3 # English base translation file
5 # Should you need to add new logical keys here is the proposed method
7 # className.ComponentType.componentName
10 # Text tokens within braces should not be translated, e.g.
11 # "The file '{filename}' exists."
12 # They are pieces that are inserted dynamically.
16 ! Set to the name of the current translation file (used for debugging purposes)
17 debug.currentFile = messages.properties
20 RocketActions.checkbox.Donotaskmeagain = Do not ask me again
21 RocketActions.lbl.Youcanchangedefop = You can change the default operation in the preferences.
22 RocketActions.showConfirmDialog.lbl1 = Delete the selected simulations?
23 RocketActions.showConfirmDialog.lbl2 = <html><i>This operation cannot be undone.</i>
24 RocketActions.showConfirmDialog.title = Delete simulations
25 RocketActions.DelCompAct.Delete = Delete
26 RocketActions.DelCompAct.ttip.Delete = Delete the selected component.
27 RocketActions.DelSimuAct.Delete = Delete
28 RocketActions.DelSimuAct.ttip.Delete = Delete the selected simulation.
29 RocketActions.DelAct.Delete = Delete
30 RocketActions.DelAct.ttip.Delete = Delete the selected component or simulation.
31 RocketActions.CutAction.Cut = Cut
32 RocketActions.CutAction.ttip.Cut = Cut this component or simulation to the clipboard and remove from this design
33 RocketActions.CopyAct.Copy = Copy
34 RocketActions.CopyAct.ttip.Copy = Copy this component (and subcomponents) to the clipboard.
35 RocketActions.PasteAct.Paste = Paste
36 RocketActions.PasteAct.ttip.Paste = Paste the component or simulation on the clipboard to the design.
37 RocketActions.EditAct.Edit = Edit
38 RocketActions.EditAct.ttip.Edit = Edit the selected component.
39 RocketActions.NewStageAct.Newstage = New stage
40 RocketActions.NewStageAct.ttip.Newstage = Add a new stage to the rocket design.
41 RocketActions.ActBoosterstage = Booster stage
42 RocketActions.MoveUpAct.Moveup = Move up
43 RocketActions.MoveUpAct.ttip.Moveup = Move this component upwards.
44 RocketActions.MoveDownAct.Movedown = Move down
45 RocketActions.MoveDownAct.ttip.Movedown = Move this component downwards.
48 RocketPanel.FigTypeAct.Sideview = Side view
49 RocketPanel.FigTypeAct.ttip.Sideview = Side view
50 RocketPanel.FigTypeAct.Backview = Back view
51 RocketPanel.FigTypeAct.ttip.Backview = Rear view
52 RocketPanel.lbl.Motorcfg = Motor configuration:
53 RocketPanel.lbl.infoMessage = <html>Click to select Shift+click to select other Double-click to edit Click+drag to move
57 BasicFrame.SimpleFileFilter1 = All rocket designs (*.ork; *.rkt)
58 BasicFrame.SimpleFileFilter2 = OpenRocket designs (*.ork)
59 BasicFrame.SimpleFileFilter3 = RockSim designs (*.rkt)
60 BasicFrame.tab.Rocketdesign = Rocket design
61 BasicFrame.tab.Flightsim = Flight simulations
62 BasicFrame.title.Addnewcomp = Add new component
63 BasicFrame.dlg.lbl1 = Design '
64 BasicFrame.dlg.lbl2 = ' has not been saved.
65 BasicFrame.dlg.lbl3 = Do you want to save it?
66 BasicFrame.dlg.title = Design not saved
67 BasicFrame.StageName.Sustainer = Sustainer
68 BasicFrame.WarningDialog.txt1 = The following problems were encountered while opening
69 BasicFrame.WarningDialog.txt2 = Some design features may not have been loaded correctly.
70 BasicFrame.WarningDialog.title = Warnings while opening file
73 ! General error messages used in multiple contexts
74 error.fileExists.title = File exists
75 error.fileExists.desc = File '{filename}' exists. Do you want to overwrite it?
77 error.writing.title = Error writing file
78 error.writing.desc = An error occurred while writing to the file:
81 ! Labels used in buttons of dialog windows
82 # TODO: Rename these to "btn.xxx"
84 button.cancel = Cancel
87 ! Common labels used in buttons of dialog windows
89 dlg.but.cancel = Cancel
93 ! General file type names
94 filetypes.pdf = PDF files
98 AboutDialog.lbl.version = Version
99 ! The texts below provide additional credits for the translation maintainer
100 ! - In AboutDialog.lbl.translation replace "English" with the current language.
101 ! - AboutDialog.lbl.translator is the translator / group name (may be empty)
102 ! - AboutDialog.lbl.translatorWebsite is a URL to the translator / group (may be empty)
103 ! - AboutDialog.lbl.translatorIcon is the file name of an icon under pix/translators/ (may be empty)
104 AboutDialog.lbl.translation = English translation by:
105 AboutDialog.lbl.translator =
106 AboutDialog.lbl.translatorWebsite =
107 AboutDialog.lbl.translatorIcon =
111 PrintDialog.title = Print or export
112 PrintDialog.but.previewAndPrint = Preview & Print
113 PrintDialog.checkbox.showByStage = Show by stage
114 PrintDialog.lbl.selectElements = Select elements to include:
115 printdlg.but.saveaspdf = Save as PDF
116 printdlg.but.preview = Preview
117 printdlg.but.settings = Settings
118 PrintDialog.error.preview.title = Unable to open preview
119 PrintDialog.error.preview.desc1 = Unable to open PDF preview.
120 PrintDialog.error.preview.desc2 = Please use the "Save as PDF" option instead.
124 PrintSettingsDialog.title = Print settings
125 PrintSettingsDialog.lbl.Templatefillcolor = Template fill color:
126 PrintSettingsDialog.lbl.Templatebordercolor = Template border color:
127 PrintSettingsDialog.lbl.Papersize = Paper size:
128 PrintSettingsDialog.lbl.Paperorientation = Paper orientation:
129 PrintSettingsDialog.but.Reset = Reset
130 PrintSettingsDialog.but.Close = Close
134 bugreport.dlg.title = Bug report
135 bugreport.dlg.but.Sendbugreport = Send bug report
136 bugreport.dlg.but.Sendbugreport.Ttip = Automatically send the bug report to the OpenRocket developers.
137 bugreport.dlg.successmsg1 = Bug report successfully sent.
138 bugreport.dlg.successmsg2 = Thank you for helping make OpenRocket better!
139 bugreport.dlg.successmsg3 = Bug report sent
140 bugreport.dlg.connectedInternet = <html>If connected to the Internet, you can simply click <em>Send bug report</em>.
141 bugreport.dlg.otherwise = Otherwise, send the text below to the address:
142 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.
143 bugreport.dlg.failedmsg1 = OpenRocket was unable to send the bug report:
144 bugreport.dlg.failedmsg2 = Please send the report manually to
145 bugreport.dlg.failedmsg3 = Error sending report
146 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.
147 bugreport.reportDialog.txt2 = <html><b>Please include a short description about what you were doing when the exception occurred.</b>
148 bugreport.dlg.provideDescription = Please provide a description of the bug first.
149 bugreport.dlg.provideDescription.title = Bug description missing
153 debuglogdlg.but.clear = Clear
154 debuglogdlg.OpenRocketdebuglog = OpenRocket debug log
155 debuglogdlg.Displayloglines = Display log lines:
156 debuglogdlg.Follow = Follow
157 debuglogdlg.col.Time = Time
158 debuglogdlg.col.Level = Level
159 debuglogdlg.col.Location = Location
160 debuglogdlg.col.Message = Message
161 debuglogdlg.lbl.Loglinenbr = Log line number:
162 debuglogdlg.lbl.Time = Time:
163 debuglogdlg.lbl.Level = Level:
164 debuglogdlg.lbl.Location = Location:
165 debuglogdlg.lbl.Logmessage = Log message:
166 debuglogdlg.lbl.Stacktrace = Stack trace:
169 ! Edit Motor configuration dialog
170 edtmotorconfdlg.but.removemotor = Remove motor
171 edtmotorconfdlg.but.Selectmotor = Select motor
172 edtmotorconfdlg.but.Removeconfiguration = Remove configuration
173 edtmotorconfdlg.but.Newconfiguration = New configuration
174 edtmotorconfdlg.lbl.Motormounts = <html><b>Motor mounts:</b>
175 edtmotorconfdlg.title.Editmotorconf = Edit motor configurations
176 edtmotorconfdlg.selectcomp = <html>Select which components function as motor mounts:
177 edtmotorconfdlg.lbl.Motorconfig = <html><b>Motor configurations:</b>
178 edtmotorconfdlg.lbl.Configname = Configuration name:
179 edtmotorconfdlg.lbl.Leavenamedefault = Leave name empty for default.
181 ! Example design dialog
182 exdesigndlg.but.open = Open
183 exdesigndlg.lbl.Selectexample = Select example designs to open:
184 exdesigndlg.lbl.Openexampledesign = Open example design
185 exdesigndlg.lbl.Exampledesignsnotfound = Example designs could not be found.
186 exdesigndlg.lbl.Examplesnotfound = Examples not found
189 ! Material edit panel
190 matedtpan.but.new = New
191 matedtpan.but.edit = Edit
192 matedtpan.but.delete = Delete
193 matedtpan.but.revertall = Revert all
194 matedtpan.col.Material = Material
195 matedtpan.col.Type = Type
196 matedtpan.col.Density = Density
197 matedtpan.col.but.ttip.New = Add a new material
198 matedtpan.title.Addcustmaterial = Add a custom material
199 matedtpan.but.ttip.edit = Edit an existing material
200 matedtpan.title.Editmaterial = Edit material
201 matedtpan.title2.Editmaterial = The built-in materials cannot be modified.
202 matedtpan.but.ttip.delete = Delete a user-defined material
203 matedtpan.but.ttip.revertall = Delete all user-defined materials
204 matedtpan.title.Deletealluser-defined = Delete all user-defined materials?
205 matedtpan.title.Revertall = Revert all?
206 matedtpan.lbl.edtmaterials = Editing materials will not affect existing rocket designs.
