#
# Should you need to add new logical keys here is the proposed method
#
-# className.ComponantType.componantName
+# className.ComponentType.componentName
+#
+#
+# Text tokens within braces should not be translated, e.g.
+# "The file '{filename}' exists."
+# They are pieces that are inserted dynamically.
#
-
! Set to the name of the current translation file (used for debugging purposes)
BasicFrame.tab.Rocketdesign = Rocket design
BasicFrame.tab.Flightsim = Flight simulations
BasicFrame.title.Addnewcomp = Add new component
-BasicFrame.item.Openrocketdesign = Open a rocket design
-BasicFrame.item.Openexamplerocketdesign = Open an example rocket design
-BasicFrame.item.SavecurRocketdesign = Save the current rocket design
-BasicFrame.item.SavecurRocketdesnewfile = Save the current rocket design to a new file
-BasicFrame.item.Printpart = Print parts list and fin template
-BasicFrame.item.Closedesign = Close the current rocket design
-BasicFrame.item.Quitprogram = Quit the program
-BasicFrame.menu.Rocketedt = Rocket editing
BasicFrame.dlg.lbl1 = Design '
BasicFrame.dlg.lbl2 = ' has not been saved.
BasicFrame.dlg.lbl3 = Do you want to save it?
BasicFrame.dlg.title = Design not saved
+BasicFrame.StageName.Sustainer = Sustainer
+BasicFrame.WarningDialog.txt1 = The following problems were encountered while opening
+BasicFrame.WarningDialog.txt2 = Some design features may not have been loaded correctly.
+BasicFrame.WarningDialog.title = Warnings while opening file
+
+
+! General error messages used in multiple contexts
+error.fileExists.title = File exists
+error.fileExists.desc = File '{filename}' exists. Do you want to overwrite it?
+
+error.writing.title = Error writing file
+error.writing.desc = An error occurred while writing to the file:
+
! Labels used in buttons of dialog windows
+# TODO: Rename these to "btn.xxx"
button.ok = OK
button.cancel = Cancel
button.close = Close
dlg.but.cancel = Cancel
dlg.but.close = Close
+
+! General file type names
+filetypes.pdf = PDF files
+
+
! About Dialog
-about.dlg.but.close = Close
-about.dlg.lbl.translation =
-about.dlg.lbl.transwebsite =
+AboutDialog.lbl.version = Version
+! The texts below provide additional credits for the translation maintainer
+! - In AboutDialog.lbl.translation replace "English" with the current language.
+! - AboutDialog.lbl.translator is the translator / group name (may be empty)
+! - AboutDialog.lbl.translatorWebsite is a URL to the translator / group (may be empty)
+! - AboutDialog.lbl.translatorIcon is the file name of an icon under pix/translators/ (may be empty)
+AboutDialog.lbl.translation = English translation by:
+AboutDialog.lbl.translator =
+AboutDialog.lbl.translatorWebsite =
+AboutDialog.lbl.translatorIcon =
+
+
+! Print dialog
+PrintDialog.title = Print or export
+PrintDialog.but.previewAndPrint = Preview & Print
+PrintDialog.checkbox.showByStage = Show by stage
+PrintDialog.lbl.selectElements = Select elements to include:
+printdlg.but.saveaspdf = Save as PDF
+printdlg.but.preview = Preview
+printdlg.but.settings = Settings
+PrintDialog.error.preview.title = Unable to open preview
+PrintDialog.error.preview.desc1 = Unable to open PDF preview.
+PrintDialog.error.preview.desc2 = Please use the "Save as PDF" option instead.
+
+
+!PrintSettingsDialog
+PrintSettingsDialog.title = Print settings
+PrintSettingsDialog.lbl.Templatefillcolor = Template fill color:
+PrintSettingsDialog.lbl.Templatebordercolor = Template border color:
+PrintSettingsDialog.lbl.Papersize = Paper size:
+PrintSettingsDialog.lbl.Paperorientation = Paper orientation:
+PrintSettingsDialog.but.Reset = Reset
+PrintSettingsDialog.but.Close = Close
+
! Bug Report dialog
bugreport.dlg.title = Bug report
bugreport.dlg.successmsg1 = Bug report successfully sent.
bugreport.dlg.successmsg2 = Thank you for helping make OpenRocket better!
bugreport.dlg.successmsg3 = Bug report sent
+bugreport.dlg.connectedInternet = <html>If connected to the Internet, you can simply click <em>Send bug report</em>.
+bugreport.dlg.otherwise = Otherwise, send the text below to the address:
+bugreport.lbl.Theinformation = The information above may be included in a public bug report. Make sure it does not contain any sensitive information you do not want to be made public.
+bugreport.dlg.failedmsg1 = OpenRocket was unable to send the bug report:
+bugreport.dlg.failedmsg2 = Please send the report manually to
+bugreport.dlg.failedmsg3 = Error sending report
+bugreport.reportDialog.txt = <html><b>You can report a bug in OpenRocket by filling in and submitting the form below.</b><br>You can also report bugs and include attachments on the project web site.
+bugreport.reportDialog.txt2 = <html><b>Please include a short description about what you were doing when the exception occurred.</b>
+bugreport.dlg.provideDescription = Please provide a description of the bug first.
