetCfg.lbl.Thickness = Thickness:
|
|
TrapezoidFinSetCfg.lbl.Posrelativeto = Position relative to:
|
|
TrapezoidFinSetCfg.lbl.plus = plus
|
|
TrapezoidFinSetCfg.tab.General = General
|
|
TrapezoidFinSetCfg.tab.Generalproperties = General properties
|
|
|
|
!MotorConfigurationModel
|
|
MotorCfgModel.Editcfg = Edit configurations
|
|
|
|
! StorageOptionChooser
|
|
StorageOptChooser.lbl.Simdatatostore = Simulated data to store:
|
|
StorageOptChooser.rdbut.Allsimdata = All simulated data
|
|
StorageOptChooser.lbl.longA1 = <html>Store all simulated data.<br>
|
|
StorageOptChooser.lbl.longA2 = This can result in very large files!
|
|
StorageOptChooser.rdbut.Every = Every
|
|
StorageOptChooser.lbl.longB1 = <html>Store plottable values approximately this far apart.<br>
|
|
StorageOptChooser.lbl.longB2 = Larger values result in smaller files.
|
|
StorageOptChooser.lbl.seconds = seconds
|
|
StorageOptChooser.rdbut.Onlyprimfig = Only primary figures
|
|
StorageOptChooser.lbl.longC1 = <html>Store only the values shown in the summary table.<br>
|
|
StorageOptChooser.lbl.longC2 = This results in the smallest files.
|
|
StorageOptChooser.checkbox.Compfile = Compress file
|
|
StorageOptChooser.lbl.UsingComp = Using compression reduces the file size significantly.
|
|
StorageOptChooser.lbl.longD1 = An estimate on how large the resulting file would be with the present options.
|
|
StorageOptChooser.ttip.Saveopt = Save options
|
|
StorageOptChooser.lbl.Estfilesize = Estimated file size:
|
|
StorageOptChooser.lbl.Saveopt = Save options
|
|
|
|
! ThrustCurveMotorSelectionPanel
|
|
TCMotorSelPan.lbl.Selrocketmotor = Select rocket motor:
|
|
TCMotorSelPan.checkbox.hideSimilar = Hide very similar thrust curves
|
|
TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Show all motors
|
|
TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Show motors with diameter less than that of the motor mount
|
|
TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Show motors with diameter equal to that of the motor mount
|
|
TCMotorSelPan.lbl.Motormountdia = Motor mount diameter:
|
|
TCMotorSelPan.lbl.Search = Search:
|
|
TCMotorSelPan.lbl.Selectthrustcurve = Select thrust curve:
|
|
TCMotorSelPan.lbl.Ejectionchargedelay = Ejection charge delay:
|
|
TCMotorSelPan.equalsIgnoreCase.None = None
|
|
TCMotorSelPan.lbl.NumberofsecondsorNone = (Number of seconds or \"None\")
|
|
TCMotorSelPan.lbl.Totalimpulse = Total impulse:
|
|
TCMotorSelPan.lbl.Avgthrust = Avg. thrust:
|
|
TCMotorSelPan.lbl.Maxthrust = Max. thrust:
|
|
TCMotorSelPan.lbl.Burntime = Burn time:
|
|
TCMotorSelPan.lbl.Launchmass = Launch mass:
|
|
TCMotorSelPan.lbl.Emptymass = Empty mass:
|
|
TCMotorSelPan.lbl.Datapoints = Data points:
|
|
TCMotorSelPan.lbl.Digest = Digest:
|
|
TCMotorSelPan.title.Thrustcurve = Thrust curve:
|
|
TCMotorSelPan.title.Thrust = Thrust
|
|
TCMotorSelPan.delayBox.None = None
|
|
|
|
|
|
! PlotDialog
|
|
PlotDialog.title.Flightdataplot = Flight data plot
|
|
PlotDialog.Chart.Simulatedflight = Simulated flight
|
|
PlotDialog.CheckBox.Showdatapoints = Show data points
|
|
PlotDialog.lbl.Chart = Click and drag down+right to zoom in, up+left to zoom out
|
|
|
|
|
|
! "main" prefix is used for the main application dialog
|
|
|
|
# FIXME: Rename the description keys
|
|
|
|
main.menu.file = File
|
|
main.menu.file.desc = File-handling related tasks
|
|
main.menu.file.new = New
|
|
main.menu.file.new.desc = Create a new rocket design
|
|
main.menu.file.open = Open...
|
|
BasicFrame.item.Openrocketdesign = Open a rocket design
|
|
main.menu.file.openExample = Open example...
|
|
BasicFrame.item.Openexamplerocketdesign = Open an example rocket design
|
|
main.menu.file.save = Save
|
|
BasicFrame.item.SavecurRocketdesign = Save the current rocket design
|
|
main.menu.file.saveAs = Save as...
|
|
BasicFrame.item.SavecurRocketdesnewfile = Save the current rocket design to a new file
|
|
main.menu.file.print = Print / Export PDF...