209 MaterialModel.title.Material = Material
210 MaterialModel.title.Defcustmat = Define custom material
214 pref.dlg.but.add = Add
215 pref.dlg.but.reset = Reset
216 pref.dlg.but.checknow = Check now
217 pref.dlg.but.defaultmetric = Default metric
218 pref.dlg.but.defaultimperial = Default imperial
219 pref.dlg.title.Preferences = Preferences
220 pref.dlg.tab.Units = Units
221 pref.dlg.tab.Defaultunits = Default units
222 pref.dlg.tab.Materials = Materials
223 pref.dlg.tab.Custommaterials = Custom materials
224 pref.dlg.tab.Options = Options
225 pref.dlg.tab.Miscellaneousoptions = Miscellaneous options
226 pref.dlg.lbl.Positiontoinsert = Position to insert new body components:
227 pref.dlg.lbl.Confirmdeletion = Confirm deletion of simulations:
228 pref.dlg.lbl.User-definedthrust = User-defined thrust curves:
229 pref.dlg.Allthrustcurvefiles = All thrust curve files (*.eng; *.rse; *.zip; directories)
230 pref.dlg.RASPfiles = RASP motor files (*.eng)
231 pref.dlg.RockSimfiles = RockSim engine files (*.rse)
232 pref.dlg.ZIParchives = ZIP archives (*.zip)
233 pref.dlg.checkbox.Checkupdates = Check for software updates at startup
234 pref.dlg.ttip.Checkupdatesnow = Check for software updates now
235 pref.dlg.lbl.Selectprefunits = Select your preferred units:
236 pref.dlg.lbl.Rocketdimensions = Rocket dimensions:
237 pref.dlg.lbl.Linedensity = Line density:
238 pref.dlg.lbl.Motordimensions = Motor dimensions:
239 pref.dlg.lbl.Surfacedensity = Surface density:
240 pref.dlg.lbl.Distance = Distance:
241 pref.dlg.lbl.Bulkdensity = Bulk density:
242 pref.dlg.lbl.Velocity = Velocity:
243 pref.dlg.lbl.Surfaceroughness = Surface roughness:
244 pref.dlg.lbl.Acceleration = Acceleration:
245 pref.dlg.lbl.Area = Area:
246 pref.dlg.lbl.Mass = Mass:
247 pref.dlg.lbl.Angle = Angle:
248 pref.dlg.lbl.Force = Force:
249 pref.dlg.lbl.Rollrate = Roll rate:
250 pref.dlg.lbl.Totalimpulse = Total impulse:
251 pref.dlg.lbl.Temperature = Temperature:
252 pref.dlg.lbl.Momentofinertia = Moment of inertia:
253 pref.dlg.lbl.Pressure = Pressure:
254 pref.dlg.lbl.Stability = Stability:
255 pref.dlg.lbl.FlightTime = Flight time:
256 pref.dlg.lbl.effect1 = The effects will take place the next time you open a window.
257 pref.dlg.lbl.Checkingupdates = Checking for updates...
258 pref.dlg.lbl.msg1 = An error occurred while communicating with the server.
259 pref.dlg.lbl.msg2 = Unable to retrieve update information
260 pref.dlg.lbl.msg3 = You are running the latest version of OpenRocket.
261 pref.dlg.lbl.msg4 = No updates available
262 pref.dlg.PrefChoiseSelector1 = Always ask
263 pref.dlg.PrefChoiseSelector2 = Insert in middle
264 pref.dlg.PrefChoiseSelector3 = Add to end
265 pref.dlg.PrefBooleanSelector1 = Delete
266 pref.dlg.PrefBooleanSelector2 = Confirm
268 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.
270 PreferencesDialog.lbl.language = Interface language:
271 PreferencesDialog.languages.default = System default
272 PreferencesDialog.lbl.languageEffect = The language will change the next time you start OpenRocket.
274 ! Simulation edit dialog
275 simedtdlg.but.runsimulation = Run simulation
276 simedtdlg.but.resettodefault = Reset to default
277 simedtdlg.but.add = Add
278 simedtdlg.but.remove = Remove
279 simedtdlg.title.Editsim = Edit simulation
280 simedtdlg.lbl.Simname = Simulation name:
281 simedtdlg.tab.Launchcond = Launch conditions
282 simedtdlg.tab.Simopt = Simulation options
283 simedtdlg.tab.Plotdata = Plot data
284 simedtdlg.tab.Exportdata = Export data
285 simedtdlg.lbl.Motorcfg = Motor configuration:
286 simedtdlg.lbl.ttip.Motorcfg = Select the motor configuration to use.
287 simedtdlg.combo.ttip.motorconf = Select the motor configuration to use.
288 simedtdlg.lbl.Wind = Wind
289 simedtdlg.lbl.Averwindspeed = Average windspeed:
290 simedtdlg.lbl.ttip.Averwindspeed = The average windspeed relative to the ground.
291 simedtdlg.lbl.Stddeviation = Standard deviation:
292 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.
293 simedtdlg.lbl.Turbulenceintensity = Turbulence intensity:
294 simedtdlg.lbl.ttip.Turbulenceintensity1 = <html>The turbulence intensity is the standard deviation divided by the average windspeed.<br>
295 simedtdlg.lbl.ttip.Turbulenceintensity2 = Typical values range from
296 simedtdlg.lbl.ttip.Turbulenceintensity3 = to
297 simedtdlg.border.Atmoscond = Atmospheric conditions
298 simedtdlg.checkbox.InterStdAtmosphere = Use International Standard Atmosphere
299 simedtdlg.checkbox.ttip.InterStdAtmosphere1 = <html>Select to use the International Standard Atmosphere model.<br>This model has a temperature of
300 simedtdlg.checkbox.ttip.InterStdAtmosphere2 = and a pressure of
301 simedtdlg.checkbox.ttip.InterStdAtmosphere3 = at sea level.
302 simedtdlg.lbl.Temperature = Temperature:
303 simedtdlg.lbl.ttip.Temperature = The temperature at the launch site.
304 simedtdlg.lbl.Pressure = Pressure:
305 simedtdlg.lbl.ttip.Pressure = The atmospheric pressure at the launch site.
306 simedtdlg.lbl.Launchsite = Launch site
307 simedtdlg.lbl.Latitude = Latitude:
308 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.
310 simedtdlg.lbl.Longitude = Longitude:
311 simedtdlg.lbl.ttip.Longitude = <html>Required for weather prediction and elevation models.
313 simedtdlg.lbl.Altitude = Altitude:
314 simedtdlg.lbl.ttip.Altitude = <html>The launch altitude above mean sea level.<br>This affects the position of the rocket in the atmospheric model.
315 simedtdlg.border.Launchrod = Launch rod
316 simedtdlg.lbl.Length = Length:
317 simedtdlg.lbl.ttip.Length = The length of the launch rod.
318 simedtdlg.lbl.Angle = Angle:
319 simedtdlg.lbl.ttip.Angle = The angle of the launch rod from vertical.
320 simedtdlg.lbl.Direction = Direction:
321 simedtdlg.lbl.ttip.Direction1 = <html>Direction of the launch rod relative to the wind.<br>
322 simedtdlg.lbl.ttip.Direction2 = = towards the wind,
323 simedtdlg.lbl.ttip.Direction3 = = downwind.
324 simedtdlg.border.Simopt = Simulator options
325 simedtdlg.lbl.Calcmethod = Calculation method:
326 simedtdlg.lbl.ttip.Calcmethod = <html>The Extended Barrowman method calculates aerodynamic forces according <br>to the Barrowman equations extended to accommodate more components.
327 simedtdlg.lbl.ExtBarrowman = Extended Barrowman
328 simedtdlg.lbl.Simmethod = Simulation method:
329 simedtdlg.lbl.ttip.Simmethod1 = <html>The six degree-of-freedom simulator allows the rocket total freedom during flight.<br>
330 simedtdlg.lbl.ttip.Simmethod2 = Integration is performed using a 4<sup>th</sup> order Runge-Kutta 4 numerical integration.
331 simedtdlg.lbl.GeodeticMethod = Geodetic calculations:
332 simedtdlg.lbl.ttip.GeodeticMethodTip = Relate to the calculation of coordinates on the earth. This also enables coriolis effect computations.
333 simedtdlg.lbl.Timestep = Time step:
334 simedtdlg.lbl.ttip.Timestep1 = <html>The time between simulation steps.<br>A smaller time step results in a more accurate but slower simulation.<br>
335 simedtdlg.lbl.ttip.Timestep2 = The 4<sup>th</sup> order simulation method is quite accurate with a time step of
336 simedtdlg.but.ttip.resettodefault = Reset the time step to its default value (
337 simedtdlg.border.Simlist = Simulator listeners
338 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.
339 simedtdlg.txt.longA2 = For details on writing simulation listeners, see the OpenRocket technical documentation.
340 simedtdlg.lbl.Curlist = Current listeners:
341 simedtdlg.lbl.Addsimlist = Add simulation listener
342 simedtdlg.lbl.Noflightdata = No flight data available.
343 simedtdlg.lbl.runsimfirst = Please run the simulation first.
344 simedtdlg.chart.Simflight = Simulated flight
345 simedtdlg.dlg.Simres = Simulation results
346 simedtdlg.IntensityDesc.None = None
347 simedtdlg.IntensityDesc.Verylow = Very low
348 simedtdlg.IntensityDesc.Low = Low
349 simedtdlg.IntensityDesc.Medium = Medium
350 simedtdlg.IntensityDesc.High = High
351 simedtdlg.IntensityDesc.Veryhigh = Very high
352 simedtdlg.IntensityDesc.Extreme = Extreme
354 GeodeticComputationStrategy.flat.name = Flat Earth
355 GeodeticComputationStrategy.flat.desc = Perform computations with a flat Earth approximation. Sufficient for low-altitude flights.
356 GeodeticComputationStrategy.spherical.name = Spherical approximation
357 GeodeticComputationStrategy.spherical.desc = <html>Perform geodetic computations assuming a spherical Earth.<br>This is sufficiently accurate for almost all purposes.
358 GeodeticComputationStrategy.wgs84.name = WGS84 ellipsoid
359 GeodeticComputationStrategy.wgs84.desc = <html>Perform geodetic computations on the WGS84 reference ellipsoid using Vincenty's method.<br>Slower and unnecessary in most cases.
365 simpanel.but.newsimulation = New simulation
366 simpanel.but.editsimulation = Edit simulation
367 simpanel.but.runsimulations = Run simulations
368 simpanel.but.deletesimulations = Delete simulations
369 simpanel.but.plotexport = Plot / export
370 simpanel.but.ttip.newsimulation = Add a new simulation
371 simpanel.but.ttip.editsim = Edit the selected simulation
372 simpanel.but.ttip.runsimu = Re-run the selected simulations
373 simpanel.but.ttip.deletesim = Delete the selected simulations
374 simpanel.checkbox.donotask = Do not ask me again
375 simpanel.lbl.defpref = You can change the default operation in the preferences.
376 simpanel.dlg.lbl.DeleteSim1 = Delete the selected simulations?