+bugreport.dlg.provideDescription.title = Bug description missing
+
! Debug log dialog
debuglogdlg.but.clear = Clear
debuglogdlg.lbl.Loglinenbr = Log line number:
debuglogdlg.lbl.Time = Time:
debuglogdlg.lbl.Level = Level:
+debuglogdlg.lbl.Location = Location:
+debuglogdlg.lbl.Logmessage = Log message:
+debuglogdlg.lbl.Stacktrace = Stack trace:
! Edit Motor configuration dialog
! Example design dialog
exdesigndlg.but.open = Open
+exdesigndlg.lbl.Selectexample = Select example designs to open:
+exdesigndlg.lbl.Openexampledesign = Open example design
+exdesigndlg.lbl.Exampledesignsnotfound = Example designs could not be found.
+exdesigndlg.lbl.Examplesnotfound = Examples not found
-! Print panel dialog
-printdlg.but.saveaspdf = Save as PDF
-printdlg.but.preview = Preview
-printdlg.but.settings = Settings
! Material edit panel
matedtpan.but.new = New
matedtpan.but.ttip.revertall = Delete all user-defined materials
matedtpan.title.Deletealluser-defined = Delete all user-defined materials?
matedtpan.title.Revertall = Revert all?
-matedtpan.lbl.edtmaterials = <html><i>Editing materials will not affect existing rocket designs.</i>
+matedtpan.lbl.edtmaterials = Editing materials will not affect existing rocket designs.
!MaterialModel
MaterialModel.title.Material = Material
pref.dlg.lbl.Motordimensions = Motor dimensions:
pref.dlg.lbl.Surfacedensity = Surface density:
pref.dlg.lbl.Distance = Distance:
-pref.dlg.lbl.Bulkdensity = Bulk density::
+pref.dlg.lbl.Bulkdensity = Bulk density:
pref.dlg.lbl.Velocity = Velocity:
pref.dlg.lbl.Surfaceroughness = Surface roughness:
pref.dlg.lbl.Acceleration = Acceleration:
pref.dlg.lbl.Momentofinertia = Moment of inertia:
pref.dlg.lbl.Pressure = Pressure:
pref.dlg.lbl.Stability = Stability:
+pref.dlg.lbl.FlightTime = Flight time:
pref.dlg.lbl.effect1 = The effects will take place the next time you open a window.
pref.dlg.lbl.Checkingupdates = Checking for updates...
pref.dlg.lbl.msg1 = An error occurred while communicating with the server.
pref.dlg.lbl.msg2 = Unable to retrieve update information
pref.dlg.lbl.msg3 = You are running the latest version of OpenRocket.
pref.dlg.lbl.msg4 = No updates available
+pref.dlg.PrefChoiseSelector1 = Always ask
+pref.dlg.PrefChoiseSelector2 = Insert in middle
+pref.dlg.PrefChoiseSelector3 = Add to end
+pref.dlg.PrefBooleanSelector1 = Delete
+pref.dlg.PrefBooleanSelector2 = Confirm
+pref.dlg.Add = Add
+pref.dlg.DescriptionArea.Adddirectories = Add directories, RASP motor files (*.eng), RockSim engine files (*.rse) or ZIP archives separated by a semicolon (;) to load external thrust curves. Changes will take effect the next time you start OpenRocket.
+
+PreferencesDialog.lbl.language = Interface language:
+PreferencesDialog.languages.default = System default
+PreferencesDialog.lbl.languageEffect = The language will change the next time you start OpenRocket.
! Simulation edit dialog
simedtdlg.but.runsimulation = Run simulation
simedtdlg.lbl.runsimfirst = Please run the simulation first.
simedtdlg.chart.Simflight = Simulated flight
simedtdlg.dlg.Simres = Simulation results
+simedtdlg.IntensityDesc.None = None
+simedtdlg.IntensityDesc.Verylow = Very low
+simedtdlg.IntensityDesc.Low = Low
+simedtdlg.IntensityDesc.Medium = Medium
+simedtdlg.IntensityDesc.High = High
+simedtdlg.IntensityDesc.Veryhigh = Very high
+simedtdlg.IntensityDesc.Extreme = Extreme
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
simplotpanel.Desc = The data will be plotted in time order even if the X axis type is not time.
simplotpanel.OptionPane.lbl1 = A maximum of 15 plots is allowed.
