--- /dev/null
+## English base translation file\r
+## Should you need to add new logical keys here is the proposed method\r
+## 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)debug.currentFile = essages.properties! RocketActionsRocketActions.checkbox.Donotaskmeagain = źćśłóńęąRocketActions.lbl.Youcanchangedefop = źćśłóńęąRocketActions.showConfirmDialog.lbl1 = źćśłóńęąRocketActions.showConfirmDialog.lbl2 = <html><i>Tego nie można cofnąć!</i>RocketActions.showConfirmDialog.title = źćśłóńęąRocketActions.DelCompAct.Delete = źćśłóńęąRocketActions.DelCompAct.ttip.Delete = źćśłóńęąRocketActions.DelSimuAct.Delete = źćśłóńęąRocketActions.DelSimuAct.ttip.Delete = źćśłóńęąRocketActions.DelAct.Delete = źćśłóńęąRocketActions.DelAct.ttip.Delete = źćśłóńęąRocketActions.CutAction.Cut = źćśłóńęąRocketActions.CutAction.ttip.Cut = źćśłóńęąRocketActions.CopyAct.Copy = źćśłóńęą\r
+RocketActions.CopyAct.ttip.Copy = źćśłóńęą\r
+RocketActions.PasteAct.Paste = źćśłóńęą\r
+RocketActions.PasteAct.ttip.Paste = źćśłóńęą\r
+RocketActions.EditAct.Edit = źćśłóńęą\r
+RocketActions.EditAct.ttip.Edit = źćśłóńęą\r
+RocketActions.NewStageAct.Newstage = źćśłóńęą\r
+RocketActions.NewStageAct.ttip.Newstage = źćśłóńęą\r
+RocketActions.ActBoosterstage = źćśłóńęą\r
+RocketActions.MoveUpAct.Moveup = źćśłóńęą\r
+RocketActions.MoveUpAct.ttip.Moveup = źćśłóńęą\r
+RocketActions.MoveDownAct.Movedown = źćśłóńęą\r
+RocketActions.MoveDownAct.ttip.Movedown = źćśłóńęą\r
+! RocketPanelRocketPanel.FigTypeAct.Sideview = źćśłóńęąRocket\r
+Panel.FigTypeAct.ttip.Sideview = źćśłóńęą\r
+RocketPanel.FigTypeAct.Backview = źćśłóńęą\r
+RocketPanel.FigTypeAct.ttip.Backview = źćśłóńęą\r
+RocketPanel.FigViewAct.2D = źćśłóńęą\r
+RocketPanel.FigViewAct.ttip.2D = źćśłóńęą\r
+RocketPanel.FigViewAct.3D = źćśłóńęą\r
+RocketPanel.FigViewAct.ttip.3D = źćśłóńęą\r
+RocketPanel.lbl.Motorcfg = źćśłóńęą\r
+RocketPanel.lbl.infoMessage " <html>Click to select Shift+click to select ożźćśłóńęąr Double-click to edit Click+drag to move"! BasicFrameBasicFrame.tab.Rocketdesign = źćśłóńęąBasicFrame.tab.Flightsim = źćśłóńęąBasicFrame.title.Addnewcomp = źćśłóńęąBasicFrame.dlg.lbl1 = źćśłóńęąBasicFrame.dlg.lbl2 = źćśłóńęąBasicFrame.dlg.lbl3 = źćśłóńęąBasicFrame.dlg.title = źćśłóńęąBasicFrame.StageName.Sustainer = źćśłóńęąBasicFrame.WarningDialog.txt1 = źćśłóńęąBasicFrame.WarningDialog.txt2 = źćśłóńęąBasicFrame.WarningDialog.title = źćśłóńęą! General error messages used in multiple contextserror.fileExists.title = źćśłóńęąerror.fileExists.desc = ile '{filename}' exists. Do you want to overwrite it?error.writing.title = źćśłóńęąerror.writing.desc = źćśłóńęą! Labels used in buttons of dialog windows"# TODO: Rename these to ""btn.xxx"""button.ok = źćśłóńęąbutton.cancel = źćśłóńęąbutton.close = źćśłóńęą! Common labels used in buttons of dialog windowsdlg.but.ok = źćśłóńęądlg.but.cancel = źćśłóńęądlg.but.close = źćśłóńęą! General file type namesfiletypes.pdf = źćśłóńęąBasicFrame.SimpleFileFilter1 = źćśłóńęąBasicFrame.SimpleFileFilter2 = źćśłóńęąBasicFrame.SimpleFileFilter3 = źćśłóńęąBasicFrame.SimpleFileFilter4 = źćśłóńęąfiletypes.images = źćśłóńęą! About DialogAboutDialog.lbl.version = źćśłóńęą! 