377 simpanel.dlg.lbl.DeleteSim2 = <html><i>This operation cannot be undone.</i>
378 simpanel.dlg.lbl.DeleteSim3 = Delete simulations
379 simpanel.col.Name = Name
380 simpanel.col.Motors = Motors
381 simpanel.col.Apogee = Apogee
382 simpanel.col.Maxvelocity = Max. velocity
383 simpanel.col.Maxacceleration = Max. acceleration
384 simpanel.col.Timetoapogee = Time to apogee
385 simpanel.col.Flighttime = Flight time
386 simpanel.col.Groundhitvelocity = Ground hit velocity
388 ! SimulationRunDialog
389 SimuRunDlg.title.RunSim = Running simulations...
390 SimuRunDlg.lbl.Running = Running ...
391 SimuRunDlg.lbl.Simutime = Simulation time:
392 SimuRunDlg.lbl.Altitude = Altitude:
393 SimuRunDlg.lbl.Velocity = Velocity:
394 SimuRunDlg.msg.Unabletosim = Unable to simulate:
395 SimuRunDlg.msg.errorOccurred = An error occurred during the simulation:
396 SimuRunDlg.msg.AnException1 = An exception occurred during the simulation:
397 SimuRunDlg.msg.AnException2 = Please report this as a bug along with the details below.
398 SimuRunDlg.msg.AssertionError1 = A computation error occurred during the simulation.
399 SimuRunDlg.msg.AssertionError2 = Please report this as a bug along with the details below.
400 SimuRunDlg.msg.unknownerror1 = An unknown error was encountered during the simulation.
401 SimuRunDlg.msg.unknownerror2 = The program may be unstable, you should save all your designs and restart OpenRocket now!
404 RK4SimulationStepper.error.valuesTooLarge = Simulation values exceeded limits. Try selecting a shorter time step.
407 ! SimulationExportPanel
408 SimExpPan.desc = Comma Separated Files (*.csv)
409 SimExpPan.border.Vartoexport = Variables to export
410 SimExpPan.but.Selectall = Select all
411 SimExpPan.but.Selectnone = Select none
412 SimExpPan.border.Fieldsep = Field separator
413 SimExpPan.lbl.Fieldsepstr = Field separator string:
414 SimExpPan.lbl.longA1 = <html>The string used to separate the fields in the exported file.<br>
415 SimExpPan.lbl.longA2 = Use ',' for a Comma Separated Values (CSV) file.
416 SimExpPan.checkbox.Includesimudesc = Include simulation description
417 SimExpPan.checkbox.ttip.Includesimudesc = Include a comment at the beginning of the file describing the simulation.
418 SimExpPan.border.Comments = Comments
419 SimExpPan.checkbox.Includefielddesc = Include field descriptions
420 SimExpPan.checkbox.ttip.Includefielddesc = Include a comment line with the descriptions of the exported variables.
421 SimExpPan.checkbox.Incflightevents = Include flight events
422 SimExpPan.checkbox.ttip.Incflightevents = Include a comment line for every flight event.
423 SimExpPan.lbl.Commentchar = Comment character:
424 SimExpPan.lbl.ttip.Commentchar = The character(s) that mark a comment line.
425 SimExpPan.but.Exporttofile = Export to file...
426 SimExpPan.Fileexists.desc1 = File \"
427 SimExpPan.Fileexists.desc2 = \" exists. Overwrite?
428 SimExpPan.Fileexists.title = File exists
429 SimExpPan.ExportingVar.desc1 = Exporting 1 variable out of
430 SimExpPan.ExportingVar.desc2 = Exporting
431 SimExpPan.ExportingVar.desc3 = variables out of
432 SimExpPan.Col.Variable = Variable
433 SimExpPan.Col.Unit = Unit
436 CsvOptionPanel.separator.space = SPACE
437 CsvOptionPanel.separator.tab = TAB
442 MotorPlot.title.Motorplot = Motor plot
443 MotorPlot.but.Select = Select
444 MotorPlot.Chart.Motorthrustcurve = Motor thrust curve
445 MotorPlot.Chart.Time = Time / s
446 MotorPlot.Chart.Thrust = Thrust / N
447 MotorPlot.txt.Designation = Designation:
448 MotorPlot.txt.Manufacturer = Manufacturer:
449 MotorPlot.txt.Type = Type:
450 MotorPlot.txt.Delays = Delays:
451 MotorPlot.txt.Comment = Comment:\n
455 ! Simulation plot panel
456 simplotpanel.lbl.Presetplotconf = Preset plot configurations:
457 simplotpanel.lbl.Xaxistype = X axis type:
458 simplotpanel.lbl.Unit = Unit:
459 simplotpanel.lbl.Yaxistypes = Y axis types:
460 simplotpanel.lbl.Flightevents = Flight events:
461 simplotpanel.but.All = All
462 simplotpanel.but.None = None
463 simplotpanel.but.NewYaxisplottype = New Y axis plot type
464 simplotpanel.but.Plotflight = Plot flight
465 simplotpanel.lbl.Axis = Axis:
466 simplotpanel.but.ttip.Removethisplot = Remove this plot
467 simplotpanel.Desc = The data will be plotted in time order even if the X axis type is not time.
468 simplotpanel.OptionPane.lbl1 = A maximum of 15 plots is allowed.
469 simplotpanel.OptionPane.lbl2 = Cannot add plot
470 simplotpanel.AUTO_NAME = Auto
471 simplotpanel.LEFT_NAME = Left
472 simplotpanel.RIGHT_NAME = Right
473 simplotpanel.CUSTOM = Custom
474 SimulationPlotPanel.error.noPlotSelected = Please add one or more variables to plot on the Y-axis.
475 SimulationPlotPanel.error.noPlotSelected.title = Nothing to plot
478 ! Component add buttons
479 compaddbuttons.Bodycompandfinsets = Body components and fin sets
480 compaddbuttons.Nosecone = Nose cone
481 compaddbuttons.Bodytube = Body tube
482 compaddbuttons.Transition = Transition
483 compaddbuttons.Trapezoidal = Trapezoidal
484 compaddbuttons.Elliptical = Elliptical
485 compaddbuttons.Freeform = Freeform
486 compaddbuttons.Launchlug = Launch lug
487 compaddbuttons.Innercomponent = Inner component
488 compaddbuttons.Innertube = Inner tube
489 compaddbuttons.Coupler = Coupler
490 compaddbuttons.Centeringring = Centering\nring
491 compaddbuttons.Bulkhead = Bulkhead
492 compaddbuttons.Engineblock = Engine\nblock
493 compaddbuttons.Massobjects = Mass objects
494 compaddbuttons.Parachute = Parachute
495 compaddbuttons.Streamer = Streamer
496 compaddbuttons.Shockcord = Shock cord
497 compaddbuttons.Masscomponent = Mass\ncomponent
498 compaddbuttons.Donotaskmeagain = Do not ask me again
499 compaddbuttons.Selectcomppos = Select component position
500 compaddbuttons.lbl.Youcanchange = You can change the default operation in the preferences.
501 compaddbuttons.lbl.insertcomp = Insert the component after the current component or as the last component?
502 compaddbuttons.askPosition.Inserthere = Insert here
503 compaddbuttons.askPosition.Addtotheend = Add to the end
504 compaddbuttons.askPosition.Cancel = Cancel
506 ! Component Analysis Dialog
507 componentanalysisdlg.componentanalysis = Component analysis
508 componentanalysisdlg.lbl.winddir = Wind direction:
509 componentanalysisdlg.TitledBorder.warnings = Warnings:
510 componentanalysisdlg.ToggleBut.worst = Worst
511 componentanalysisdlg.lbl.angleofattack = Angle of attack:
512 componentanalysisdlg.lbl.machnumber = Mach number:
513 componentanalysisdlg.lbl.rollrate = Roll rate:
514 componentanalysisdlg.lbl.activestages = Active stages:
515 componentanalysisdlg.lbl.motorconf = Motor configuration:
516 componentanalysisdlg.TabStability.Col = Component
517 componentanalysisdlg.TabStability = Stability
518 componentanalysisdlg.TabStability.ttip = Stability information
519 componentanalysisdlg.dragTableModel.Col.Component = Component
520 componentanalysisdlg.dragTableModel.Col.Pressure = <html>Pressure C<sub>D</sub>
521 componentanalysisdlg.dragTableModel.Col.Base = <html>Base C<sub>D</sub>
522 componentanalysisdlg.dragTableModel.Col.friction = <html>Friction C<sub>D</sub>
523 componentanalysisdlg.dragTableModel.Col.total = <html>Total C<sub>D</sub>
524 componentanalysisdlg.dragTabchar = Drag characteristics
525 componentanalysisdlg.dragTabchar.ttip = Drag characteristics
526 componentanalysisdlg.rollTableModel.Col.component = Component
527 componentanalysisdlg.rollTableModel.Col.rollforc = Roll forcing coefficient
528 componentanalysisdlg.rollTableModel.Col.rolldamp = Roll damping coefficient
529 componentanalysisdlg.rollTableModel.Col.total = <html>Total C<sub>l</sub>
530 componentanalysisdlg.rollTableModel = Roll dynamics
531 componentanalysisdlg.rollTableModel.ttip = Roll dynamics
532 componentanalysisdlg.println.closingmethod = Closing method called:
533 componentanalysisdlg.println.settingnam = SETTING NAN VALUES
534 componentanalysisdlg.lbl.reflenght = Reference length:
535 componentanalysisdlg.lbl.refarea = Reference area:
536 !componentanalysisdlg.But.close =Close
537 componentanalysisdlg.TabStability.Col.Component = Component
539 ! Custom Material dialog
540 custmatdlg.title.Custommaterial = Custom material
541 custmatdlg.lbl.Materialname = Material name:
542 custmatdlg.lbl.Materialtype = Material type:
543 custmatdlg.lbl.Materialdensity = Material density:
544 custmatdlg.checkbox.Addmaterial = Add material to database
547 ! Ring Component Config
548 ringcompcfg.OuterRadius = OuterRadius
549 ringcompcfg.Automatic = Automatic
550 ringcompcfg.InnerRadius = InnerRadius
551 ringcompcfg.Thickness = Thickness
552 ringcompcfg.Length = Length
553 ringcompcfg.Positionrelativeto = Position relative to:
554 ringcompcfg.plus = plus
555 ringcompcfg.PositionValue = PositionValue
556 ringcompcfg.Radialdistance = Radial distance:
557 ringcompcfg.Distancefrom = Distance from the rocket centerline
558 ringcompcfg.Radialdirection = Radial direction:
559 ringcompcfg.radialdirectionfrom = The radial direction from the rocket centerline
560 ringcompcfg.but.Reset = Reset
561 ringcompcfg.but.Resetcomponant = Reset the component to the rocket centerline
562 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.
563 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.