|
|
main.menu.file.print.desc = Print or save as PDF the parts list and fin templates
|
|
main.menu.file.close = Close
|
|
BasicFrame.item.Closedesign = Close the current rocket design
|
|
main.menu.file.quit = Quit
|
|
BasicFrame.item.Quitprogram = Quit the program
|
|
|
|
main.menu.edit = Edit
|
|
BasicFrame.menu.Rocketedt = Rocket editing
|
|
main.menu.edit.undo = Undo
|
|
main.menu.edit.undo.desc = Undo the previous operation
|
|
main.menu.edit.redo = Redo
|
|
main.menu.edit.redo.desc = Redo the previously undone operation
|
|
main.menu.edit.cut = Cut
|
|
main.menu.edit.copy = Copy
|
|
main.menu.edit.paste = Paste
|
|
main.menu.edit.delete = Delete
|
|
main.menu.edit.resize = Scale...
|
|
main.menu.edit.resize.desc = Scale parts of the rocket design
|
|
main.menu.edit.preferences = Preferences
|
|
main.menu.edit.preferences.desc = Setup the application preferences
|
|
|
|
main.menu.analyze = Analyze
|
|
main.menu.analyze.desc = Rocket analysis
|
|
main.menu.analyze.componentAnalysis = Component analysis
|
|
main.menu.analyze.componentAnalysis.desc = Analyze the rocket components separately
|
|
main.menu.analyze.optimization = Rocket optimization
|
|
main.menu.analyze.optimization.desc = General rocket design optimization
|
|
|
|
main.menu.help = Help
|
|
main.menu.help.desc = Information about OpenRocket
|
|
main.menu.help.tours = Guided tours
|
|
main.menu.help.tours.desc = Take guided tours on OpenRocket
|
|
main.menu.help.license = License
|
|
main.menu.help.license.desc = OpenRocket license information
|
|
main.menu.help.bugReport = Bug report
|
|
main.menu.help.bugReport.desc = Information about reporting bugs in OpenRocket
|
|
main.menu.help.debugLog = Debug log
|
|
main.menu.help.debugLog.desc = View the OpenRocket debug log
|
|
main.menu.help.about = About
|
|
main.menu.help.about.desc = Copyright details about OpenRocket
|
|
|
|
main.menu.debug = Debug
|
|
main.menu.debug.whatisthismenu = What is this menu?
|
|
main.menu.debug.createtestrocket = Create test rocket
|
|
|
|
! database
|
|
! Translate here all material database
|
|
!
|
|
|
|
! Material database
|
|
! BULK_MATERIAL
|
|
Databases.materials.Acrylic = Acrylic
|
|
Databases.materials.Balsa = Balsa
|
|
Databases.materials.Basswood = Basswood
|
|
Databases.materials.Birch = Birch
|
|
Databases.materials.Cardboard = Cardboard
|
|
Databases.materials.Carbonfiber = Carbon fiber
|
|
Databases.materials.Cork = Cork
|
|
Databases.materials.DepronXPS = Depron (XPS)
|
|
Databases.materials.Fiberglass = Fiberglass
|
|
Databases.materials.Kraftphenolic = Kraft phenolic
|
|
Databases.materials.Maple = Maple
|
|
Databases.materials.Paperoffice = Paper (office)
|
|
Databases.materials.Pine = Pine
|
|
Databases.materials.Plywoodbirch = Plywood (birch)
|
|
Databases.materials.PolycarbonateLexan = Polycarbonate (Lexan)
|
|
Databases.materials.Polystyrene = Polystyrene
|
|
Databases.materials.PVC = PVC
|
|
Databases.materials.Spruce = Spruce
|
|
Databases.materials.StyrofoamgenericEPS = Styrofoam (generic EPS)
|
|
Databases.materials.StyrofoamBluefoamXPS = Styrofoam \"Blue foam\" (XPS)
|
|
Databases.materials.Quantumtubing = Quantum tubing
|
|
Databases.materials.BlueTube = Blue tube
|
|
!SURFACE_MATERIAL
|
|
Databases.materials.Ripstopnylon = Ripstop nylon
|
|
Databases.materials.Mylar = Mylar
|
|
Databases.materials.Polyethylenethin = Polyethylene (thin)
|
|
Databases.materials.Polyethyleneheavy = Polyethylene (heavy)
|
|
Databases.materials.Silk = Silk
|
|
Databases.materials.Paperoffice = Paper (office)
|
|
Databases.materials.Cellophane = Cellophane
|
|
Databases.materials.Crepepaper = Cr\u00eape paper
|
|
! LINE_MATERIAL
|
|
Databases.materials.Threadheavy-duty = Thread (heavy-duty)
|
|
Databases.materials.Elasticcordround2mm = Elastic cord (round 2mm, 1/16 in)
|
|
Databases.materials.Elasticcordflat6mm = Elastic cord (flat 6mm, 1/4 in)
|
|
Databases.materials.Elasticcordflat12mm = Elastic cord (flat 12mm, 1/2 in)
|
|
Databases.materials.Elasticcordflat19mm = Elastic cord (flat 19mm, 3/4 in)
|
|
Databases.materials.Elasticcordflat25mm = Elastic cord (flat 25mm, 1 in)
|
|
Databases.materials.Braidednylon2mm = Braided nylon (2 mm, 1/16 in)
|
|
Databases.materials.Braidednylon3mm = Braided nylon (3 mm, 1/8 in)
|
|
Databases.materials.Tubularnylon11mm = Tubular nylon (11 mm, 7/16 in)
|
|
Databases.materials.Tubularnylon14mm = Tubular nylon (14 mm, 9/16 in)
|
|
Databases.materials.Tubularnylon25mm = Tubular nylon (25 mm, 1 in)
|
|
|
|
! ExternalComponent
|
|
ExternalComponent.Rough = Rough
|
|
ExternalComponent.Unfinished = Unfinished
|
|
ExternalComponent.Regularpaint = Regular paint
|
|
ExternalComponent.Smoothpaint = Smooth paint
|
|
ExternalComponent.Polished = Polished
|
|
|
|
! LineStyle
|
|
LineStyle.Solid = Solid
|
|
LineStyle.Dashed = Dashed
|
|
LineStyle.Dotted = Dotted
|
|
LineStyle.Dash-dotted = Dash-dotted
|
|
LineStyle.Defaultstyle = Default style
|
|
|
|
! Shape
|
|
Shape.Conical = Conical
|
|
Shape.Conical.desc1 = A conical nose cone has a profile of a triangle.