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 = źćśłóńęąAboutDialog.lbl.translator AboutDialog.lbl.translatorWebsite AboutDialog.lbl.translatorIcon ! Print dialogPrintDialog.title = źćśłóńęąPrintDialog.but.previewAndPrint = źćśłóńęąPrintDialog.checkbox.showByStage = źćśłóńęąPrintDialog.lbl.selectElements = źćśłóńęąprintdlg.but.saveaspdf = źćśłóńęąprintdlg.but.preview = źćśłóńęąprintdlg.but.settings = źćśłóńęąPrintDialog.error.preview.title = źćśłóńęąPrintDialog.error.preview.desc1 = źćśłóńęąPrintDialog.error.preview.desc2 = źćśłóńęą!PrintSettingsDialogPrintSettingsDialog.title = źćśłóńęąPrintSettingsDialog.lbl.Templatefillcolor = źćśłóńęąPrintSettingsDialog.lbl.Templatebordercolor = źćśłóńęąPrintSettingsDialog.lbl.Papersize = źćśłóńęąPrintSettingsDialog.lbl.Paperorientation = źćśłóńęąPrintSettingsDialog.but.Reset = źćśłóńęąPrintSettingsDialog.but.Close = źćśłóńęą! Bug Report dialogbugreport.dlg.title = źćśłóńęąbugreport.dlg.but.Sendbugreport = źćśłóńęąbugreport.dlg.but.Sendbugreport.Ttip = źćśłóńęąbugreport.dlg.successmsg1 = źćśłóńęąbugreport.dlg.successmsg2 = źćśłóńęąbugreport.dlg.successmsg3 = źćśłóńęąbugreport.dlg.connectedInternet = <html>If connected to żźćśłóńęą Internet, you can simply click <em>Send bug report</em>.bugreport.dlg.otherwise = żźćśłóńęąrwise, send żźćśłóńęą text below to żźćśłóńęą address:bugreport.lbl.Theinformation = źćśłóńęą information above may be included in żźćśłóńęą public bug report. Make sure it does not contain any sensitive information you do not want to be made public.bugreport.dlg.failedmsg1 = penRocket was unable to send żźćśłóńęą bug report:bugreport.dlg.failedmsg2 = lease send żźćśłóńęą report manually tobugreport.dlg.failedmsg3 = rror sending reportbugreport.reportDialog.txt = <html><b>You can report żźćśłóńęą bug in OpenRocket by filling in and submitting żźćśłóńęą form below.</b><br>You can also report bugs and include attachments on żźćśłóńęą project web site.bugreport.reportDialog.txt2 = <html><b>Please includeżźćśłóńęąshort description about what you were doing when żźćśłóńęą exception occurred.</b>bugreport.dlg.provideDescription = lease provideżźćśłóńęądescription of żźćśłóńęą bug first.bugreport.dlg.provideDescription.title = ug description missing! Debug log dialogdebuglogdlg.but.clear = leardebuglogdlg.OpenRocketdebuglog = penRocket debug logdebuglogdlg.Displayloglines = isplay log lines:debuglogdlg.Follow = ollowdebuglogdlg.col.Time = imedebuglogdlg.col.Level = eveldebuglogdlg.col.Location = ocationdebuglogdlg.col.Message = essagedebuglogdlg.lbl.Loglinenbr = og line number:debuglogdlg.lbl.Time = ime:debuglogdlg.lbl.Level = evel:debuglogdlg.lbl.Location = ocation:debuglogdlg.lbl.Logmessage = og message:debuglogdlg.lbl.Stacktrace = tack trace:! Edit Motor configuration dialogedtmotorconfdlg.but.removemotor = emove motoredtmotorconfdlg.but.Selectmotor = elect