567 BodyTubecfg.lbl.Bodytubelength = Body tube length:
568 BodyTubecfg.lbl.Outerdiameter = Outer diameter:
569 BodyTubecfg.lbl.Innerdiameter = Inner diameter:
570 BodyTubecfg.lbl.Wallthickness = Wall thickness:
571 BodyTubecfg.tab.General = General
572 BodyTubecfg.tab.Generalproperties = General properties
573 BodyTubecfg.tab.Motor = Motor
574 BodyTubecfg.tab.Motormountconf = Motor mount configuration
575 BodyTubecfg.checkbox.Automatic = Automatic
576 BodyTubecfg.checkbox.Filled = Filled
579 FinSetConfig.tab.Fintabs = Fin tabs
580 FinSetConfig.tab.Through-the-wall = Through-the-wall fin tabs
581 FinSetConfig.but.Converttofreeform = Convert to freeform
582 FinSetConfig.but.Converttofreeform.ttip = Convert this fin set into a freeform fin set
583 FinSetConfig.Convertfinset = Convert fin set
584 FinSetConfig.but.Splitfins = Split fins
585 FinSetConfig.but.Splitfins.ttip = Split the fin set into separate fins
586 FinSetConfig.but.AutoCalc = Calculate automatically
587 FinSetConfig.lbl.Through-the-wall = Through-the-wall fin tabs:
588 FinSetConfig.lbl.Tablength = Tab length:
589 FinSetConfig.ttip.Tablength = The length of the fin tab.
590 FinSetConfig.lbl.Tabheight = Tab height:
591 FinSetConfig.ttip.Tabheight = The spanwise height of the fin tab.
592 FinSetConfig.lbl.Tabposition = Tab position:
593 FinSetConfig.ttip.Tabposition = The position of the fin tab.
594 FinSetConfig.lbl.relativeto = relative to
596 ! MotorDatabaseLoadingDialog
597 MotorDbLoadDlg.title = Loading motors
598 MotorDbLoadDlg.Loadingmotors = Loading motors...
601 RocketCfg.lbl.Designname = Design name:
602 RocketCfg.lbl.Designer = Designer:
603 RocketCfg.lbl.Comments = Comments:
604 RocketCfg.lbl.Revisionhistory = Revision history:
605 RocketCfg.lbl.Material = Material:
608 ShockCordCfg.lbl.Shockcordlength = Shock cord length:
610 ! RocketComponentConfig
611 RocketCompCfg.lbl.Componentname = Component name:
612 RocketCompCfg.ttip.Thecomponentname = The component name.
613 RocketCompCfg.tab.Override = Override
614 RocketCompCfg.tab.MassandCGoverride = Mass and CG override options
615 RocketCompCfg.tab.Figure = Figure
616 RocketCompCfg.tab.Figstyleopt = Figure style options
617 RocketCompCfg.tab.Comment = Comment
618 RocketCompCfg.tab.Specifyacomment = Specify a comment for the component
619 RocketCompCfg.lbl.Mass = Mass:
620 RocketCompCfg.lbl.Componentmass = Component mass:
621 RocketCompCfg.lbl.overriddento = (overridden to
622 RocketCompCfg.lbl.overriddenby = (overridden by
623 RocketCompCfg.lbl.Componentmaterial = Component material:
624 RocketCompCfg.lbl.Componentfinish = Component finish:
625 RocketCompCfg.lbl.ttip.componentmaterialaffects = The component material affects the weight of the component.
626 RocketCompCfg.combo.ttip.componentmaterialaffects = The component material affects the weight of the component.
627 RocketCompCfg.lbl.longA1 = <html>The component finish affects the aerodynamic drag of the component.<br>
628 RocketCompCfg.lbl.longA2 = The value indicated is the average roughness height of the surface.
629 RocketCompCfg.but.Setforall = Set for all
630 RocketCompCfg.but.ttip.Setforall = Set this finish for all components of the rocket.
631 RocketCompCfg.lbl.Overridemassorcenter = Override the mass or center of gravity of the
632 RocketCompCfg.checkbox.Overridemass = Override mass:
633 RocketCompCfg.checkbox.Overridecenterofgrav = Override center of gravity:
634 RocketCompCfg.checkbox.OverridemassandCG = Override mass and CG of all subcomponents
635 RocketCompCfg.lbl.longB1 = <html>The overridden mass does not include motors.<br>
636 RocketCompCfg.lbl.longB2 = The center of gravity is measured from the front end of the
637 RocketCompCfg.lbl.Commentsonthe = Comments on the
638 RocketCompCfg.lbl.Figurestyle = Figure style:
639 RocketCompCfg.lbl.Componentcolor = Component color:
640 RocketCompCfg.lbl.Choosecolor = Choose color
641 RocketCompCfg.checkbox.Usedefaultcolor = Use default color
642 RocketCompCfg.lbl.Complinestyle = Component line style:
643 RocketCompCfg.but.Saveasdefstyle = Save as default style
644 RocketCompCfg.lbl.Diameter = Diameter:
645 RocketCompCfg.lbl.Length = Length:
646 RocketCompCfg.lbl.Thickness = Thickness:
647 RocketCompCfg.checkbox.Endcapped = End capped
648 RocketCompCfg.ttip.Endcapped = Whether the end of the shoulder is capped.
649 RocketCompCfg.title.Noseconeshoulder = Nose cone shoulder
650 RocketCompCfg.title.Aftshoulder = Aft shoulder
651 RocketCompCfg.border.Foreshoulder = Fore shoulder
652 !RocketCompCfg.lbl.Length = Length:
655 BulkheadCfg.tab.Diameter = Diameter:
656 BulkheadCfg.tab.Thickness = Thickness:
657 BulkheadCfg.tab.General = General
658 BulkheadCfg.tab.Generalproperties = General properties
661 CenteringRingCfg.tab.Outerdiam = Outer diameter:
662 CenteringRingCfg.tab.Innerdiam = Inner diameter:
663 CenteringRingCfg.tab.Thickness = Thickness:
664 CenteringRingCfg.tab.General = General
665 CenteringRingCfg.tab.Generalproperties = General properties
667 !ComponentConfigDialog
668 ComponentCfgDlg.configuration = configuration
669 ComponentCfgDlg.configuration1 =
670 ComponentCfgDlg.Modify = Modify
672 !EllipticalFinSetConfig
673 EllipticalFinSetCfg.Nbroffins = Number of fins:
674 EllipticalFinSetCfg.Rotation = Rotation:
675 EllipticalFinSetCfg.Fincant = Fin cant:
676 EllipticalFinSetCfg.Rootchord = Root chord:
677 EllipticalFinSetCfg.Height = Height:
678 EllipticalFinSetCfg.Positionrelativeto = Position relative to:
679 EllipticalFinSetCfg.plus = plus
680 EllipticalFinSetCfg.FincrossSection = Fin cross section:
681 EllipticalFinSetCfg.Thickness = Thickness:
682 EllipticalFinSetCfg.General = General
683 EllipticalFinSetCfg.Generalproperties = General properties
684 EllipticalFinSetCfg.ttip.Fincant = The angle that the fins are canted with respect to the rocket body.
686 !FreeformFinSetConfig
687 FreeformFinSetCfg.tab.General = General
688 FreeformFinSetCfg.tab.ttip.General = General properties
689 FreeformFinSetCfg.tab.Shape = Shape
690 FreeformFinSetCfg.tab.ttip.Finshape = Fin shape
691 FreeformFinSetCfg.lbl.Numberoffins = Number of fins:
692 FreeformFinSetCfg.lbl.Finrotation = Fin rotation:
693 FreeformFinSetCfg.lbl.Fincant = Fin cant:
694 FreeformFinSetCfg.lbl.ttip.Fincant = The angle that the fins are canted with respect to the rocket body.
695 FreeformFinSetCfg.lbl.Posrelativeto = Position relative to:
696 FreeformFinSetCfg.lbl.plus = plus
697 FreeformFinSetCfg.lbl.FincrossSection = Fin cross section:
698 FreeformFinSetCfg.lbl.Thickness = Thickness:
699 ! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle
700 FreeformFinSetConfig.lbl.doubleClick1 = Double-click
701 FreeformFinSetConfig.lbl.doubleClick2 = to edit
702 FreeformFinSetConfig.lbl.clickDrag = Click+drag: Add and move points
703 FreeformFinSetConfig.lbl.ctrlClick = Ctrl+click: Remove point
707 InnerTubeCfg.tab.Motor = Motor
708 InnerTubeCfg.tab.ttip.Motor = Motor mount configuration
709 InnerTubeCfg.tab.Cluster = Cluster
710 InnerTubeCfg.tab.ttip.Cluster = Cluster configuration
711 InnerTubeCfg.tab.Radialpos = Radial position
712 InnerTubeCfg.tab.ttip.Radialpos = Radial position
713 InnerTubeCfg.lbl.Selectclustercfg = Select cluster configuration:
714 InnerTubeCfg.lbl.TubeSep = Tube separation:
715 InnerTubeCfg.lbl.ttip.TubeSep = The separation of the tubes, 1.0 = touching each other
716 InnerTubeCfg.lbl.Rotation = Rotation:
717 InnerTubeCfg.lbl.ttip.Rotation = Rotation angle of the cluster configuration
718 InnerTubeCfg.lbl.Rotangle = Rotation angle of the cluster configuration
719 InnerTubeCfg.but.Splitcluster = Split cluster
720 InnerTubeCfg.lbl.longA1 = <html>Split the cluster into separate components.<br>
721 InnerTubeCfg.lbl.longA2 = This also duplicates all components attached to this inner tube.
722 InnerTubeCfg.but.Resetsettings = Reset settings
723 InnerTubeCfg.but.ttip.Resetsettings = Reset the separation and rotation to the default values
726 LaunchLugCfg.lbl.Length = Length:
727 LaunchLugCfg.lbl.Outerdiam = Outer diameter:
728 LaunchLugCfg.lbl.Innerdiam = Inner diameter:
729 LaunchLugCfg.lbl.Thickness = Thickness:
730 LaunchLugCfg.lbl.Radialpos = Radial position:
731 LaunchLugCfg.lbl.Posrelativeto = Position relative to:
732 LaunchLugCfg.lbl.plus = plus
733 LaunchLugCfg.tab.General = General
734 LaunchLugCfg.tab.Generalprop = General properties
736 ! MassComponentConfig
737 MassComponentCfg.lbl.Mass = Mass:
738 MassComponentCfg.lbl.Length = Length:
739 MassComponentCfg.lbl.Diameter = Diameter:
740 MassComponentCfg.lbl.PosRelativeto = Position relative to:
741 MassComponentCfg.lbl.plus = plus
742 MassComponentCfg.tab.General = General
743 MassComponentCfg.tab.ttip.General = General properties
744 MassComponentCfg.tab.Radialpos = Radial position
745 MassComponentCfg.tab.ttip.Radialpos = Radial position configuration
746 MassComponentCfg.lbl.Radialdistance = Radial distance:
747 MassComponentCfg.lbl.Radialdirection = Radial direction:
748 MassComponentCfg.but.Reset = Reset
751 MotorCfg.checkbox.compmotormount = This component is a motor mount
752 MotorCfg.lbl.Motorcfg = Motor configuration:
753 MotorCfg.but.New = New
754 MotorCfg.lbl.Currentmotor = Current motor:
755 MotorCfg.lbl.Motoroverhang = Motor overhang:
756 MotorCfg.lbl.Ignitionat = Ignition at:
757 MotorCfg.lbl.plus = plus
758 MotorCfg.lbl.seconds = seconds
759 MotorCfg.lbl.longA1 = The current design has only one stage.
760 MotorCfg.lbl.longA2 = Stages can be added by clicking \"New stage\".
761 MotorCfg.lbl.longB1 = The current design has
762 MotorCfg.lbl.longB2 = stages.
763 MotorCfg.but.Selectmotor = Select motor
764 MotorCfg.but.Removemotor = Remove motor
765 MotorCfg.lbl.motorLabel = None
768 NoseConeCfg.lbl.Noseconeshape = Nose cone shape:
769 NoseConeCfg.lbl.Shapeparam = Shape parameter:
770 NoseConeCfg.lbl.Noseconelength = Nose cone length:
771 NoseConeCfg.lbl.Basediam = Base diameter:
772 NoseConeCfg.checkbox.Automatic = Automatic
773 NoseConeCfg.lbl.Wallthickness = Wall thickness:
774 NoseConeCfg.checkbox.Filled = Filled
775 NoseConeCfg.tab.General = General
776 NoseConeCfg.tab.ttip.General = General properties
777 NoseConeCfg.tab.Shoulder = Shoulder
778 NoseConeCfg.tab.ttip.Shoulder = Shoulder properties
781 ParachuteCfg.lbl.Canopy = Canopy:
782 ParachuteCfg.lbl.Diameter = Diameter:
783 ParachuteCfg.lbl.Material = Material:
784 ParachuteCfg.combo.MaterialModel = The component material affects the weight of the component.
785 ParachuteCfg.lbl.longA1 = <html>Drag coefficient C<sub>D</sub>:
786 ParachuteCfg.lbl.longB1 = <html>The drag coefficient relative to the total area of the parachute.<br>
787 ParachuteCfg.lbl.longB2 = A larger drag coefficient yields a slowed descent rate.
788 ParachuteCfg.lbl.longB3 = A typical value for parachutes is 0.8.
789 ParachuteCfg.but.Reset = Reset
790 ParachuteCfg.lbl.Shroudlines = Shroud lines:
791 ParachuteCfg.lbl.Numberoflines = Number of lines:
792 ParachuteCfg.lbl.Linelength = Line length:
793 ParachuteCfg.lbl.Material = Material:
794 ParachuteCfg.lbl.Posrelativeto = Position relative to:
795 ParachuteCfg.lbl.plus = plus
796 ParachuteCfg.lbl.Packedlength = Packed length:
797 ParachuteCfg.lbl.Packeddiam = Packed diameter:
798 ParachuteCfg.lbl.Deploysat = Deploys at:
799 ParachuteCfg.lbl.seconds = seconds
800 ParachuteCfg.lbl.Altitude = Altitude:
801 ParachuteCfg.tab.General = General
802 ParachuteCfg.tab.ttip.General = General properties
803 ParachuteCfg.tab.Radialpos = Radial position
804 ParachuteCfg.tab.ttip.Radialpos = Radial position configuration
805 ParachuteCfg.lbl.Radialdistance = Radial distance:
806 ParachuteCfg.lbl.Radialdirection = Radial direction:
807 ParachuteCfg.but.Reset = Reset
808 ParachuteCfg.lbl.plusdelay = plus
811 ShockCordCfg.lbl.Shockcordlength = Shock cord length:
812 ShockCordCfg.lbl.Shockcordmaterial = Shock cord material:
813 ShockCordCfg.lbl.Posrelativeto = Position relative to:
814 ShockCordCfg.lbl.plus = plus
815 ShockCordCfg.lbl.Packedlength = Packed length:
816 ShockCordCfg.lbl.Packeddiam = Packed diameter:
817 ShockCordCfg.tab.General = General
818 ShockCordCfg.tab.ttip.General = General properties
821 SleeveCfg.tab.Outerdiam = Outer diameter:
822 SleeveCfg.tab.Innerdiam = Inner diameter:
823 SleeveCfg.tab.Wallthickness = Wall thickness:
824 SleeveCfg.tab.Length = Length:
825 SleeveCfg.tab.General = General
826 SleeveCfg.tab.Generalproperties = General properties
829 StreamerCfg.lbl.Striplength = Strip length:
830 StreamerCfg.lbl.Stripwidth = Strip width:
831 StreamerCfg.lbl.Striparea = Strip area:
832 StreamerCfg.lbl.Aspectratio = Aspect ratio:
833 StreamerCfg.lbl.Material = Material:
834 StreamerCfg.combo.ttip.MaterialModel = The component material affects the weight of the component.
835 StreamerCfg.lbl.longA1 = <html>Drag coefficient C<sub>D</sub>:
836 StreamerCfg.lbl.longB1 = <html>The drag coefficient relative to the total area of the streamer.<br>
837 StreamerCfg.lbl.longB2 = A larger drag coefficient yields a slowed descent rate.
838 StreamerCfg.lbl.Automatic = Automatic
839 StreamerCfg.lbl.longC1 = The drag coefficient is relative to the area of the streamer.
840 StreamerCfg.lbl.Posrelativeto = Position relative to:
841 StreamerCfg.lbl.plus = plus
842 StreamerCfg.lbl.Packedlength = Packed length:
843 StreamerCfg.lbl.Packeddiam = Packed diameter:
844 StreamerCfg.lbl.Deploysat = Deploys at:
845 StreamerCfg.lbl.seconds = seconds
846 StreamerCfg.lbl.Altitude = Altitude:
847 StreamerCfg.tab.General = General
848 StreamerCfg.tab.ttip.General = General properties
849 StreamerCfg.tab.Radialpos = Radial position
850 StreamerCfg.tab.ttip.Radialpos = Radial position configuration
851 StreamerCfg.lbl.Radialdistance = Radial distance:
852 StreamerCfg.lbl.Radialdirection = Radial direction:
853 StreamerCfg.but.Reset = Reset
854 StreamerCfg.lbl.plusdelay = plus
856 ! ThicknessRingComponentConfig
857 ThicknessRingCompCfg.tab.Outerdiam = Outer diameter:
858 ThicknessRingCompCfg.tab.Innerdiam = Inner diameter:
859 ThicknessRingCompCfg.tab.Wallthickness = Wall thickness:
860 ThicknessRingCompCfg.tab.Length = Length:
861 ThicknessRingCompCfg.tab.General = General
862 ThicknessRingCompCfg.tab.Generalprop = General properties
865 TransitionCfg.lbl.Transitionshape = Transition shape:
866 TransitionCfg.checkbox.Clipped = Clipped
867 TransitionCfg.lbl.Shapeparam = Shape parameter:
868 TransitionCfg.lbl.Transitionlength = Transition length:
869 TransitionCfg.lbl.Forediam = Fore diameter:
870 TransitionCfg.checkbox.Automatic = Automatic
871 TransitionCfg.lbl.Aftdiam = Aft diameter:
872 TransitionCfg.lbl.Wallthickness = Wall thickness:
873 TransitionCfg.checkbox.Filled = Filled
874 TransitionCfg.tab.General = General
875 TransitionCfg.tab.Generalproperties = General properties
876 TransitionCfg.tab.Shoulder = Shoulder
877 TransitionCfg.tab.Shoulderproperties = Shoulder properties
879 ! TrapezoidFinSetConfig
880 TrapezoidFinSetCfg.lbl.Nbroffins = Number of fins:
881 TrapezoidFinSetCfg.lbl.ttip.Nbroffins = The number of fins in the fin set.
882 TrapezoidFinSetCfg.lbl.Finrotation = Fin rotation:
883 TrapezoidFinSetCfg.lbl.ttip.Finrotation = The angle of the first fin in the fin set.
884 TrapezoidFinSetCfg.lbl.Fincant = Fin cant:
885 TrapezoidFinSetCfg.lbl.ttip.Fincant =The angle that the fins are canted with respect to the rocket body.
886 TrapezoidFinSetCfg.lbl.Rootchord = Root chord:
887 TrapezoidFinSetCfg.lbl.Tipchord = Tip chord:
888 TrapezoidFinSetCfg.lbl.Height = Height:
889 TrapezoidFinSetCfg.lbl.Sweeplength = Sweep length:
890 TrapezoidFinSetCfg.lbl.Sweepangle = Sweep angle:
891 TrapezoidFinSetCfg.lbl.FincrossSection = Fin cross section:
892 TrapezoidFinSetCfg.lbl.Thickness = Thickness:
893 TrapezoidFinSetCfg.lbl.Posrelativeto = Position relative to:
894 TrapezoidFinSetCfg.lbl.plus = plus
895 TrapezoidFinSetCfg.tab.General = General
896 TrapezoidFinSetCfg.tab.Generalproperties = General properties
898 !MotorConfigurationModel
899 MotorCfgModel.Editcfg = Edit configurations
901 ! StorageOptionChooser
902 StorageOptChooser.lbl.Simdatatostore = Simulated data to store:
903 StorageOptChooser.rdbut.Allsimdata = All simulated data
904 StorageOptChooser.lbl.longA1 = <html>Store all simulated data.<br>
905 StorageOptChooser.lbl.longA2 = This can result in very large files!
906 StorageOptChooser.rdbut.Every = Every
907 StorageOptChooser.lbl.longB1 = <html>Store plottable values approximately this far apart.<br>
908 StorageOptChooser.lbl.longB2 = Larger values result in smaller files.
909 StorageOptChooser.lbl.seconds = seconds
910 StorageOptChooser.rdbut.Onlyprimfig = Only primary figures
911 StorageOptChooser.lbl.longC1 = <html>Store only the values shown in the summary table.<br>
912 StorageOptChooser.lbl.longC2 = This results in the smallest files.
913 StorageOptChooser.checkbox.Compfile = Compress file
914 StorageOptChooser.lbl.UsingComp = Using compression reduces the file size significantly.
915 StorageOptChooser.lbl.longD1 = An estimate on how large the resulting file would be with the present options.
916 StorageOptChooser.ttip.Saveopt = Save options
917 StorageOptChooser.lbl.Estfilesize = Estimated file size:
918 StorageOptChooser.lbl.Saveopt = Save options
920 ! ThrustCurveMotorSelectionPanel
921 TCMotorSelPan.lbl.Selrocketmotor = Select rocket motor:
922 TCMotorSelPan.checkbox.hideSimilar = Hide very similar thrust curves
923 TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Show all motors
924 TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Show motors with diameter less than that of the motor mount
925 TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Show motors with diameter equal to that of the motor mount
926 TCMotorSelPan.lbl.Motormountdia = Motor mount diameter:
927 TCMotorSelPan.lbl.Search = Search:
928 TCMotorSelPan.lbl.Selectthrustcurve = Select thrust curve:
929 TCMotorSelPan.lbl.Ejectionchargedelay = Ejection charge delay:
930 TCMotorSelPan.equalsIgnoreCase.None = None
931 TCMotorSelPan.lbl.NumberofsecondsorNone = (Number of seconds or \"None\")
932 TCMotorSelPan.lbl.Totalimpulse = Total impulse:
933 TCMotorSelPan.lbl.Avgthrust = Avg. thrust:
934 TCMotorSelPan.lbl.Maxthrust = Max. thrust:
935 TCMotorSelPan.lbl.Burntime = Burn time:
936 TCMotorSelPan.lbl.Launchmass = Launch mass:
937 TCMotorSelPan.lbl.Emptymass = Empty mass:
938 TCMotorSelPan.lbl.Datapoints = Data points:
939 TCMotorSelPan.lbl.Digest = Digest:
940 TCMotorSelPan.title.Thrustcurve = Thrust curve:
941 TCMotorSelPan.title.Thrust = Thrust
942 TCMotorSelPan.delayBox.None = None
946 PlotDialog.title.Flightdataplot = Flight data plot
947 PlotDialog.Chart.Simulatedflight = Simulated flight
948 PlotDialog.CheckBox.Showdatapoints = Show data points
949 PlotDialog.lbl.Chart = Click and drag down+right to zoom in, up+left to zoom out
952 ! "main" prefix is used for the main application dialog
954 # FIXME: Rename the description keys
956 main.menu.file = File
957 main.menu.file.desc = File-handling related tasks
958 main.menu.file.new = New
959 main.menu.file.new.desc = Create a new rocket design
960 main.menu.file.open = Open...