|
|
Shape.Conical.desc2 = A conical transition has straight sides.
|
|
Shape.Ogive = Ogive
|
|
Shape.Ogive.desc1 = An ogive nose cone has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube, values less than 1 produce <b>secant ogives</b>.
|
|
Shape.Ogive.desc2 = An ogive transition has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube at the aft end, values less than 1 produce <b>secant ogives</b>.
|
|
Shape.Ellipsoid = Ellipsoid
|
|
Shape.Ellipsoid.desc1 = An ellipsoidal nose cone has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>.
|
|
Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>. If the transition is not clipped, then the profile is extended at the center by the corresponding radius.
|
|
Shape.Powerseries = Power series
|
|
Shape.Powerseries.desc1 = A power series nose cone has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 this is a <b>\u00BD-power</b> or <b>parabolic</b> nose cone, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 a <b>conical</b> nose cone.
|
|
Shape.Powerseries.desc2 = A power series transition has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 the transition is <b>\u00BD-power</b> or <b>parabolic</b>, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 <b>conical</b>.
|
|
Shape.Parabolicseries = Parabolic series
|
|
Shape.Parabolicseries.desc1 = A parabolic series nose cone has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> nose cone.
|
|
Shape.Parabolicseries.desc2 = A parabolic series transition has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube at the aft end, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> transition.
|
|
Shape.Haackseries = Haack series
|
|
Shape.Haackseries.desc1 = The Haack series nose cones are designed to minimize drag. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> nose cone, which minimizes drag for fixed length and diameter, while a value of 0.333 produces an <b>LV-Haack</b> nose cone, which minimizes drag for fixed length and volume.
|
|
Shape.Haackseries.desc2 = The Haack series <i>nose cones</i> are designed to minimize drag. These transition shapes are their equivalents, but do not necessarily produce optimal drag for transitions. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> shape, while a value of 0.333 produces an <b>LV-Haack</b> shape.
|
|
|
|
|
|
! RocketComponent
|
|
RocketComponent.Position.TOP = Top of the parent component
|
|
RocketComponent.Position.MIDDLE = Middle of the parent component
|
|
RocketComponent.Position.BOTTOM = Bottom of the parent component
|
|
RocketComponent.Position.AFTER = After the parent component
|
|
RocketComponent.Position.ABSOLUTE = Tip of the nose cone
|
|
|
|
! LaunchLug
|
|
LaunchLug.Launchlug = Launch lug
|
|
! NoseCone
|
|
NoseCone.NoseCone = Nose cone
|
|
! Transition
|
|
Transition.Transition = Transition
|
|
!Stage
|
|
Stage.Stage = Stage
|
|
! BodyTube
|
|
BodyTube.BodyTube = Body tube
|
|
! TubeCoupler
|
|
TubeCoupler.TubeCoupler = Tube coupler
|
|
!InnerTube
|
|
InnerTube.InnerTube = Inner Tube
|
|
! TrapezoidFinSet
|
|
TrapezoidFinSet.TrapezoidFinSet = Trapezoidal fin set
|
|
! FreeformFinSet
|
|