simplotpanel.OptionPane.lbl2 = Cannot add plot
-
+simplotpanel.AUTO_NAME = Auto
+simplotpanel.LEFT_NAME = Left
+simplotpanel.RIGHT_NAME = Right
+simplotpanel.CUSTOM = Custom
! Component add buttons
compaddbuttons.Bodycompandfinsets = Body components and fin sets
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
ringcompcfg.PositionValue = PositionValue
ringcompcfg.Radialdistance = Radial distance:
ringcompcfg.Distancefrom = Distance from the rocket centerline
-ringcompcfg.Radialdirection = Radial direction
+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:
RocketCfg.lbl.Material = Material:
! ShockCordConfig
-ShockCordCfg.lbl.Shockcordlength = Shock cord length
+ShockCordCfg.lbl.Shockcordlength = Shock cord length:
! RocketComponentConfig
RocketCompCfg.lbl.Componentname = Component name:
!ComponentConfigDialog
ComponentCfgDlg.configuration = configuration
+ComponentCfgDlg.configuration1 =
ComponentCfgDlg.Modify = Modify
!EllipticalFinSetConfig
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
LaunchLugCfg.tab.Generalprop = General properties
! MassComponentConfig
-MassComponentCfg.lbl.Mass = Mass
-MassComponentCfg.lbl.Length = Length
-MassComponentCfg.lbl.Diameter = Diameter
+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
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
StreamerCfg.lbl.Radialdistance = Radial distance:
StreamerCfg.lbl.Radialdirection = Radial direction:
StreamerCfg.but.Reset = Reset
+StreamerCfg.lbl.plusdelay = plus
! ThicknessRingComponentConfig
ThicknessRingCompCfg.tab.Outerdiam = Outer diameter:
! ThrustCurveMotorSelectionPanel
TCMotorSelPan.lbl.Selrocketmotor = Select rocket motor:
TCMotorSelPan.checkbox.hideSimilar = Hide very similar thrust curves
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Show all motors
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Show motors with diameter less than that of the motor mount
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Show motors with diameter equal to that of the motor mount
+TCMotorSelPan.lbl.Motormountdia = Motor mount diameter:
+TCMotorSelPan.lbl.Search = Search:
+TCMotorSelPan.lbl.Selectthrustcurve = Select thrust curve:
+TCMotorSelPan.lbl.Ejectionchargedelay = Ejection charge delay:
+TCMotorSelPan.equalsIgnoreCase.None = None
+TCMotorSelPan.lbl.NumberofsecondsorNone = (Number of seconds or \"None\")
+TCMotorSelPan.lbl.Totalimpulse = Total impulse:
+TCMotorSelPan.lbl.Avgthrust = Avg. thrust:
+TCMotorSelPan.lbl.Maxthrust = Max. thrust:
+TCMotorSelPan.lbl.Burntime = Burn time:
+TCMotorSelPan.lbl.Launchmass = Launch mass:
+TCMotorSelPan.lbl.Emptymass = Empty mass:
+TCMotorSelPan.lbl.Datapoints = Data points:
+TCMotorSelPan.lbl.Digest = Digest:
+TCMotorSelPan.title.Thrustcurve = Thrust curve:
+TCMotorSelPan.title.Thrust = Thrust
+TCMotorSelPan.delayBox.None = None
+
! PlotDialog
PlotDialog.title.Flightdataplot = Flight data plot
PlotDialog.Chart.Simulatedflight = Simulated flight
PlotDialog.CheckBox.Showdatapoints = Show data points
-PlotDialog.lbl.Chart = Click+drag down+right to zoom in, up+left to zoom out
+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...
-main.menu.file.print = Print...
+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.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.Birch = Birch
+Databases.materials.Cardboard = Cardboard
+Databases.materials.Carbonfiber = Carbon fiber
+Databases.materials.Cork = Cork
+Databases.materials.DepronXPS = Depron (XPS)
+Databases.materials.Fiberglass = Fiberglass
+Databases.materials.Kraftphenolic = Kraft phenolic
+Databases.materials.Maple = Maple
+Databases.materials.Paperoffice = Paper (office)
+Databases.materials.Pine = Pine
+Databases.materials.Plywoodbirch = Plywood (birch)
+Databases.materials.PolycarbonateLexan = Polycarbonate (Lexan)
+Databases.materials.Polystyrene = Polystyrene
+Databases.materials.PVC = PVC
+Databases.materials.Spruce = Spruce
+Databases.materials.StyrofoamgenericEPS = Styrofoam (generic EPS)
+Databases.materials.StyrofoamBluefoamXPS = Styrofoam \"Blue foam\" (XPS)
+Databases.materials.Quantumtubing = Quantum tubing
+!SURFACE_MATERIAL
+Databases.materials.Ripstopnylon = Ripstop nylon
+Databases.materials.Mylar = Mylar
+Databases.materials.Polyethylenethin = Polyethylene (thin)
+Databases.materials.Polyethyleneheavy = Polyethylene (heavy)
+Databases.materials.Silk = Silk
+Databases.materials.Paperoffice = Paper (office)
+Databases.materials.Cellophane = Cellophane
+Databases.materials.Crepepaper = Cr\u00eape paper
+! LINE_MATERIAL
+Databases.materials.Threadheavy-duty = Thread (heavy-duty)
+Databases.materials.Elasticcordround2mm = Elastic cord (round 2mm, 1/16 in)
+Databases.materials.Elasticcordflat6mm = Elastic cord (flat 6mm, 1/4 in)
+Databases.materials.Elasticcordflat12mm = Elastic cord (flat 12mm, 1/2 in)
+Databases.materials.Elasticcordflat19mm = Elastic cord (flat 19mm, 3/4 in)
+Databases.materials.Elasticcordflat25mm = Elastic cord (flat 25mm, 1 in)
+Databases.materials.Braidednylon2mm = Braided nylon (2 mm, 1/16 in)
+Databases.materials.Braidednylon3mm = Braided nylon (3 mm, 1/8 in)
+Databases.materials.Tubularnylon11mm = Tubular nylon (11 mm, 7/16 in)
+Databases.materials.Tubularnylon14mm = Tubular nylon (14 mm, 9/16 in)
+Databases.materials.Tubularnylon25mm = Tubular nylon (25 mm, 1 in)
+
+! ExternalComponent
+ExternalComponent.Rough = Rough
+ExternalComponent.Unfinished = Unfinished
+ExternalComponent.Regularpaint = Regular paint
+ExternalComponent.Smoothpaint = Smooth paint
+ExternalComponent.Polished = Polished
+
+! LineStyle
+LineStyle.Solid = Solid
+LineStyle.Dashed = Dashed
+LineStyle.Dotted = Dotted
+LineStyle.Dash-dotted = Dash-dotted
+LineStyle.Defaultstyle = Default style
+
+! Shape
+Shape.Conical = Conical
+Shape.Conical.desc1 = A conical nose cone has a profile of a triangle.