motoredtmotorconfdlg.but.Removeconfiguration = emove configurationedtmotorconfdlg.but.Newconfiguration = ew configurationedtmotorconfdlg.lbl.Motormounts = <html><b>Motor mounts:</b>edtmotorconfdlg.title.Editmotorconf = dit motor configurationsedtmotorconfdlg.selectcomp = <html>Select which components function as motor mounts:edtmotorconfdlg.lbl.Motorconfig = <html><b>Motor configurations:</b>edtmotorconfdlg.lbl.Configname = onfiguration name:edtmotorconfdlg.lbl.Leavenamedefault = eave name empty for default.! Example design dialogexdesigndlg.but.open = penexdesigndlg.lbl.Selectexample = elect example designs to open:exdesigndlg.lbl.Openexampledesign = pen example designexdesigndlg.lbl.Exampledesignsnotfound = xample designs could not be found.exdesigndlg.lbl.Examplesnotfound = xamples not found! Material edit panelmatedtpan.but.new = ewmatedtpan.but.edit = ditmatedtpan.but.delete = eletematedtpan.but.revertall = evert allmatedtpan.col.Material = aterialmatedtpan.col.Type = ypematedtpan.col.Density = ensitymatedtpan.col.but.ttip.New = ddżźćśłóńęąnew materialmatedtpan.title.Addcustmaterial = ddżźćśłóńęącustom materialmatedtpan.but.ttip.edit = dit an existing materialmatedtpan.title.Editmaterial = dit materialmatedtpan.title2.Editmaterial = źćśłóńęą built-in materials cannot be modified.matedtpan.but.ttip.delete = elete żźćśłóńęą user-defined materialmatedtpan.but.ttip.revertall = elete all user-defined materialsmatedtpan.title.Deletealluser-defined = elete all user-defined materials?matedtpan.title.Revertall = evert all?matedtpan.lbl.edtmaterials = diting materials will not affect existing rocket designs.!MaterialModelMaterialModel.title.Material = aterialMaterialModel.title.Defcustmat = efine custom material! Preference dialogpref.dlg.but.add = ddpref.dlg.but.reset = esetpref.dlg.but.checknow = heck nowpref.dlg.but.defaultmetric = efault metricpref.dlg.but.defaultimperial = efault imperialpref.dlg.title.Preferences = referencespref.dlg.tab.Units = nitspref.dlg.tab.Defaultunits = efault unitspref.dlg.tab.Materials = aterialspref.dlg.tab.Custommaterials = ustom materialspref.dlg.tab.Options = ptionspref.dlg.tab.Miscellaneousoptions = iscellaneous optionspref.dlg.lbl.Positiontoinsert = osition to insert new body components:pref.dlg.lbl.Confirmdeletion = onfirm deletion of simulations:pref.dlg.lbl.User-definedthrust = ser-defined thrust curves:pref.dlg.lbl.Windspeed = ind speedpref.dlg.Allthrustcurvefiles " All thrust curve files (*.eng; *.rse; *.zip; directories)"pref.dlg.RASPfiles = ASP motor files (*.eng)pref.dlg.RockSimfiles = ockSim engine files (*.rse)pref.dlg.ZIParchives = IP archives (*.zip)pref.dlg.checkbox.Checkupdates = heck for software updates at startuppref.dlg.ttip.Checkupdatesnow = heck for software updates nowpref.dlg.lbl.Selectprefunits = elect your preferred units:pref.dlg.lbl.Rocketdimensions = ocket dimensions:pref.dlg.lbl.Linedensity = ine density:pref.dlg.lbl.Motordimensions = otor dimensions:pref.dlg.lbl.Surfacedensity = urface density:pref.dlg.lbl.Distance = istance:pref.dlg.lbl.Bulkdensity = ulk density:pref.dlg.lbl.Velocity = elocity:pref.dlg.lbl.Surfaceroughness = urface roughness:pref.dlg.lbl.Acceleration = cceleration:pref.dlg.lbl.Area = rea:pref.dlg.lbl.Mass = ass:pref.dlg.lbl.Angle = ngle:pref.dlg.lbl.Force = orce:pref.dlg.lbl.Rollrate = oll rate:pref.dlg.lbl.Totalimpulse = otal impulse:pref.dlg.lbl.Temperature = emperature:pref.dlg.lbl.Momentofinertia = oment of inertia:pref.dlg.lbl.Pressure = ressure:pref.dlg.lbl.Stability = tability:pref.dlg.lbl.FlightTime = light time:pref.dlg.lbl.effect1 = źćśłóńęą effects will take place żźćśłóńęą next time you open żźćśłóńęą window.pref.dlg.lbl.Checkingupdates = hecking for updates...pref.dlg.lbl.msg1 = n error occurred while communicating with żźćśłóńęą server.pref.dlg.lbl.msg2 = nable to retrieve update informationpref.dlg.lbl.msg3 = ou are running żźćśłóńęą latest version of OpenRocket.pref.dlg.lbl.msg4 = o updates availablepref.dlg.PrefChoiseSelector1 = lways askpref.dlg.PrefChoiseSelector2 = nsert in middlepref.dlg.PrefChoiseSelector3 = dd to endpref.dlg.PrefBooleanSelector1 = eletepref.dlg.PrefBooleanSelector2 = onfirmpref.dlg.Add = ddpref.dlg.DescriptionArea.Adddirectories " Add directories, RASP motor files (*.eng), RockSim engine files (*.rse) or ZIP archives separated by żźćśłóńęą semicolon (;) to load external thrust curves. Changes will take effect żźćśłóńęą next time you start OpenRocket."PreferencesDialog.lbl.language = nterface language:PreferencesDialog.languages.default = ystem defaultPreferencesDialog.lbl.languageEffect = źćśłóńęą language will change żźćśłóńęą next time you start OpenRocket.! Simulation edit dialogsimedtdlg.but.runsimulation = un simulationsimedtdlg.but.resettodefault = eset to defaultsimedtdlg.but.add = ddsimedtdlg.but.remove = emovesimedtdlg.title.Editsim = dit simulationsimedtdlg.lbl.Simname = imulation name:simedtdlg.tab.Launchcond = aunch conditionssimedtdlg.tab.Simopt = imulation optionssimedtdlg.tab.Plotdata = lot datasimedtdlg.tab.Exportdata = xport datasimedtdlg.lbl.Motorcfg = otor configuration:simedtdlg.lbl.ttip.Motorcfg = elect żźćśłóńęą motor configuration to use.simedtdlg.combo.ttip.motorconf = elect żźćśłóńęą motor configuration to use.simedtdlg.lbl.Wind = indsimedtdlg.lbl.Averwindspeed = verage windspeed:simedtdlg.lbl.ttip.Averwindspeed = źćśłóńęą average windspeed relative to żźćśłóńęą ground.simedtdlg.lbl.Stddeviation = tandard deviation:simedtdlg.lbl.ttip.Stddeviation = <html>żźćśłóńęą standard deviation of żźćśłóńęą windspeed.<br>żźćśłóńęą windspeed is within twice żźćśłóńęą standard deviation from żźćśłóńęą average for 95% of żźćśłóńęą time.simedtdlg.lbl.Turbulenceintensity = urbulence intensity:simedtdlg.lbl.ttip.Turbulenceintensity1 = <html>żźćśłóńęą turbulence intensity is żźćśłóńęą standard deviation divided by żźćśłóńęą average windspeed.<br>simedtdlg.lbl.ttip.Turbulenceintensity2 = ypical values range fromsimedtdlg.lbl.ttip.Turbulenceintensity3 = osimedtdlg.border.Atmoscond = tmospheric conditionssimedtdlg.checkbox.InterStdAtmosphere = se International Standard Atmospheresimedtdlg.checkbox.ttip.InterStdAtmosphere1 = <html>Select to use żźćśłóńęą International Standard Atmosphere model.