961 BasicFrame.item.Openrocketdesign = Open a rocket design
962 main.menu.file.openExample = Open example...
963 BasicFrame.item.Openexamplerocketdesign = Open an example rocket design
964 main.menu.file.save = Save
965 BasicFrame.item.SavecurRocketdesign = Save the current rocket design
966 main.menu.file.saveAs = Save as...
967 BasicFrame.item.SavecurRocketdesnewfile = Save the current rocket design to a new file
968 main.menu.file.print = Print / Export PDF...
969 main.menu.file.print.desc = Print or save as PDF the parts list and fin templates
970 main.menu.file.close = Close
971 BasicFrame.item.Closedesign = Close the current rocket design
972 main.menu.file.quit = Quit
973 BasicFrame.item.Quitprogram = Quit the program
975 main.menu.edit = Edit
976 BasicFrame.menu.Rocketedt = Rocket editing
977 main.menu.edit.undo = Undo
978 main.menu.edit.undo.desc = Undo the previous operation
979 main.menu.edit.redo = Redo
980 main.menu.edit.redo.desc = Redo the previously undone operation
981 main.menu.edit.cut = Cut
982 main.menu.edit.copy = Copy
983 main.menu.edit.paste = Paste
984 main.menu.edit.delete = Delete
985 main.menu.edit.resize = Scale...
986 main.menu.edit.resize.desc = Scale parts of the rocket design
987 main.menu.edit.preferences = Preferences
988 main.menu.edit.preferences.desc = Setup the application preferences
990 main.menu.analyze = Analyze
991 main.menu.analyze.desc = Rocket analysis
992 main.menu.analyze.componentAnalysis = Component analysis
993 main.menu.analyze.componentAnalysis.desc = Analyze the rocket components separately
994 main.menu.analyze.optimization = Rocket optimization
995 main.menu.analyze.optimization.desc = General rocket design optimization
997 main.menu.help = Help
998 main.menu.help.desc = Information about OpenRocket
999 main.menu.help.license = License
1000 main.menu.help.license.desc = OpenRocket license information
1001 main.menu.help.bugReport = Bug report
1002 main.menu.help.bugReport.desc = Information about reporting bugs in OpenRocket
1003 main.menu.help.debugLog = Debug log
1004 main.menu.help.debugLog.desc = View the OpenRocket debug log
1005 main.menu.help.about = About
1006 main.menu.help.about.desc = Copyright details about OpenRocket
1008 main.menu.debug = Debug
1009 main.menu.debug.whatisthismenu = What is this menu?
1010 main.menu.debug.createtestrocket = Create test rocket
1013 ! Translate here all material database
1018 Databases.materials.Acrylic = Acrylic
1019 Databases.materials.Balsa = Balsa
1020 Databases.materials.Birch = Birch
1021 Databases.materials.Cardboard = Cardboard
1022 Databases.materials.Carbonfiber = Carbon fiber
1023 Databases.materials.Cork = Cork
1024 Databases.materials.DepronXPS = Depron (XPS)
1025 Databases.materials.Fiberglass = Fiberglass
1026 Databases.materials.Kraftphenolic = Kraft phenolic
1027 Databases.materials.Maple = Maple
1028 Databases.materials.Paperoffice = Paper (office)
1029 Databases.materials.Pine = Pine
1030 Databases.materials.Plywoodbirch = Plywood (birch)
1031 Databases.materials.PolycarbonateLexan = Polycarbonate (Lexan)
1032 Databases.materials.Polystyrene = Polystyrene
1033 Databases.materials.PVC = PVC
1034 Databases.materials.Spruce = Spruce
1035 Databases.materials.StyrofoamgenericEPS = Styrofoam (generic EPS)
1036 Databases.materials.StyrofoamBluefoamXPS = Styrofoam \"Blue foam\" (XPS)
1037 Databases.materials.Quantumtubing = Quantum tubing
1038 Databases.materials.BlueTube = Blue tube
1040 Databases.materials.Ripstopnylon = Ripstop nylon
1041 Databases.materials.Mylar = Mylar
1042 Databases.materials.Polyethylenethin = Polyethylene (thin)
1043 Databases.materials.Polyethyleneheavy = Polyethylene (heavy)
1044 Databases.materials.Silk = Silk
1045 Databases.materials.Paperoffice = Paper (office)
1046 Databases.materials.Cellophane = Cellophane
1047 Databases.materials.Crepepaper = Cr\u00eape paper
1049 Databases.materials.Threadheavy-duty = Thread (heavy-duty)
1050 Databases.materials.Elasticcordround2mm = Elastic cord (round 2mm, 1/16 in)
1051 Databases.materials.Elasticcordflat6mm = Elastic cord (flat 6mm, 1/4 in)
1052 Databases.materials.Elasticcordflat12mm = Elastic cord (flat 12mm, 1/2 in)
1053 Databases.materials.Elasticcordflat19mm = Elastic cord (flat 19mm, 3/4 in)
1054 Databases.materials.Elasticcordflat25mm = Elastic cord (flat 25mm, 1 in)
1055 Databases.materials.Braidednylon2mm = Braided nylon (2 mm, 1/16 in)
1056 Databases.materials.Braidednylon3mm = Braided nylon (3 mm, 1/8 in)
1057 Databases.materials.Tubularnylon11mm = Tubular nylon (11 mm, 7/16 in)
1058 Databases.materials.Tubularnylon14mm = Tubular nylon (14 mm, 9/16 in)
1059 Databases.materials.Tubularnylon25mm = Tubular nylon (25 mm, 1 in)
1062 ExternalComponent.Rough = Rough
1063 ExternalComponent.Unfinished = Unfinished
1064 ExternalComponent.Regularpaint = Regular paint
1065 ExternalComponent.Smoothpaint = Smooth paint
1066 ExternalComponent.Polished = Polished
1069 LineStyle.Solid = Solid
1070 LineStyle.Dashed = Dashed
1071 LineStyle.Dotted = Dotted
1072 LineStyle.Dash-dotted = Dash-dotted
1073 LineStyle.Defaultstyle = Default style
1076 Shape.Conical = Conical
1077 Shape.Conical.desc1 = A conical nose cone has a profile of a triangle.
1078 Shape.Conical.desc2 = A conical transition has straight sides.
1080 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>.
1081 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>.
1082 Shape.Ellipsoid = Ellipsoid
1083 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>.
1084 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.
1085 Shape.Powerseries = Power series
1086 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.
1087 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>.
1088 Shape.Parabolicseries = Parabolic series
1089 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.
1090 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.
1091 Shape.Haackseries = Haack series
1092 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.
1093 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.