+Shape.Conical.desc2 = A conical transition has straight sides.
+Shape.Ogive = Ogive
+Shape.Ogive.desc1 = An ogive nose cone has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube, values less than 1 produce <b>secant ogives</b>.
+Shape.Ogive.desc2 = An ogive transition has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube at the aft end, values less than 1 produce <b>secant ogives</b>.
+Shape.Ellipsoid = Ellipsoid
+Shape.Ellipsoid.desc1 = An ellipsoidal nose cone has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>.
+Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>. If the transition is not clipped, then the profile is extended at the center by the corresponding radius.
+Shape.Powerseries = Power series
+Shape.Powerseries.desc1 = A power series nose cone has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 this is a <b>\u00BD-power</b> or <b>parabolic</b> nose cone, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 a <b>conical</b> nose cone.
+Shape.Powerseries.desc2 = A power series transition has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 the transition is <b>\u00BD-power</b> or <b>parabolic</b>, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 <b>conical</b>.
+Shape.Parabolicseries = Parabolic series
+Shape.Parabolicseries.desc1 = A parabolic series nose cone has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> nose cone.
+Shape.Parabolicseries.desc2 = A parabolic series transition has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube at the aft end, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> transition.
+Shape.Haackseries = Haack series
+Shape.Haackseries.desc1 = The Haack series nose cones are designed to minimize drag. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> nose cone, which minimizes drag for fixed length and diameter, while a value of 0.333 produces an <b>LV-Haack</b> nose cone, which minimizes drag for fixed length and volume.
+Shape.Haackseries.desc2 = The Haack series <i>nose cones</i> are designed to minimize drag. These transition shapes are their equivalents, but do not necessarily produce optimal drag for transitions. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> shape, while a value of 0.333 produces an <b>LV-Haack</b> shape.
+
+
+! RocketComponent
+RocketComponent.Position.TOP = Top of the parent component
+RocketComponent.Position.MIDDLE = Middle of the parent component
+RocketComponent.Position.BOTTOM = Bottom of the parent component
+RocketComponent.Position.AFTER = After the parent component
+RocketComponent.Position.ABSOLUTE = Tip of the nose cone
+
+! LaunchLug
+LaunchLug.Launchlug = Launch lug
+! NoseCone
+NoseCone.NoseCone = Nose cone
+! Transition
+Transition.Transition = Transition
+!Stage
+Stage.Stage = Stage
+! BodyTube
+BodyTube.BodyTube = Body tube
+! TubeCoupler
+TubeCoupler.TubeCoupler = Tube coupler
+!InnerTube
+InnerTube.InnerTube = Inner Tube
+! TrapezoidFinSet
+TrapezoidFinSet.TrapezoidFinSet = Trapezoidal fin set
+! FreeformFinSet
+FreeformFinSet.FreeformFinSet = Freeform fin set
+!MassComponent
+MassComponent.MassComponent = Mass component
+! Parachute
+Parachute.Parachute = Parachute
+! ShockCord
+ShockCord.ShockCord = Shock cord
+! Bulkhead
+Bulkhead.Bulkhead = Bulkhead
+
+!Rocket
+Rocket.motorCount.Nomotor = [No motors]
+Rocket.compname.Rocket = Rocket
+
+!MotorMount
+MotorMount.IgnitionEvent.AUTOMATIC = Automatic (launch or ejection charge)
+MotorMount.IgnitionEvent.LAUNCH = Launch
+MotorMount.IgnitionEvent.EJECTION_CHARGE = First ejection charge of previous stage
+MotorMount.IgnitionEvent.BURNOUT = First burnout of previous stage
+MotorMount.IgnitionEvent.NEVER = Never
+
+!ComponentIcons
+ComponentIcons.Nosecone = Nose cone
+ComponentIcons.Bodytube = Body tube
+ComponentIcons.Transition = Transition
+ComponentIcons.Trapezoidalfinset = Trapezoidal fin set
+ComponentIcons.Ellipticalfinset = Elliptical fin set
+ComponentIcons.Freeformfinset = Freeform fin set
+ComponentIcons.Launchlug = Launch lug
+ComponentIcons.Innertube = Inner tube
+ComponentIcons.Tubecoupler = Tube coupler
+ComponentIcons.Centeringring = Centering ring
+ComponentIcons.Bulkhead = Bulk head
+ComponentIcons.Engineblock = Engine block
+ComponentIcons.Parachute = Parachute
+ComponentIcons.Streamer = Streamer
+ComponentIcons.Shockcord = Shock cord
+ComponentIcons.Masscomponent = Mass component