<br>This model has żźćśłóńęą temperature ofsimedtdlg.checkbox.ttip.InterStdAtmosphere2 = nd żźćśłóńęą pressure ofsimedtdlg.checkbox.ttip.InterStdAtmosphere3 = t sea level.simedtdlg.lbl.Temperature = emperature:simedtdlg.lbl.ttip.Temperature = źćśłóńęą temperature at żźćśłóńęą launch site.simedtdlg.lbl.Pressure = ressure:simedtdlg.lbl.ttip.Pressure = źćśłóńęą atmospheric pressure at żźćśłóńęą launch site.simedtdlg.lbl.Launchsite = aunch sitesimedtdlg.lbl.Latitude = atitude:simedtdlg.lbl.ttip.Latitude = <html>żźćśłóńęą launch site latitude affects żźćśłóńęą gravitational pull of Earth.<br>Positive values are on żźćśłóńęą Norżźćśłóńęąrn hemisphere, negative values on żźćśłóńęą Soużźćśłóńęąrn hemisphere.simedtdlg.lbl.Longitude = ongitude:simedtdlg.lbl.ttip.Longitude = <html>Required for weażźćśłóńęąr prediction and elevation models.simedtdlg.lbl.Altitude = ltitude:simedtdlg.lbl.ttip.Altitude = <html>żźćśłóńęą launch altitude above mean sea level.<br>This affects żźćśłóńęą position of żźćśłóńęą rocket in żźćśłóńęą atmospheric model.simedtdlg.border.Launchrod = aunch rodsimedtdlg.lbl.Length = ength:simedtdlg.lbl.ttip.Length = źćśłóńęą length of żźćśłóńęą launch rod.simedtdlg.lbl.Angle = ngle:simedtdlg.lbl.ttip.Angle = źćśłóńęą angle of żźćśłóńęą launch rod from vertical.simedtdlg.lbl.Direction = irection:simedtdlg.lbl.ttip.Direction1 = <html>Direction of żźćśłóńęą launch rod relative to żźćśłóńęą wind.<br>simedtdlg.lbl.ttip.Direction2 = owards the wind,simedtdlg.lbl.ttip.Direction3 = ownwind.simedtdlg.border.Simopt = imulator optionssimedtdlg.lbl.Calcmethod = alculation method:simedtdlg.lbl.ttip.Calcmethod = <html>żźćśłóńęą Extended Barrowman method calculates aerodynamic forces according <br>to żźćśłóńęą Barrowman equations extended to accommodate more components.simedtdlg.lbl.ExtBarrowman = xtended Barrowmansimedtdlg.lbl.Simmethod = imulation method:simedtdlg.lbl.ttip.Simmethod1 = <html>żźćśłóńęą six degree-of-freedom simulator allows żźćśłóńęą rocket total freedom during flight.<br>simedtdlg.lbl.ttip.Simmethod2 = ntegration is performed using żźćśłóńęą 4<sup>th</sup> order Runge-Kutta 4 numerical integration.simedtdlg.lbl.GeodeticMethod = eodetic calculations:simedtdlg.lbl.ttip.GeodeticMethodTip = elate to żźćśłóńęą calculation of coordinates on żźćśłóńęą earth. This also enables coriolis effect computations.simedtdlg.lbl.Timestep = ime step:simedtdlg.lbl.ttip.Timestep1 = <html>żźćśłóńęą time between simulation steps.<br>A smaller time step results in żźćśłóńęą more accurate but slower simulation.