FreeformFinSet.FreeformFinSet = Freeform fin set
|
|
!MassComponent
|
|
MassComponent.MassComponent = Mass component
|
|
! Parachute
|
|
Parachute.Parachute = Parachute
|
|
! ShockCord
|
|
ShockCord.ShockCord = Shock cord
|
|
! Bulkhead
|
|
Bulkhead.Bulkhead = Bulkhead
|
|
|
|
!Rocket
|
|
Rocket.motorCount.Nomotor = [No motors]
|
|
Rocket.compname.Rocket = Rocket
|
|
|
|
!MotorMount
|
|
MotorMount.IgnitionEvent.AUTOMATIC = Automatic (launch or ejection charge)
|
|
MotorMount.IgnitionEvent.LAUNCH = Launch
|
|
MotorMount.IgnitionEvent.EJECTION_CHARGE = First ejection charge of previous stage
|
|
MotorMount.IgnitionEvent.BURNOUT = First burnout of previous stage
|
|
MotorMount.IgnitionEvent.NEVER = Never
|
|
|
|
!ComponentIcons
|
|
ComponentIcons.Nosecone = Nose cone
|
|
ComponentIcons.Bodytube = Body tube
|
|
ComponentIcons.Transition = Transition
|
|
ComponentIcons.Trapezoidalfinset = Trapezoidal fin set
|
|
ComponentIcons.Ellipticalfinset = Elliptical fin set
|
|
ComponentIcons.Freeformfinset = Freeform fin set
|
|
ComponentIcons.Launchlug = Launch lug
|
|
ComponentIcons.Innertube = Inner tube
|
|
ComponentIcons.Tubecoupler = Tube coupler
|
|
ComponentIcons.Centeringring = Centering ring
|
|
ComponentIcons.Bulkhead = Bulk head
|
|
ComponentIcons.Engineblock = Engine block
|
|
ComponentIcons.Parachute = Parachute
|
|
ComponentIcons.Streamer = Streamer
|
|
ComponentIcons.Shockcord = Shock cord
|
|
ComponentIcons.Masscomponent = Mass component
|
|
ComponentIcons.disabled = (disabled)
|
|
|
|
! StageAction
|
|
StageAction.Stage = Stage
|
|
|
|
! RecoveryDevice
|
|
RecoveryDevice.DeployEvent.LAUNCH = Launch (plus NN seconds)
|
|
RecoveryDevice.DeployEvent.EJECTION = First ejection charge of this stage
|
|
RecoveryDevice.DeployEvent.APOGEE = Apogee
|
|
RecoveryDevice.DeployEvent.ALTITUDE = Specific altitude during descent
|
|
RecoveryDevice.DeployEvent.NEVER = Never
|
|
|
|
! FlightEvent
|
|
FlightEvent.Type.LAUNCH = Launch
|
|
FlightEvent.Type.IGNITION = Motor ignition
|
|
FlightEvent.Type.LIFTOFF = Lift-off
|
|
FlightEvent.Type.LAUNCHROD = Launch rod clearance
|
|
FlightEvent.Type.BURNOUT = Motor burnout
|
|
FlightEvent.Type.EJECTION_CHARGE = Ejection charge
|
|
FlightEvent.Type.STAGE_SEPARATION = Stage separation
|
|
FlightEvent.Type.APOGEE = Apogee
|
|
FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Recovery device deployment
|
|
FlightEvent.Type.GROUND_HIT = Ground hit
|
|
FlightEvent.Type.SIMULATION_END = Simulation end
|
|
FlightEvent.Type.ALTITUDE = Altitude change
|
|
|
|
! ThrustCurveMotorColumns
|
|
TCurveMotorCol.MANUFACTURER = Manufacturer
|
|
TCurveMotorCol.DESIGNATION = Designation
|
|
TCurveMotorCol.TYPE = Type
|
|
TCurveMotorCol.DIAMETER = Diameter
|
|
TCurveMotorCol.LENGTH = Length
|
|
|
|
! RocketInfo
|
|
RocketInfo.lengthLine.Length = Length
|
|
RocketInfo.lengthLine.maxdiameter = , max. diameter
|
|
RocketInfo.massText1 = Mass with motors
|
|
RocketInfo.massText2 = Mass with no motors
|
|
RocketInfo.at = at M=
|
|
RocketInfo.cgText = CG:
|
|
RocketInfo.cpText = CP:
|
|
RocketInfo.stabText = Stability:
|
|
RocketInfo.Warning = Warning:
|
|
RocketInfo.Calculating = Calculating...