+ComponentIcons.disabled = (disabled)
+
+! StageAction
+StageAction.Stage = Stage
+
+! RecoveryDevice
+RecoveryDevice.DeployEvent.LAUNCH = Launch (plus NN seconds)
+RecoveryDevice.DeployEvent.EJECTION = First ejection charge of this stage
+RecoveryDevice.DeployEvent.APOGEE = Apogee
+RecoveryDevice.DeployEvent.ALTITUDE = Specific altitude during descent
+RecoveryDevice.DeployEvent.NEVER = Never
+
+! FlightEvent
+FlightEvent.Type.LAUNCH = Launch
+FlightEvent.Type.IGNITION = Motor ignition
+FlightEvent.Type.LIFTOFF = Lift-off
+FlightEvent.Type.LAUNCHROD = Launch rod clearance
+FlightEvent.Type.BURNOUT = Motor burnout
+FlightEvent.Type.EJECTION_CHARGE = Ejection charge
+FlightEvent.Type.STAGE_SEPARATION = Stage separation
+FlightEvent.Type.APOGEE = Apogee
+FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Recovery device deployment
+FlightEvent.Type.GROUND_HIT = Ground hit
+FlightEvent.Type.SIMULATION_END = Simulation end
+FlightEvent.Type.ALTITUDE = Altitude change
+
+! ThrustCurveMotorColumns
+TCurveMotorCol.MANUFACTURER = Manufacturer
+TCurveMotorCol.DESIGNATION = Designation
+TCurveMotorCol.TYPE = Type
+TCurveMotorCol.DIAMETER = Diameter
+TCurveMotorCol.LENGTH = Length
+
+! RocketInfo
+RocketInfo.lengthLine.Length = Length
+RocketInfo.lengthLine.maxdiameter = , max. diameter
+RocketInfo.massText1 = Mass with motors
+RocketInfo.massText2 = Mass with no motors
+RocketInfo.at = at M=
+RocketInfo.cgText = CG:
+RocketInfo.cpText = CP:
+RocketInfo.stabText = Stability:
+RocketInfo.Warning = Warning:
+RocketInfo.Calculating = Calculating...
+RocketInfo.Apogee = Apogee:
+RocketInfo.Maxvelocity = Max. velocity:
+RocketInfo.Maxacceleration = Max. acceleration:
+RocketInfo.apogeeValue = N/A
+RocketInfo.Mach = (Mach
+RocketInfo.velocityValue = N/A
+RocketInfo.accelerationValue = N/A
+
+! FinSet
+FinSet.CrossSection.SQUARE = Square
+FinSet.CrossSection.ROUNDED = Rounded
+FinSet.CrossSection.AIRFOIL = Airfoil
+FinSet.TabRelativePosition.FRONT = Root chord leading edge
+FinSet.TabRelativePosition.CENTER = Root chord midpoint
+FinSet.TabRelativePosition.END = Root chord trailing edge
+
+! FlightDataType
+FlightDataType.TYPE_TIME = Time
+FlightDataType.TYPE_ALTITUDE = Altitude
+FlightDataType.TYPE_VELOCITY_Z = Vertical velocity
+FlightDataType.TYPE_ACCELERATION_Z = Vertical acceleration
+FlightDataType.TYPE_VELOCITY_TOTAL = Total velocity
+FlightDataType.TYPE_ACCELERATION_TOTAL = Total acceleration
+FlightDataType.TYPE_POSITION_X = Position upwind
+FlightDataType.TYPE_POSITION_Y = Position parallel to wind
+FlightDataType.TYPE_POSITION_XY = Lateral distance
+FlightDataType.TYPE_POSITION_DIRECTION = Lateral direction
+FlightDataType.TYPE_VELOCITY_XY = Lateral velocity
+FlightDataType.TYPE_ACCELERATION_XY = Lateral acceleration
+FlightDataType.TYPE_AOA = Angle of attack
+FlightDataType.TYPE_ROLL_RATE = Roll rate
+FlightDataType.TYPE_PITCH_RATE = Pitch rate
+FlightDataType.TYPE_YAW_RATE = Yaw rate
+FlightDataType.TYPE_MASS = Mass
+FlightDataType.TYPE_LONGITUDINAL_INERTIA = Longitudinal moment of inertia
+FlightDataType.TYPE_ROTATIONAL_INERTIA = Rotational moment of inertia
+FlightDataType.TYPE_CP_LOCATION = CP location
+FlightDataType.TYPE_CG_LOCATION = CG location
+FlightDataType.TYPE_STABILITY = Stability margin calibers
+FlightDataType.TYPE_MACH_NUMBER = Mach number
+FlightDataType.TYPE_REYNOLDS_NUMBER = Reynolds number
+FlightDataType.TYPE_THRUST_FORCE = Thrust
+FlightDataType.TYPE_DRAG_FORCE = Drag force
+FlightDataType.TYPE_DRAG_COEFF = Drag coefficient
+FlightDataType.TYPE_AXIAL_DRAG_COEFF = Axial drag coefficient
+FlightDataType.TYPE_FRICTION_DRAG_COEFF = Friction drag coefficient
+FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Pressure drag coefficient
+FlightDataType.TYPE_BASE_DRAG_COEFF = Base drag coefficient
+FlightDataType.TYPE_NORMAL_FORCE_COEFF = Normal force coefficient
+FlightDataType.TYPE_PITCH_MOMENT_COEFF = Pitch moment coefficient
+FlightDataType.TYPE_YAW_MOMENT_COEFF = Yaw moment coefficient
+FlightDataType.TYPE_SIDE_FORCE_COEFF = Side force coefficient
+FlightDataType.TYPE_ROLL_MOMENT_COEFF = Roll moment coefficient
+FlightDataType.TYPE_ROLL_FORCING_COEFF = Roll forcing coefficient
+FlightDataType.TYPE_ROLL_DAMPING_COEFF = Roll damping coefficient
+FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Pitch damping coefficient
+FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Yaw damping coefficient
+FlightDataType.TYPE_REFERENCE_LENGTH = Reference lenght
+FlightDataType.TYPE_REFERENCE_AREA = Reference area
+FlightDataType.TYPE_ORIENTATION_THETA = Vertical orientation (zenith)
+FlightDataType.TYPE_ORIENTATION_PHI = Lateral orientation (azimuth)
+FlightDataType.TYPE_WIND_VELOCITY = Wind velocity
+FlightDataType.TYPE_AIR_TEMPERATURE = Air temperature
+FlightDataType.TYPE_AIR_PRESSURE = Air pressure
+FlightDataType.TYPE_SPEED_OF_SOUND = Speed of sound
+FlightDataType.TYPE_TIME_STEP = Simulation time step
+FlightDataType.TYPE_COMPUTATION_TIME = Computation time
+
+! PlotConfiguration
+PlotConfiguration.Verticalmotion = Vertical motion vs. time
+PlotConfiguration.Totalmotion = Total motion vs. time
+PlotConfiguration.Flightside = Flight side profile
+PlotConfiguration.Stability = Stability vs. time
+PlotConfiguration.Dragcoef = Drag coefficients vs. Mach number
+PlotConfiguration.Rollcharacteristics = Roll characteristics
+PlotConfiguration.Angleofattack = Angle of attack and orientation vs. time
+PlotConfiguration.Simulationtime = Simulation time step and computation time
+
+! Warning
+Warning.LargeAOA.str1 = Large angle of attack encountered.
+Warning.LargeAOA.str2 = Large angle of attack encountered (
+Warning.DISCONTINUITY = Discontinuity in rocket body diameter.
+Warning.THICK_FIN = Thick fins may not be modeled accurately.
+Warning.JAGGED_EDGED_FIN = Jagged-edged fin predictions may be inaccurate.
+Warning.LISTENERS_AFFECTED = Listeners modified the flight simulation
+Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Recovery device opened while motor still burning.
+Warning.FILE_INVALID_PARAMETER = Invalid parameter encountered, ignoring.
+
+
+! Scale dialog
+ScaleDialog.lbl.scaleRocket = Entire rocket
+ScaleDialog.lbl.scaleSubselection = Selection and all subcomponents
+ScaleDialog.lbl.scaleSelection = Only selected component
+ScaleDialog.title = Scale design
+ScaleDialog.lbl.scale = Scale:
+ScaleDialog.lbl.scale.ttip = Select whether to scale the entire design or only the selected component
+ScaleDialog.lbl.scaling = Scaling to apply:
+ScaleDialog.lbl.scaling.ttip = Resulting size, values above 100% grow and values below 100% shrink the design.
+! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"
+ScaleDialog.lbl.scaleFrom = Scale from
+ScaleDialog.lbl.scaleTo = to
+ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and resulting length.
+ScaleDialog.checkbox.scaleMass = Update explicit mass values
+ScaleDialog.checkbox.scaleMass.ttip = Scale mass component and override mass values by the cube of the scaling factor
+ScaleDialog.button.scale = Scale
+ScaleDialog.undo.scaleRocket = Scale rocket
+ScaleDialog.undo.scaleComponent = Scale component
+ScaleDialog.undo.scaleComponents = Scale components
+
+!icons
+Icons.Undo = Undo
+Icons.Redo = Redo
+
+OpenRocketPrintable.Partsdetail = Parts detail
+OpenRocketPrintable.Fintemplates = Fin templates
+OpenRocketPrintable.DesignReport = Design Report
+
+OpenRocketDocument.Redo = Redo
+OpenRocketDocument.Undo = Undo
+
+!EllipticalFinSet
+EllipticalFinSet.Ellipticalfinset = Elliptical fin set
+
+! Optimization
+
+! Modifiers
+
+optimization.modifier.nosecone.length = Length
+optimization.modifier.nosecone.length.desc = Optimize the nose cone length.
+optimization.modifier.nosecone.diameter = Diameter
+optimization.modifier.nosecone.diameter.desc = Optimize the nose cone base diameter.
+optimization.modifier.nosecone.thickness = Thickness
+optimization.modifier.nosecone.thickness.desc = Optimize the nose cone wall thickness.
+optimization.modifier.nosecone.shapeparameter = Shape parameter
+optimization.modifier.nosecone.shapeparameter.desc = Optimize the nose cone shape parameter.
+
+optimization.modifier.transition.length = Length
+optimization.modifier.transition.length.desc = Optimize the transition length.
+optimization.modifier.transition.forediameter = Fore diameter
+optimization.modifier.transition.forediameter.desc = Optimize the transition fore diameter.
+optimization.modifier.transition.aftdiameter = Aft diameter
+optimization.modifier.transition.aftdiameter.desc = Optimize the transition aft diameter.
+optimization.modifier.transition.thickness = Thickness
+optimization.modifier.transition.thickness.desc = Optimize the transition wall thickness.