1097 RocketComponent.Position.TOP = Top of the parent component
1098 RocketComponent.Position.MIDDLE = Middle of the parent component
1099 RocketComponent.Position.BOTTOM = Bottom of the parent component
1100 RocketComponent.Position.AFTER = After the parent component
1101 RocketComponent.Position.ABSOLUTE = Tip of the nose cone
1104 LaunchLug.Launchlug = Launch lug
1106 NoseCone.NoseCone = Nose cone
1108 Transition.Transition = Transition
1112 BodyTube.BodyTube = Body tube
1114 TubeCoupler.TubeCoupler = Tube coupler
1116 InnerTube.InnerTube = Inner Tube
1118 TrapezoidFinSet.TrapezoidFinSet = Trapezoidal fin set
1120 FreeformFinSet.FreeformFinSet = Freeform fin set
1122 MassComponent.MassComponent = Mass component
1124 Parachute.Parachute = Parachute
1126 ShockCord.ShockCord = Shock cord
1128 Bulkhead.Bulkhead = Bulkhead
1131 Rocket.motorCount.Nomotor = [No motors]
1132 Rocket.compname.Rocket = Rocket
1135 MotorMount.IgnitionEvent.AUTOMATIC = Automatic (launch or ejection charge)
1136 MotorMount.IgnitionEvent.LAUNCH = Launch
1137 MotorMount.IgnitionEvent.EJECTION_CHARGE = First ejection charge of previous stage
1138 MotorMount.IgnitionEvent.BURNOUT = First burnout of previous stage
1139 MotorMount.IgnitionEvent.NEVER = Never
1142 ComponentIcons.Nosecone = Nose cone
1143 ComponentIcons.Bodytube = Body tube
1144 ComponentIcons.Transition = Transition
1145 ComponentIcons.Trapezoidalfinset = Trapezoidal fin set
1146 ComponentIcons.Ellipticalfinset = Elliptical fin set
1147 ComponentIcons.Freeformfinset = Freeform fin set
1148 ComponentIcons.Launchlug = Launch lug
1149 ComponentIcons.Innertube = Inner tube
1150 ComponentIcons.Tubecoupler = Tube coupler
1151 ComponentIcons.Centeringring = Centering ring
1152 ComponentIcons.Bulkhead = Bulk head
1153 ComponentIcons.Engineblock = Engine block
1154 ComponentIcons.Parachute = Parachute
1155 ComponentIcons.Streamer = Streamer
1156 ComponentIcons.Shockcord = Shock cord
1157 ComponentIcons.Masscomponent = Mass component
1158 ComponentIcons.disabled = (disabled)
1161 StageAction.Stage = Stage
1164 RecoveryDevice.DeployEvent.LAUNCH = Launch (plus NN seconds)
1165 RecoveryDevice.DeployEvent.EJECTION = First ejection charge of this stage
1166 RecoveryDevice.DeployEvent.APOGEE = Apogee
1167 RecoveryDevice.DeployEvent.ALTITUDE = Specific altitude during descent
1168 RecoveryDevice.DeployEvent.NEVER = Never
1171 FlightEvent.Type.LAUNCH = Launch
1172 FlightEvent.Type.IGNITION = Motor ignition
1173 FlightEvent.Type.LIFTOFF = Lift-off
1174 FlightEvent.Type.LAUNCHROD = Launch rod clearance
1175 FlightEvent.Type.BURNOUT = Motor burnout
1176 FlightEvent.Type.EJECTION_CHARGE = Ejection charge
1177 FlightEvent.Type.STAGE_SEPARATION = Stage separation
1178 FlightEvent.Type.APOGEE = Apogee
1179 FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Recovery device deployment
1180 FlightEvent.Type.GROUND_HIT = Ground hit
1181 FlightEvent.Type.SIMULATION_END = Simulation end
1182 FlightEvent.Type.ALTITUDE = Altitude change
1184 ! ThrustCurveMotorColumns
1185 TCurveMotorCol.MANUFACTURER = Manufacturer
1186 TCurveMotorCol.DESIGNATION = Designation
1187 TCurveMotorCol.TYPE = Type
1188 TCurveMotorCol.DIAMETER = Diameter
1189 TCurveMotorCol.LENGTH = Length
1192 RocketInfo.lengthLine.Length = Length
1193 RocketInfo.lengthLine.maxdiameter = , max. diameter
1194 RocketInfo.massText1 = Mass with motors
1195 RocketInfo.massText2 = Mass with no motors
1196 RocketInfo.at = at M=
1197 RocketInfo.cgText = CG:
1198 RocketInfo.cpText = CP:
1199 RocketInfo.stabText = Stability:
1200 RocketInfo.Warning = Warning:
1201 RocketInfo.Calculating = Calculating...
1202 RocketInfo.Apogee = Apogee:
1203 RocketInfo.Maxvelocity = Max. velocity:
1204 RocketInfo.Maxacceleration = Max. acceleration:
1205 RocketInfo.apogeeValue = N/A
1206 RocketInfo.Mach = (Mach
1207 RocketInfo.velocityValue = N/A
1208 RocketInfo.accelerationValue = N/A
1211 FinSet.CrossSection.SQUARE = Square
1212 FinSet.CrossSection.ROUNDED = Rounded
1213 FinSet.CrossSection.AIRFOIL = Airfoil
1214 FinSet.TabRelativePosition.FRONT = Root chord leading edge
1215 FinSet.TabRelativePosition.CENTER = Root chord midpoint
1216 FinSet.TabRelativePosition.END = Root chord trailing edge
1219 FlightDataType.TYPE_TIME = Time
1220 FlightDataType.TYPE_ALTITUDE = Altitude
1221 FlightDataType.TYPE_VELOCITY_Z = Vertical velocity
1222 FlightDataType.TYPE_ACCELERATION_Z = Vertical acceleration
1223 FlightDataType.TYPE_VELOCITY_TOTAL = Total velocity
1224 FlightDataType.TYPE_ACCELERATION_TOTAL = Total acceleration
1225 FlightDataType.TYPE_POSITION_X = Position upwind
1226 FlightDataType.TYPE_POSITION_Y = Position parallel to wind
1227 FlightDataType.TYPE_POSITION_XY = Lateral distance
1228 FlightDataType.TYPE_POSITION_DIRECTION = Lateral direction
1229 FlightDataType.TYPE_VELOCITY_XY = Lateral velocity
1230 FlightDataType.TYPE_ACCELERATION_XY = Lateral acceleration
1231 FlightDataType.TYPE_AOA = Angle of attack
1232 FlightDataType.TYPE_ROLL_RATE = Roll rate
1233 FlightDataType.TYPE_PITCH_RATE = Pitch rate
1234 FlightDataType.TYPE_YAW_RATE = Yaw rate
1235 FlightDataType.TYPE_MASS = Mass
1236 FlightDataType.TYPE_LONGITUDINAL_INERTIA = Longitudinal moment of inertia
1237 FlightDataType.TYPE_ROTATIONAL_INERTIA = Rotational moment of inertia
1238 FlightDataType.TYPE_CP_LOCATION = CP location
1239 FlightDataType.TYPE_CG_LOCATION = CG location
1240 FlightDataType.TYPE_STABILITY = Stability margin calibers
1241 FlightDataType.TYPE_MACH_NUMBER = Mach number
1242 FlightDataType.TYPE_REYNOLDS_NUMBER = Reynolds number
1243 FlightDataType.TYPE_THRUST_FORCE = Thrust
1244 FlightDataType.TYPE_DRAG_FORCE = Drag force
1245 FlightDataType.TYPE_DRAG_COEFF = Drag coefficient
1246 FlightDataType.TYPE_AXIAL_DRAG_COEFF = Axial drag coefficient
1247 FlightDataType.TYPE_FRICTION_DRAG_COEFF = Friction drag coefficient
1248 FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Pressure drag coefficient
1249 FlightDataType.TYPE_BASE_DRAG_COEFF = Base drag coefficient
1250 FlightDataType.TYPE_NORMAL_FORCE_COEFF = Normal force coefficient
1251 FlightDataType.TYPE_PITCH_MOMENT_COEFF = Pitch moment coefficient
1252 FlightDataType.TYPE_YAW_MOMENT_COEFF = Yaw moment coefficient
1253 FlightDataType.TYPE_SIDE_FORCE_COEFF = Side force coefficient
1254 FlightDataType.TYPE_ROLL_MOMENT_COEFF = Roll moment coefficient
1255 FlightDataType.TYPE_ROLL_FORCING_COEFF = Roll forcing coefficient
1256 FlightDataType.TYPE_ROLL_DAMPING_COEFF = Roll damping coefficient
1257 FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Pitch damping coefficient
1258 FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Yaw damping coefficient
1259 FlightDataType.TYPE_REFERENCE_LENGTH = Reference lenght
1260 FlightDataType.TYPE_REFERENCE_AREA = Reference area
1261 FlightDataType.TYPE_ORIENTATION_THETA = Vertical orientation (zenith)
1262 FlightDataType.TYPE_ORIENTATION_PHI = Lateral orientation (azimuth)
1263 FlightDataType.TYPE_WIND_VELOCITY = Wind velocity
1264 FlightDataType.TYPE_AIR_TEMPERATURE = Air temperature
1265 FlightDataType.TYPE_AIR_PRESSURE = Air pressure
1266 FlightDataType.TYPE_SPEED_OF_SOUND = Speed of sound
1267 FlightDataType.TYPE_TIME_STEP = Simulation time step
1268 FlightDataType.TYPE_COMPUTATION_TIME = Computation time
1269 FlightDataType.TYPE_LATITUDE = Latitude
1270 FlightDataType.TYPE_LONGITUDE = Longitude
1271 FlightDataType.TYPE_CORIOLIS_ACCELERATION = Coriolis acceleration
1274 PlotConfiguration.Verticalmotion = Vertical motion vs. time
1275 PlotConfiguration.Totalmotion = Total motion vs. time
1276 PlotConfiguration.Flightside = Flight side profile
1277 PlotConfiguration.Stability = Stability vs. time
1278 PlotConfiguration.Dragcoef = Drag coefficients vs. Mach number
1279 PlotConfiguration.Rollcharacteristics = Roll characteristics
1280 PlotConfiguration.Angleofattack = Angle of attack and orientation vs. time
1281 PlotConfiguration.Simulationtime = Simulation time step and computation time
1284 Warning.LargeAOA.str1 = Large angle of attack encountered.
1285 Warning.LargeAOA.str2 = Large angle of attack encountered (
1286 Warning.DISCONTINUITY = Discontinuity in rocket body diameter.
1287 Warning.THICK_FIN = Thick fins may not be modeled accurately.
1288 Warning.JAGGED_EDGED_FIN = Jagged-edged fin predictions may be inaccurate.
1289 Warning.LISTENERS_AFFECTED = Listeners modified the flight simulation
1290 Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Recovery device opened while motor still burning.
1291 Warning.FILE_INVALID_PARAMETER = Invalid parameter encountered, ignoring.
1295 ScaleDialog.lbl.scaleRocket = Entire rocket
1296 ScaleDialog.lbl.scaleSubselection = Selection and all subcomponents
1297 ScaleDialog.lbl.scaleSelection = Only selected component
1298 ScaleDialog.title = Scale design
1299 ScaleDialog.lbl.scale = Scale:
1300 ScaleDialog.lbl.scale.ttip = Select whether to scale the entire design or only the selected component
1301 ScaleDialog.lbl.scaling = Scaling to apply:
1302 ScaleDialog.lbl.scaling.ttip = Resulting size, values above 100% grow and values below 100% shrink the design.
1303 ! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"
1304 ScaleDialog.lbl.scaleFrom = Scale from
1305 ScaleDialog.lbl.scaleTo = to
1306 ScaleDialog.lbl.scaleFromTo.ttip = Define the scaling based on an original and resulting length.
1307 ScaleDialog.checkbox.scaleMass = Update explicit mass values
1308 ScaleDialog.checkbox.scaleMass.ttip = Scale mass component and override mass values by the cube of the scaling factor
1309 ScaleDialog.button.scale = Scale
1310 ScaleDialog.undo.scaleRocket = Scale rocket
1311 ScaleDialog.undo.scaleComponent = Scale component
1312 ScaleDialog.undo.scaleComponents = Scale components
1318 OpenRocketPrintable.Partsdetail = Parts detail
1319 OpenRocketPrintable.Fintemplates = Fin templates
1320 OpenRocketPrintable.DesignReport = Design Report
1322 OpenRocketDocument.Redo = Redo
1323 OpenRocketDocument.Undo = Undo
1326 EllipticalFinSet.Ellipticalfinset = Elliptical fin set
1332 optimization.modifier.nosecone.length = Length
1333 optimization.modifier.nosecone.length.desc = Optimize the nose cone length.
1334 optimization.modifier.nosecone.diameter = Diameter
1335 optimization.modifier.nosecone.diameter.desc = Optimize the nose cone base diameter.
1336 optimization.modifier.nosecone.thickness = Thickness
1337 optimization.modifier.nosecone.thickness.desc = Optimize the nose cone wall thickness.
1338 optimization.modifier.nosecone.shapeparameter = Shape parameter
1339 optimization.modifier.nosecone.shapeparameter.desc = Optimize the nose cone shape parameter.
1341 optimization.modifier.transition.length = Length
1342 optimization.modifier.transition.length.desc = Optimize the transition length.
1343 optimization.modifier.transition.forediameter = Fore diameter
1344 optimization.modifier.transition.forediameter.desc = Optimize the transition fore diameter.
1345 optimization.modifier.transition.aftdiameter = Aft diameter
1346 optimization.modifier.transition.aftdiameter.desc = Optimize the transition aft diameter.
1347 optimization.modifier.transition.thickness = Thickness
1348 optimization.modifier.transition.thickness.desc = Optimize the transition wall thickness.
1349 optimization.modifier.transition.shapeparameter = Shape parameter
1350 optimization.modifier.transition.shapeparameter.desc = Optimize the transition shape parameter.
1352 optimization.modifier.bodytube.length = Length
1353 optimization.modifier.bodytube.length.desc = Optimize the body tube length.
1354 optimization.modifier.bodytube.outerDiameter = Outer diameter
1355 optimization.modifier.bodytube.outerDiameter.desc = Optimize the body tube outer diameter while maintaining the wall thickness.
1356 optimization.modifier.bodytube.thickness = Thickness
1357 optimization.modifier.bodytube.thickness.desc = Optimize the body tube wall thickness.
1359 optimization.modifier.trapezoidfinset.rootChord = Root chord
1360 optimization.modifier.trapezoidfinset.rootChord.desc = Optimize the root chord length of the fin set (length of fin at the rocket body).