|
|
RocketInfo.Apogee = Apogee:
|
|
RocketInfo.Maxvelocity = Max. velocity:
|
|
RocketInfo.Maxacceleration = Max. acceleration:
|
|
RocketInfo.apogeeValue = N/A
|
|
RocketInfo.Mach = (Mach
|
|
RocketInfo.velocityValue = N/A
|
|
RocketInfo.accelerationValue = N/A
|
|
|
|
! FinSet
|
|
FinSet.CrossSection.SQUARE = Square
|
|
FinSet.CrossSection.ROUNDED = Rounded
|
|
FinSet.CrossSection.AIRFOIL = Airfoil
|
|
FinSet.TabRelativePosition.FRONT = Root chord leading edge
|
|
FinSet.TabRelativePosition.CENTER = Root chord midpoint
|
|
FinSet.TabRelativePosition.END = Root chord trailing edge
|
|
|
|
! FlightDataType
|
|
FlightDataType.TYPE_TIME = Time
|
|
FlightDataType.TYPE_ALTITUDE = Altitude
|
|
FlightDataType.TYPE_VELOCITY_Z = Vertical velocity
|
|
FlightDataType.TYPE_ACCELERATION_Z = Vertical acceleration
|
|
FlightDataType.TYPE_VELOCITY_TOTAL = Total velocity
|
|
FlightDataType.TYPE_ACCELERATION_TOTAL = Total acceleration
|
|
FlightDataType.TYPE_POSITION_X = Position upwind
|
|
FlightDataType.TYPE_POSITION_Y = Position parallel to wind
|
|
FlightDataType.TYPE_POSITION_XY = Lateral distance
|
|
FlightDataType.TYPE_POSITION_DIRECTION = Lateral direction
|
|
FlightDataType.TYPE_VELOCITY_XY = Lateral velocity
|
|
FlightDataType.TYPE_ACCELERATION_XY = Lateral acceleration
|
|
FlightDataType.TYPE_AOA = Angle of attack
|
|
FlightDataType.TYPE_ROLL_RATE = Roll rate
|
|
FlightDataType.TYPE_PITCH_RATE = Pitch rate
|
|
FlightDataType.TYPE_YAW_RATE = Yaw rate
|
|
FlightDataType.TYPE_MASS = Mass
|
|
FlightDataType.TYPE_LONGITUDINAL_INERTIA = Longitudinal moment of inertia
|
|
FlightDataType.TYPE_ROTATIONAL_INERTIA = Rotational moment of inertia
|
|
FlightDataType.TYPE_CP_LOCATION = CP location
|
|
FlightDataType.TYPE_CG_LOCATION = CG location
|
|
FlightDataType.TYPE_STABILITY = Stability margin calibers
|
|
FlightDataType.TYPE_MACH_NUMBER = Mach number
|
|
FlightDataType.TYPE_REYNOLDS_NUMBER = Reynolds number
|
|
FlightDataType.TYPE_THRUST_FORCE = Thrust
|
|
FlightDataType.TYPE_DRAG_FORCE = Drag force
|
|
FlightDataType.TYPE_DRAG_COEFF = Drag coefficient
|
|
FlightDataType.TYPE_AXIAL_DRAG_COEFF = Axial drag coefficient
|
|
FlightDataType.TYPE_FRICTION_DRAG_COEFF = Friction drag coefficient
|
|
FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Pressure drag coefficient
|
|
FlightDataType.TYPE_BASE_DRAG_COEFF = Base drag coefficient
|
|
FlightDataType.TYPE_NORMAL_FORCE_COEFF = Normal force coefficient
|
|
FlightDataType.TYPE_PITCH_MOMENT_COEFF = Pitch moment coefficient
|
|
FlightDataType.TYPE_YAW_MOMENT_COEFF = Yaw moment coefficient
|
|
FlightDataType.TYPE_SIDE_FORCE_COEFF = Side force coefficient
|
|
FlightDataType.TYPE_ROLL_MOMENT_COEFF = Roll moment coefficient
|
|
FlightDataType.TYPE_ROLL_FORCING_COEFF = Roll forcing coefficient
|
|
FlightDataType.TYPE_ROLL_DAMPING_COEFF = Roll damping coefficient
|
|
FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Pitch damping coefficient
|
|
FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Yaw damping coefficient
|
|
FlightDataType.TYPE_REFERENCE_LENGTH = Reference lenght
|
|
FlightDataType.TYPE_REFERENCE_AREA = Reference area
|
|
FlightDataType.TYPE_ORIENTATION_THETA = Vertical orientation (zenith)
|
|
FlightDataType.TYPE_ORIENTATION_PHI = Lateral orientation (azimuth)
|
|
FlightDataType.TYPE_WIND_VELOCITY = Wind velocity
|
|
FlightDataType.TYPE_AIR_TEMPERATURE = Air temperature
|
|
FlightDataType.TYPE_AIR_PRESSURE = Air pressure
|
|
FlightDataType.TYPE_SPEED_OF_SOUND = Speed of sound
|
|
FlightDataType.TYPE_TIME_STEP = Simulation time step
|
|
FlightDataType.TYPE_COMPUTATION_TIME = Computation time
|
|
FlightDataType.TYPE_LATITUDE = Latitude
|
|
FlightDataType.TYPE_LONGITUDE = Longitude
|
|
FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration
|
|
|
|
! PlotConfiguration
|
|
PlotConfiguration.Verticalmotion = Vertical motion vs. time
|
|
PlotConfiguration.Totalmotion = Total motion vs. time
|
|
PlotConfiguration.Flightside = Flight side profile
|
|
PlotConfiguration.Stability = Stability vs. time
|
|
PlotConfiguration.Dragcoef = Drag coefficients vs. Mach number
|
|
PlotConfiguration.Rollcharacteristics = Roll characteristics
|
|
PlotConfiguration.Angleofattack = Angle of attack and orientation vs. time
|
|
PlotConfiguration.Simulationtime = Simulation time step and computation time
|
|
|
|
! Warning
|
|
Warning.LargeAOA.str1 = Large angle of attack encountered.
|
|
Warning.LargeAOA.str2 = Large angle of attack encountered (
|
|
Warning.DISCONTINUITY = Discontinuity in rocket body diameter.
|
|
Warning.THICK_FIN = Thick fins may not be modeled accurately.
|
|
Warning.JAGGED_EDGED_FIN = Jagged-edged fin predictions may be inaccurate.