+optimization.modifier.transition.shapeparameter = Shape parameter
+optimization.modifier.transition.shapeparameter.desc = Optimize the transition shape parameter.
+
+optimization.modifier.bodytube.length = Length
+optimization.modifier.bodytube.length.desc = Optimize the body tube length.
+optimization.modifier.bodytube.outerDiameter = Outer diameter
+optimization.modifier.bodytube.outerDiameter.desc = Optimize the body tube outer diameter while maintaining the wall thickness.
+optimization.modifier.bodytube.thickness = Thickness
+optimization.modifier.bodytube.thickness.desc = Optimize the body tube wall thickness.
+
+optimization.modifier.trapezoidfinset.rootChord = Root chord
+optimization.modifier.trapezoidfinset.rootChord.desc = Optimize the root chord length of the fin set (length of fin at the rocket body).
+optimization.modifier.trapezoidfinset.tipChord = Tip chord
+optimization.modifier.trapezoidfinset.tipChord.desc = Optimize the tip chord length of the fin set (length of fin at outer edge).
+optimization.modifier.trapezoidfinset.sweep = Sweep
+optimization.modifier.trapezoidfinset.sweep.desc = Optimize the sweep of the fin set (distance that the leading edge sweeps backwards).
+optimization.modifier.trapezoidfinset.height = Height
+optimization.modifier.trapezoidfinset.height.desc = Optimize the height (semi-span) of the fin set.
+
+optimization.modifier.ellipticalfinset.length = Root chord
+optimization.modifier.ellipticalfinset.length.desc = Optimize the root chord length of the fin set.
+optimization.modifier.ellipticalfinset.height = Height
+optimization.modifier.ellipticalfinset.height.desc = Optimize the height (semi-span) of the fin set.
+
+optimization.modifier.finset.cant = Cant angle
+optimization.modifier.finset.cant.desc = Optimize the cant angle of the fin set.
+optimization.modifier.finset.position = Position
+optimization.modifier.finset.position.desc = Optimize the fin set position along the rocket body.
+
+optimization.modifier.launchlug.length = Length
+optimization.modifier.launchlug.length.desc = Optimize the launch lug length.
+optimization.modifier.launchlug.outerDiameter = Outer diameter
+optimization.modifier.launchlug.outerDiameter.desc = Optimize the outer diameter of the launch lug.
+optimization.modifier.launchlug.thickness = Thickness
+optimization.modifier.launchlug.thickness.desc = Optimize the launch lug thickness while keeping the outer diameter constant.
+optimization.modifier.launchlug.position = Position
+optimization.modifier.launchlug.position.desc = Optimize the launch lug position along the rocket body.
+
+
+optimization.modifier.internalcomponent.position = Position
+optimization.modifier.internalcomponent.position.desc = Optimize the position of the component relative to the parent component.
+
+optimization.modifier.masscomponent.mass = Mass
+optimization.modifier.masscomponent.mass.desc = Optimize the mass of the mass component.
+
+optimization.modifier.parachute.diameter = Diameter
+optimization.modifier.parachute.diameter.desc = Optimize the parachute canopy diameter.
+optimization.modifier.parachute.coefficient = Drag coefficient
+optimization.modifier.parachute.coefficient.desc = Optimize the drag coefficient of the parachute. Typical parachutes have a drag coefficient of about 0.8.
+
+optimization.modifier.streamer.length = Length
+optimization.modifier.streamer.length.desc = Optimize the length of the streamer.
+optimization.modifier.streamer.width = Width
+optimization.modifier.streamer.width.desc = Optimize the width of the streamer.
+optimization.modifier.streamer.aspectRatio = Aspect ratio
+optimization.modifier.streamer.aspectRatio.desc = Optimize the aspect ratio of the streamer (length/width). You should NOT select streamer length or width at the same time with the aspect ratio.
+optimization.modifier.streamer.coefficient = Drag coefficient
+optimization.modifier.streamer.coefficient.desc = Optimize the drag coefficient of the streamer.
+
+optimization.modifier.recoverydevice.deployDelay = Deployment delay
+optimization.modifier.recoverydevice.deployDelay.desc = Optimize the deployment delay of the recovery device.
+optimization.modifier.recoverydevice.deployAltitude = Deployment altitude
+optimization.modifier.recoverydevice.deployAltitude.desc = Optimize the deployment altitude of the recovery device.
+
+optimization.modifier.rocketcomponent.overrideMass = Override mass
+optimization.modifier.rocketcomponent.overrideMass.desc = Optimize the overridden mass of the component.
+optimization.modifier.rocketcomponent.overrideCG = Override CG
+optimization.modifier.rocketcomponent.overrideCG.desc = Optimize the overridden center of gravity of the component.
+
+optimization.modifier.motormount.overhang = Motor overhang
+optimization.modifier.motormount.overhang.desc = Optimize the motor overhang.
+optimization.modifier.motormount.delay = Motor ignition delay
+optimization.modifier.motormount.delay.desc = Optimize the motor ignition delay.