<br>simedtdlg.lbl.ttip.Timestep2 = źćśłóńęą 4<sup>th</sup> order simulation method is quite accurate with żźćśłóńęą time step ofsimedtdlg.but.ttip.resettodefault = eset żźćśłóńęą time step to its default value (simedtdlg.border.Simlist = imulator listenerssimedtdlg.txt.longA1 = <html><i>Simulation listeners</i> is an advanced feature that allows user-written code to listen to and interact with żźćśłóńęą simulation.simedtdlg.txt.longA2 = or details on writing simulation listeners, see żźćśłóńęą OpenRocket technical documentation.simedtdlg.lbl.Curlist = urrent listeners:simedtdlg.lbl.Addsimlist = dd simulation listenersimedtdlg.lbl.Noflightdata = o flight data available.simedtdlg.lbl.runsimfirst = lease run żźćśłóńęą simulation first.simedtdlg.chart.Simflight = imulated flightsimedtdlg.dlg.Simres = imulation resultssimedtdlg.IntensityDesc.None = onesimedtdlg.IntensityDesc.Verylow = ery lowsimedtdlg.IntensityDesc.Low = owsimedtdlg.IntensityDesc.Medium = ediumsimedtdlg.IntensityDesc.High = ighsimedtdlg.IntensityDesc.Veryhigh = ery highsimedtdlg.IntensityDesc.Extreme = xtremeGeodeticComputationStrategy.flat.name = lat EarthGeodeticComputationStrategy.flat.desc = erform computations with żźćśłóńęą flat Earth approximation. Sufficient for low-altitude flights.GeodeticComputationStrategy.spherical.name = pherical approximationGeodeticComputationStrategy.spherical.desc = <html>Perform geodetic computations assuming żźćśłóńęą spherical Earth.<br>This is sufficiently accurate for almost all purposes.GeodeticComputationStrategy.wgs84.name = GS84 ellipsoidGeodeticComputationStrategy.wgs84.desc = <html>Perform geodetic computations on żźćśłóńęą WGS84 reference ellipsoid using Vincenty's method.<br>Slower and unnecessary in most cases.! Simulation Panelsimpanel.but.newsimulation = ew simulationsimpanel.but.editsimulation = dit simulationsimpanel.but.runsimulations = un simulationssimpanel.but.deletesimulations = elete simulationssimpanel.but.plotexport = lot / exportsimpanel.but.ttip.newsimulation = dd żźćśłóńęą new simulationsimpanel.but.ttip.editsim = dit żźćśłóńęą selected simulationsimpanel.but.ttip.runsimu = e-run żźćśłóńęą selected simulationssimpanel.but.ttip.deletesim = elete żźćśłóńęą selected simulationssimpanel.checkbox.donotask = o not ask me againsimpanel.lbl.defpref = ou can change żźćśłóńęą default operation in żźćśłóńęą preferences.simpanel.dlg.lbl.DeleteSim1 = elete żźćśłóńęą selected simulations?simpanel.dlg.lbl.DeleteSim2 = <html><i>This operation cannot be undone.</i>simpanel.dlg.lbl.DeleteSim3 = elete simulationssimpanel.col.Name = amesimpanel.col.Motors = otorssimpanel.col.Velocityoffrod = elocity off rodsimpanel.col.Velocityatdeploy = elocity at deploymentsimpanel.col.Apogee = pogeesimpanel.col.Maxvelocity = ax. velocitysimpanel.col.Maxacceleration = ax. accelerationsimpanel.col.Timetoapogee = ime to apogeesimpanel.col.Flighttime = light timesimpanel.col.Groundhitvelocity = round hit velocity! SimulationRunDialogSimuRunDlg.title.RunSim = unning simulations...SimuRunDlg.lbl.Running = unning ...SimuRunDlg.lbl.Simutime = imulation time:SimuRunDlg.lbl.Altitude = ltitude:SimuRunDlg.lbl.Velocity = elocity:SimuRunDlg.msg.Unabletosim = nable to simulate:SimuRunDlg.msg.errorOccurred = n error occurred during żźćśłóńęą simulation:SimuRunDlg.msg.AnException1 = n exception occurred