|
|
Warning.LISTENERS_AFFECTED = Listeners modified the flight simulation
|
|
Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Recovery device opened while motor still burning.
|
|
Warning.FILE_INVALID_PARAMETER = Invalid parameter encountered, ignoring.
|
|
|
|
|
|
! Scale dialog
|
|
ScaleDialog.lbl.scaleRocket = Entire rocket
|
|
ScaleDialog.lbl.scaleSubselection = Selection and all subcomponents
|
|
ScaleDialog.lbl.scaleSelection = Only selected component
|
|
ScaleDialog.title = Scale design
|
|
ScaleDialog.lbl.scale = Scale:
|
|
ScaleDialog.lbl.scale.ttip = Select whether to scale the entire design or only the selected component
|
|
ScaleDialog.lbl.scaling = Scaling to apply:
|
|
ScaleDialog.lbl.scaling.ttip = Resulting size, values above 100% grow and values below 100% shrink the design.
|
|
! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"
|
|
ScaleDialog.lbl.scaleFrom = Scale from
|
|
ScaleDialog.lbl.scaleTo = to
|
|
ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and resulting length.
|
|
ScaleDialog.checkbox.scaleMass = Update explicit mass values
|
|
ScaleDialog.checkbox.scaleMass.ttip = Scale mass component and override mass values by the cube of the scaling factor
|
|
ScaleDialog.button.scale = Scale
|
|
ScaleDialog.undo.scaleRocket = Scale rocket
|
|
ScaleDialog.undo.scaleComponent = Scale component
|
|
ScaleDialog.undo.scaleComponents = Scale components
|
|
|
|
!icons
|
|
Icons.Undo = Undo
|
|
Icons.Redo = Redo
|
|
|
|
OpenRocketPrintable.Partsdetail = Parts detail
|
|
OpenRocketPrintable.Fintemplates = Fin templates
|
|
OpenRocketPrintable.Transitiontemplates = Transition templates
|
|
OpenRocketPrintable.Noseconetemplates = Nose Cone templates
|
|
OpenRocketPrintable.Finmarkingguide = Fin marking guide
|
|
OpenRocketPrintable.DesignReport = Design Report
|
|
|
|
OpenRocketDocument.Redo = Redo
|
|
OpenRocketDocument.Undo = Undo
|
|
|
|
!EllipticalFinSet
|
|
EllipticalFinSet.Ellipticalfinset = Elliptical fin set
|
|
|
|
! Optimization
|
|
|
|
! Modifiers
|
|
|
|
optimization.modifier.nosecone.length = Length
|
|
optimization.modifier.nosecone.length.desc = Optimize the nose cone length.
|
|
optimization.modifier.nosecone.diameter = Diameter
|
|
optimization.modifier.nosecone.diameter.desc = Optimize the nose cone base diameter.
|
|
optimization.modifier.nosecone.thickness = Thickness
|
|
optimization.modifier.nosecone.thickness.desc = Optimize the nose cone wall thickness.
|
|
optimization.modifier.nosecone.shapeparameter = Shape parameter
|
|
optimization.modifier.nosecone.shapeparameter.desc = Optimize the nose cone shape parameter.
|
|
|
|
optimization.modifier.transition.length = Length
|
|
optimization.modifier.transition.length.desc = Optimize the transition length.
|
|
optimization.modifier.transition.forediameter = Fore diameter
|
|
optimization.modifier.transition.forediameter.desc = Optimize the transition fore diameter.
|
|
optimization.modifier.transition.aftdiameter = Aft diameter
|
|
optimization.modifier.transition.aftdiameter.desc = Optimize the transition aft diameter.
|
|
optimization.modifier.transition.thickness = Thickness
|
|
optimization.modifier.transition.thickness.desc = Optimize the transition wall thickness.
|
|
optimization.modifier.transition.shapeparameter = Shape parameter
|
|
optimization.modifier.transition.shapeparameter.desc = Optimize the transition shape parameter.
|
|
|
|
optimization.modifier.bodytube.length = Length
|
|
optimization.modifier.bodytube.length.desc = Optimize the body tube length.
|
|
optimization.modifier.bodytube.outerDiameter = Outer diameter
|
|
optimization.modifier.bodytube.outerDiameter.desc = Optimize the body tube outer diameter while maintaining the wall thickness.
|
|
optimization.modifier.bodytube.thickness = Thickness
|
|
optimization.modifier.bodytube.thickness.desc = Optimize the body tube wall thickness.
|
|
|
|
optimization.modifier.trapezoidfinset.rootChord = Root chord
|
|
optimization.modifier.trapezoidfinset.rootChord.desc = Optimize the root chord length of the fin set (length of fin at the rocket body).
|
|
optimization.modifier.trapezoidfinset.tipChord = Tip chord
|
|
optimization.modifier.trapezoidfinset.tipChord.desc = Optimize the tip chord length of the fin set (length of fin at outer edge).
|
|
optimization.modifier.trapezoidfinset.sweep = Sweep
|
|
optimization.modifier.trapezoidfinset.sweep.desc = Optimize the sweep of the fin set (distance that the leading edge sweeps backwards).