+
+
+
+
+! General rocket design optimization dialog
+
+GeneralOptimizationDialog.title = Rocket optimization
+GeneralOptimizationDialog.goal.maximize = Maximize value
+GeneralOptimizationDialog.goal.minimize = Minimize value
+GeneralOptimizationDialog.goal.seek = Seek value of
+GeneralOptimizationDialog.btn.start = Start optimization
+GeneralOptimizationDialog.btn.stop = Stop optimization
+GeneralOptimizationDialog.lbl.paramsToOptimize = Parameters to optimize:
+GeneralOptimizationDialog.btn.add = Add
+GeneralOptimizationDialog.btn.add.ttip = Add the selected parameter to the optimization
+GeneralOptimizationDialog.btn.remove = Remove
+GeneralOptimizationDialog.btn.remove.ttip = Remove the selected parameter from the optimization
+GeneralOptimizationDialog.btn.removeAll = Remove all
+GeneralOptimizationDialog.btn.removeAll.ttip = Remove all parameters from the optimization
+GeneralOptimizationDialog.lbl.availableParams = Available parameters:
+GeneralOptimizationDialog.lbl.optimizationOpts = Optimization options
+GeneralOptimizationDialog.lbl.optimizeSim = Optimize simulation:
+GeneralOptimizationDialog.lbl.optimizeSim.ttip = Select which simulation to optimize
+GeneralOptimizationDialog.lbl.optimizeValue = Optimized value:
+GeneralOptimizationDialog.lbl.optimizeValue.ttip = Select what value is to be optimized
+GeneralOptimizationDialog.lbl.optimizeGoal = Optimization goal:
+GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Select the goal of the optimization
+GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Custom value to seek
+GeneralOptimizationDialog.lbl.requireStability = Required stability
+GeneralOptimizationDialog.lbl.requireMinStability = Minimum stability:
+GeneralOptimizationDialog.lbl.requireMinStability.ttip = Require a minimum static stability margin for the design
+GeneralOptimizationDialog.lbl.requireMaxStability = Maximum stability:
+GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Require a maximum static stability margin for the design
+GeneralOptimizationDialog.status.bestValue = Best value:
+GeneralOptimizationDialog.status.bestValue.ttip = Best optimization value found so far.
+GeneralOptimizationDialog.status.stepCount = Step count:
+GeneralOptimizationDialog.status.stepCount.ttip = Number of optimization steps that have been performed.
+GeneralOptimizationDialog.status.evalCount = Evaluations:
+GeneralOptimizationDialog.status.evalCount.ttip = Total number of function evaluations (simulations) that have been performed.
+GeneralOptimizationDialog.status.stepSize = Step size:
+GeneralOptimizationDialog.status.stepSize.ttip = Current optimization step size (relative to the optimization parameter ranges)
+GeneralOptimizationDialog.btn.plotPath = Plot path
+GeneralOptimizationDialog.btn.plotPath.ttip = Plot the optimization path (one and two dimensional optimization only)
+GeneralOptimizationDialog.btn.save = Save path
+GeneralOptimizationDialog.btn.save.ttip = Save the results of the function evaluations (simulations) as a CSV file.
+GeneralOptimizationDialog.btn.apply = Apply optimization
+GeneralOptimizationDialog.btn.apply.ttip = Apply the optimization results to the rocket design
+GeneralOptimizationDialog.btn.reset = Reset
+GeneralOptimizationDialog.btn.reset.ttip = Reset the rocket design to the current rocket design
+GeneralOptimizationDialog.btn.close = Close
+GeneralOptimizationDialog.btn.close.ttip = Close the dialog without modifying the rocket design
+GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters.
+GeneralOptimizationDialog.error.selectParams.title = Select optimization parameters
+GeneralOptimizationDialog.error.optimizationFailure.text = The optimization failed to run:
+GeneralOptimizationDialog.error.optimizationFailure.title = Optimization failed
+GeneralOptimizationDialog.undoText = Apply optimization
+GeneralOptimizationDialog.basicSimulationName = Basic simulation
+GeneralOptimizationDialog.noSimulationName = No simulation
+GeneralOptimizationDialog.table.col.parameter = Parameter
+GeneralOptimizationDialog.table.col.current = Current
+GeneralOptimizationDialog.table.col.min = Minimum
+GeneralOptimizationDialog.table.col.max = Maximum
+GeneralOptimizationDialog.export.header = Include header line
+GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions.
+GeneralOptimizationDialog.export.stability = Stability
+
+
+! Dialog for plotting optimization results
+OptimizationPlotDialog.title = Optimization results
+OptimizationPlotDialog.lbl.zoomInstructions = Click and drag down+right to zoom in, up+left to zoom out
+OptimizationPlotDialog.plot1d.title = Optimization result
+OptimizationPlotDialog.plot1d.series = Optimization result
+OptimizationPlotDialog.plot2d.title = Optimization path
+OptimizationPlotDialog.plot2d.path = Optimization path
+OptimizationPlotDialog.plot2d.evals = Evaluations
+OptimizationPlotDialog.plot.ttip.stability = Stability:
+OptimizationPlotDialog.plot.label.optimum = Optimum
+
+! Optimization parameters
+MaximumAltitudeParameter.name = Apogee altitude
+MaximumVelocityParameter.name = Maximum velocity
+MaximumAccelerationParameter.name = Maximum acceleration
+StabilityParameter.name = Stability
+GroundHitVelocityParameter.name = Ground hit speed
+LandingDistanceParameter.name = Landing distance
+TotalFlightTimeParameter.name = Total flight time
+DeploymentVelocityParameter.name = Velocity at parachute deployment
+
projects / debian / openrocket / blobdiff