1361 optimization.modifier.trapezoidfinset.tipChord = Tip chord
1362 optimization.modifier.trapezoidfinset.tipChord.desc = Optimize the tip chord length of the fin set (length of fin at outer edge).
1363 optimization.modifier.trapezoidfinset.sweep = Sweep
1364 optimization.modifier.trapezoidfinset.sweep.desc = Optimize the sweep of the fin set (distance that the leading edge sweeps backwards).
1365 optimization.modifier.trapezoidfinset.height = Height
1366 optimization.modifier.trapezoidfinset.height.desc = Optimize the height (semi-span) of the fin set.
1368 optimization.modifier.ellipticalfinset.length = Root chord
1369 optimization.modifier.ellipticalfinset.length.desc = Optimize the root chord length of the fin set.
1370 optimization.modifier.ellipticalfinset.height = Height
1371 optimization.modifier.ellipticalfinset.height.desc = Optimize the height (semi-span) of the fin set.
1373 optimization.modifier.finset.cant = Cant angle
1374 optimization.modifier.finset.cant.desc = Optimize the cant angle of the fin set.
1375 optimization.modifier.finset.position = Position
1376 optimization.modifier.finset.position.desc = Optimize the fin set position along the rocket body.
1378 optimization.modifier.launchlug.length = Length
1379 optimization.modifier.launchlug.length.desc = Optimize the launch lug length.
1380 optimization.modifier.launchlug.outerDiameter = Outer diameter
1381 optimization.modifier.launchlug.outerDiameter.desc = Optimize the outer diameter of the launch lug.
1382 optimization.modifier.launchlug.thickness = Thickness
1383 optimization.modifier.launchlug.thickness.desc = Optimize the launch lug thickness while keeping the outer diameter constant.
1384 optimization.modifier.launchlug.position = Position
1385 optimization.modifier.launchlug.position.desc = Optimize the launch lug position along the rocket body.
1388 optimization.modifier.internalcomponent.position = Position
1389 optimization.modifier.internalcomponent.position.desc = Optimize the position of the component relative to the parent component.
1391 optimization.modifier.masscomponent.mass = Mass
1392 optimization.modifier.masscomponent.mass.desc = Optimize the mass of the mass component.
1394 optimization.modifier.parachute.diameter = Diameter
1395 optimization.modifier.parachute.diameter.desc = Optimize the parachute canopy diameter.
1396 optimization.modifier.parachute.coefficient = Drag coefficient
1397 optimization.modifier.parachute.coefficient.desc = Optimize the drag coefficient of the parachute. Typical parachutes have a drag coefficient of about 0.8.
1399 optimization.modifier.streamer.length = Length
1400 optimization.modifier.streamer.length.desc = Optimize the length of the streamer.
1401 optimization.modifier.streamer.width = Width
1402 optimization.modifier.streamer.width.desc = Optimize the width of the streamer.
1403 optimization.modifier.streamer.aspectRatio = Aspect ratio
1404 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.
1405 optimization.modifier.streamer.coefficient = Drag coefficient
1406 optimization.modifier.streamer.coefficient.desc = Optimize the drag coefficient of the streamer.
1408 optimization.modifier.recoverydevice.deployDelay = Deployment delay
1409 optimization.modifier.recoverydevice.deployDelay.desc = Optimize the deployment delay of the recovery device.
1410 optimization.modifier.recoverydevice.deployAltitude = Deployment altitude
1411 optimization.modifier.recoverydevice.deployAltitude.desc = Optimize the deployment altitude of the recovery device.
1413 optimization.modifier.rocketcomponent.overrideMass = Override mass
1414 optimization.modifier.rocketcomponent.overrideMass.desc = Optimize the overridden mass of the component.
1415 optimization.modifier.rocketcomponent.overrideCG = Override CG
1416 optimization.modifier.rocketcomponent.overrideCG.desc = Optimize the overridden center of gravity of the component.
1418 optimization.modifier.motormount.overhang = Motor overhang
1419 optimization.modifier.motormount.overhang.desc = Optimize the motor overhang.
1420 optimization.modifier.motormount.delay = Motor ignition delay
1421 optimization.modifier.motormount.delay.desc = Optimize the motor ignition delay.
1426 ! General rocket design optimization dialog
1428 GeneralOptimizationDialog.title = Rocket optimization
1429 GeneralOptimizationDialog.goal.maximize = Maximize value
1430 GeneralOptimizationDialog.goal.minimize = Minimize value
1431 GeneralOptimizationDialog.goal.seek = Seek value of
1432 GeneralOptimizationDialog.btn.start = Start optimization
1433 GeneralOptimizationDialog.btn.stop = Stop optimization
1434 GeneralOptimizationDialog.lbl.paramsToOptimize = Parameters to optimize:
1435 GeneralOptimizationDialog.btn.add = Add
1436 GeneralOptimizationDialog.btn.add.ttip = Add the selected parameter to the optimization
1437 GeneralOptimizationDialog.btn.remove = Remove
1438 GeneralOptimizationDialog.btn.remove.ttip = Remove the selected parameter from the optimization
1439 GeneralOptimizationDialog.btn.removeAll = Remove all
1440 GeneralOptimizationDialog.btn.removeAll.ttip = Remove all parameters from the optimization
1441 GeneralOptimizationDialog.lbl.availableParams = Available parameters:
1442 GeneralOptimizationDialog.lbl.optimizationOpts = Optimization options
1443 GeneralOptimizationDialog.lbl.optimizeSim = Optimize simulation:
1444 GeneralOptimizationDialog.lbl.optimizeSim.ttip = Select which simulation to optimize
1445 GeneralOptimizationDialog.lbl.optimizeValue = Optimized value:
1446 GeneralOptimizationDialog.lbl.optimizeValue.ttip = Select what value is to be optimized
1447 GeneralOptimizationDialog.lbl.optimizeGoal = Optimization goal:
1448 GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Select the goal of the optimization
1449 GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Custom value to seek
1450 GeneralOptimizationDialog.lbl.requireStability = Required stability
1451 GeneralOptimizationDialog.lbl.requireMinStability = Minimum stability:
1452 GeneralOptimizationDialog.lbl.requireMinStability.ttip = Require a minimum static stability margin for the design
1453 GeneralOptimizationDialog.lbl.requireMaxStability = Maximum stability:
1454 GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Require a maximum static stability margin for the design
1455 GeneralOptimizationDialog.status.bestValue = Best value:
1456 GeneralOptimizationDialog.status.bestValue.ttip = Best optimization value found so far.
1457 GeneralOptimizationDialog.status.stepCount = Step count:
1458 GeneralOptimizationDialog.status.stepCount.ttip = Number of optimization steps that have been performed.
1459 GeneralOptimizationDialog.status.evalCount = Evaluations:
1460 GeneralOptimizationDialog.status.evalCount.ttip = Total number of function evaluations (simulations) that have been performed.
1461 GeneralOptimizationDialog.status.stepSize = Step size:
1462 GeneralOptimizationDialog.status.stepSize.ttip = Current optimization step size (relative to the optimization parameter ranges)
1463 GeneralOptimizationDialog.btn.plotPath = Plot path
1464 GeneralOptimizationDialog.btn.plotPath.ttip = Plot the optimization path (one and two dimensional optimization only)
1465 GeneralOptimizationDialog.btn.save = Save path
1466 GeneralOptimizationDialog.btn.save.ttip = Save the results of the function evaluations (simulations) as a CSV file.
1467 GeneralOptimizationDialog.btn.apply = Apply optimization
1468 GeneralOptimizationDialog.btn.apply.ttip = Apply the optimization results to the rocket design
1469 GeneralOptimizationDialog.btn.reset = Reset
1470 GeneralOptimizationDialog.btn.reset.ttip = Reset the rocket design to the current rocket design
1471 GeneralOptimizationDialog.btn.close = Close
1472 GeneralOptimizationDialog.btn.close.ttip = Close the dialog without modifying the rocket design
1473 GeneralOptimizationDialog.error.selectParams.text = First select some parameters to optimize from the available parameters.
1474 GeneralOptimizationDialog.error.selectParams.title = Select optimization parameters
1475 GeneralOptimizationDialog.error.optimizationFailure.text = The optimization failed to run:
1476 GeneralOptimizationDialog.error.optimizationFailure.title = Optimization failed
1477 GeneralOptimizationDialog.undoText = Apply optimization
1478 GeneralOptimizationDialog.basicSimulationName = Basic simulation
1479 GeneralOptimizationDialog.noSimulationName = No simulation
1480 GeneralOptimizationDialog.table.col.parameter = Parameter
1481 GeneralOptimizationDialog.table.col.current = Current
1482 GeneralOptimizationDialog.table.col.min = Minimum
1483 GeneralOptimizationDialog.table.col.max = Maximum
1484 GeneralOptimizationDialog.export.header = Include header line
1485 GeneralOptimizationDialog.export.header.ttip = Include a header line as the first line containing the field descriptions.
1486 GeneralOptimizationDialog.export.stability = Stability
1489 ! Dialog for plotting optimization results
1490 OptimizationPlotDialog.title = Optimization results
1491 OptimizationPlotDialog.lbl.zoomInstructions = Click and drag down+right to zoom in, up+left to zoom out
1492 OptimizationPlotDialog.plot1d.title = Optimization result
1493 OptimizationPlotDialog.plot1d.series = Optimization result
1494 OptimizationPlotDialog.plot2d.title = Optimization path
1495 OptimizationPlotDialog.plot2d.path = Optimization path
1496 OptimizationPlotDialog.plot2d.evals = Evaluations
1497 OptimizationPlotDialog.plot.ttip.stability = Stability:
1498 OptimizationPlotDialog.plot.label.optimum = Optimum
1500 ! Optimization parameters
1501 MaximumAltitudeParameter.name = Apogee altitude
1502 MaximumVelocityParameter.name = Maximum velocity
1503 MaximumAccelerationParameter.name = Maximum acceleration
1504 StabilityParameter.name = Stability
1505 GroundHitVelocityParameter.name = Ground hit speed
1506 LandingDistanceParameter.name = Landing distance
1507 TotalFlightTimeParameter.name = Total flight time
1508 DeploymentVelocityParameter.name = Velocity at parachute deployment
1511 ! Compass directions drawn on a compass rose.
1512 CompassRose.lbl.north = N
1513 CompassRose.lbl.east = E
1514 CompassRose.lbl.south = S
1515 CompassRose.lbl.west = W
1517 ! Compass directions with subdirections. These might not be localized even if the directions on the compass rose are.
1518 CompassSelectionButton.lbl.N = N
1519 CompassSelectionButton.lbl.NE = NE
1520 CompassSelectionButton.lbl.E = E
1521 CompassSelectionButton.lbl.SE = SE
1522 CompassSelectionButton.lbl.S = S
1523 CompassSelectionButton.lbl.SW = SW
1524 CompassSelectionButton.lbl.W = W
1525 CompassSelectionButton.lbl.NW = NW
projects / debian / openrocket / blob