|
|
optimization.modifier.trapezoidfinset.height = Height
|
|
optimization.modifier.trapezoidfinset.height.desc = Optimize the height (semi-span) of the fin set.
|
|
|
|
optimization.modifier.ellipticalfinset.length = Root chord
|
|
optimization.modifier.ellipticalfinset.length.desc = Optimize the root chord length of the fin set.
|
|
optimization.modifier.ellipticalfinset.height = Height
|
|
optimization.modifier.ellipticalfinset.height.desc = Optimize the height (semi-span) of the fin set.
|
|
|
|
optimization.modifier.finset.cant = Cant angle
|
|
optimization.modifier.finset.cant.desc = Optimize the cant angle of the fin set.
|
|
optimization.modifier.finset.position = Position
|
|
optimization.modifier.finset.position.desc = Optimize the fin set position along the rocket body.
|
|
|
|
optimization.modifier.launchlug.length = Length
|
|
optimization.modifier.launchlug.length.desc = Optimize the launch lug length.
|
|
optimization.modifier.launchlug.outerDiameter = Outer diameter
|
|
optimization.modifier.launchlug.outerDiameter.desc = Optimize the outer diameter of the launch lug.
|
|
optimization.modifier.launchlug.thickness = Thickness
|
|
optimization.modifier.launchlug.thickness.desc = Optimize the launch lug thickness while keeping the outer diameter constant.
|
|
optimization.modifier.launchlug.position = Position
|
|
optimization.modifier.launchlug.position.desc = Optimize the launch lug position along the rocket body.
|
|
|
|
|
|
optimization.modifier.internalcomponent.position = Position
|
|
optimization.modifier.internalcomponent.position.desc = Optimize the position of the component relative to the parent component.
|
|
|
|
optimization.modifier.masscomponent.mass = Mass
|
|
optimization.modifier.masscomponent.mass.desc = Optimize the mass of the mass component.
|
|
|
|
optimization.modifier.parachute.diameter = Diameter
|
|
optimization.modifier.parachute.diameter.desc = Optimize the parachute canopy diameter.
|
|
optimization.modifier.parachute.coefficient = Drag coefficient
|
|
optimization.modifier.parachute.coefficient.desc = Optimize the drag coefficient of the parachute. Typical parachutes have a drag coefficient of about 0.8.
|
|
|
|
optimization.modifier.streamer.length = Length
|
|
optimization.modifier.streamer.length.desc = Optimize the length of the streamer.
|
|
optimization.modifier.streamer.width = Width
|
|
optimization.modifier.streamer.width.desc = Optimize the width of the streamer.
|
|
optimization.modifier.streamer.aspectRatio = Aspect ratio
|
|
optimization.modifier.streamer.aspectRatio.desc = Optimize the aspect ratio of the streamer (length/width). You should NOT select streamer length or width at the same time with the aspect ratio.
|
|
optimization.modifier.streamer.coefficient = Drag coefficient
|
|
optimization.modifier.streamer.coefficient.desc = Optimize the drag coefficient of the streamer.
|
|
|
|
optimization.modifier.recoverydevice.deployDelay = Deployment delay
|
|
optimization.modifier.recoverydevice.deployDelay.desc = Optimize the deployment delay of the recovery device.
|
|
optimization.modifier.recoverydevice.deployAltitude = Deployment altitude
|
|
optimization.modifier.recoverydevice.deployAltitude.desc = Optimize the deployment altitude of the recovery device.
|
|
|
|
optimization.modifier.rocketcomponent.overrideMass = Override mass
|
|
optimization.modifier.rocketcomponent.overrideMass.desc = Optimize the overridden mass of the component.
|
|
optimization.modifier.rocketcomponent.overrideCG = Override CG
|
|
optimization.modifier.rocketcomponent.overrideCG.desc = Optimize the overridden center of gravity of the component.
|
|
|
|
optimization.modifier.motormount.overhang = Motor overhang
|
|
optimization.modifier.motormount.overhang.desc = Optimize the motor overhang.
|
|
optimization.modifier.motormount.delay = Motor ignition delay
|
|
optimization.modifier.motormount.delay.desc = Optimize the motor ignition delay.
|
|
|
|
|
|
|
|
|
|
! General rocket design optimization dialog
|
|
|
|
GeneralOptimizationDialog.title = Rocket optimization
|
|
GeneralOptimizationDialog.goal.maximize = Maximize value
|
|
GeneralOptimizationDialog.goal.minimize = Minimize value
|
|
GeneralOptimizationDialog.goal.seek = Seek value of
|
|
GeneralOptimizationDialog.btn.start = Start optimization
|
|
GeneralOptimizationDialog.btn.stop = Stop optimization
|
|
GeneralOptimizationDialog.lbl.paramsToOptimize = Parameters to optimize:
|
|
GeneralOptimizationDialog.btn.add = Add
|
|
GeneralOptimizationDialog.btn.add.ttip = Add the selected parameter to the optimization
|
|
GeneralOptimizationDialog.btn.remove = Remove
|
|
GeneralOptimizationDialog.btn.remove.ttip = Remove the selected parameter from the optimization
|
|
GeneralOptimizationDialog.btn.removeAll = Remove all
|
|
GeneralOptimizationDialog.btn.removeAll.ttip = Remove all parameters from the optimization
|
|
GeneralOptimizationDialog.lbl.availableParams = Available parameters:
|
|
GeneralOptimizationDialog.lbl.optimizationOpts = Optimization options
|
|
GeneralOptimizationDialog.lbl.optimizeSim = Optimize simulation:
|
|
GeneralOptimizationDialog.lbl.optimizeSim.ttip = Select which simulation to optimize
|
|
GeneralOptimizationDialog.lbl.optimizeValue = Optimized value:
|
|
GeneralOptimizationDialog.lbl.optimizeValue.ttip = Select what value is to be optimized
|
|
GeneralOptimizationDialog.lbl.optimizeGoal = Optimization goal:
|
|
GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Select the goal of the optimization
|
|
GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Custom value to seek
|
|
GeneralOptimizationDialog.lbl.requireStability = Required stability
|
|
GeneralOptimizationDialog.lbl.requireMinStability = Minimum stability:
|
|
GeneralOptimizationDialog.lbl.requireMinStability.ttip = Require a minimum static stability margin for the design
|
|
GeneralOptimizationDialog.lbl.requireMaxStability = Maximum stability:
|
|
GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Require a maximum static stability margin for the design
|
|
GeneralOptimizationDialog.status.bestValue = Best value:
|
|
GeneralOptimizationDialog.status.bestValue.ttip = Best optimization value found so far.
|
|
GeneralOptimizationDialog.status.stepCount = Step count:
|
|
GeneralOptimizationDialog.status.stepCount.ttip = Number of optimization steps that have been performed.
|
|
GeneralOptimizationDialog.status.evalCount = Evaluations:
|
|
GeneralOptimizationDialog.status.evalCount.ttip = Total number of function evaluations (simulations) that have been performed.
|
|
GeneralOptimizationDialog.status.stepSize = Step size:
|
|
GeneralOptimizationDialog.status.stepSize.ttip = Current optimization step size (relative to the optimization parameter ranges)
|
|
GeneralOptimizationDialog.btn.plotPath = Plot path
|
|
GeneralOptimizationDialog.btn.plotPath.ttip = Plot the optimization path (one and two dimensional optimization only)
|
|
GeneralOptimizationDialog.btn.save = Save path
|
|
GeneralOptimizationDialog.btn.save.ttip = Save the results of the function evaluations (simulations) as a CSV file.
|
|
GeneralOptimizationDialog.btn.apply = Apply optimization
|
|
GeneralOptimizationDialog.btn.apply.ttip = Apply the optimization results to the rocket design
|
|
GeneralOptimizationDialog.btn.reset = Reset
|
|
GeneralOptimizationDialog.btn.reset.ttip = Reset the rocket design to the current rocket design
|
|
GeneralOptimizationDialog.btn.close = Close
|
|
GeneralOptimizationDialog.btn.close.ttip = Close the dialog without modifying the rocket design
|
|
GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters.
|
|
GeneralOptimizationDialog.error.selectParams.title = Select optimization parameters
|
|
GeneralOptimizationDialog.error.optimizationFailure.text = The optimization failed to run:
|
|
GeneralOptimizationDialog.error.optimizationFailure.title = Optimization failed
|
|
GeneralOptimizationDialog.undoText = Apply optimization
|
|
GeneralOptimizationDialog.basicSimulationName = Basic simulation
|
|
GeneralOptimizationDialog.noSimulationName = No simulation
|
|
GeneralOptimizationDialog.table.col.parameter = Parameter
|
|
GeneralOptimizationDialog.table.col.current = Current
|
|
GeneralOptimizationDialog.table.col.min = Minimum
|
|
GeneralOptimizationDialog.table.col.max = Maximum
|
|
GeneralOptimizationDialog.export.header = Include header line
|
|
GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions.
|
|
GeneralOptimizationDialog.export.stability = Stability
|
|
|
|
|
|
! Dialog for plotting optimization results
|
|
OptimizationPlotDialog.title = Optimization results
|
|
OptimizationPlotDialog.lbl.zoomInstructions = Click and drag down+right to zoom in, up+left to zoom out
|
|
OptimizationPlotDialog.plot1d.title = Optimization result
|
|
OptimizationPlotDialog.plot1d.series = Optimization result
|
|
OptimizationPlotDialog.plot2d.title = Optimization path
|
|
OptimizationPlotDialog.plot2d.path = Optimization path
|
|
OptimizationPlotDialog.plot2d.evals = Evaluations
|
|
OptimizationPlotDialog.plot.ttip.stability = Stability:
|
|
OptimizationPlotDialog.plot.label.optimum = Optimum
|
|
|
|
! Optimization parameters
|
|
MaximumAltitudeParameter.name = Apogee altitude
|
|
MaximumVelocityParameter.name = Maximum velocity
|
|
MaximumAccelerationParameter.name = Maximum acceleration
|
|
StabilityParameter.name = Stability
|
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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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