during żźćśłóńęą simulation:SimuRunDlg.msg.AnException2 = lease report this as żźćśłóńęą bug along with żźćśłóńęą details below.SimuRunDlg.msg.AssertionError1 = źćśłóńęą computation error occurred during żźćśłóńęą simulation.SimuRunDlg.msg.AssertionError2 = lease report this as żźćśłóńęą bug along with żźćśłóńęą details below.SimuRunDlg.msg.unknownerror1 = n unknown error was encountered during żźćśłóńęą simulation.SimuRunDlg.msg.unknownerror2 = źćśłóńęą program may be unstable, you should save all your designs and restart OpenRocket now!RK4SimulationStepper.error.valuesTooLarge = imulation values exceeded limits. Try selecting żźćśłóńęą shorter time step.! SimulationExportPanelSimExpPan.desc = omma Separated Files (*.csv)SimExpPan.border.Vartoexport = ariables to exportSimExpPan.but.Selectall = elect allSimExpPan.but.Selectnone = elect noneSimExpPan.border.Fieldsep = ield separatorSimExpPan.lbl.Fieldsepstr = ield separator string:SimExpPan.lbl.longA1 = <html>żźćśłóńęą string used to separate żźćśłóńęą fields in żźćśłóńęą exported file.<br>SimExpPan.lbl.longA2 = se ',' for żźćśłóńęą Comma Separated Values (CSV) file.SimExpPan.checkbox.Includesimudesc = nclude simulation descriptionSimExpPan.checkbox.ttip.Includesimudesc = nclude żźćśłóńęą comment at żźćśłóńęą beginning of żźćśłóńęą file describing żźćśłóńęą simulation.SimExpPan.border.Comments = ommentsSimExpPan.checkbox.Includefielddesc = nclude field descriptionsSimExpPan.checkbox.ttip.Includefielddesc = nclude żźćśłóńęą comment line with żźćśłóńęą descriptions of żźćśłóńęą exported variables.SimExpPan.checkbox.Incflightevents = nclude flight eventsSimExpPan.checkbox.ttip.Incflightevents = nclude żźćśłóńęą comment line for every flight event.SimExpPan.lbl.Commentchar = omment character:SimExpPan.lbl.ttip.Commentchar = źćśłóńęą character(s) that mark żźćśłóńęą comment line.SimExpPan.but.Exporttofile = xport to file...SimExpPan.Fileexists.desc1 " File \"""SimExpPan.Fileexists.desc2 " \"" exists. Overwrite?"SimExpPan.Fileexists.title = ile existsSimExpPan.ExportingVar.desc1 = xporting 1 variable out ofSimExpPan.ExportingVar.desc2 = xportingSimExpPan.ExportingVar.desc3 = ariables out ofSimExpPan.Col.Variable = ariableSimExpPan.Col.Unit = nitCsvOptionPanel.separator.space = PACECsvOptionPanel.separator.tab = AB! MotorPlotMotorPlot.title.Motorplot = otor plotMotorPlot.but.Select = electMotorPlot.Chart.Motorthrustcurve = otor thrust curveMotorPlot.Chart.Time = ime / sMotorPlot.Chart.Thrust = hrust / NMotorPlot.txt.Designation = esignation:MotorPlot.txt.Manufacturer = anufacturer:MotorPlot.txt.Type = ype:MotorPlot.txt.Delays = elays:MotorPlot.txt.Comment = omment:\n! Simulation plot panelsimplotpanel.lbl.Presetplotconf = reset plot configurations:simplotpanel.lbl.Xaxistype = axis type:simplotpanel.lbl.Unit = nit:simplotpanel.lbl.Yaxistypes = axis types:simplotpanel.lbl.Flightevents = light events:simplotpanel.but.All = llsimplotpanel.but.None = onesimplotpanel.but.NewYaxisplottype = ew Y axis plot typesimplotpanel.but.Plotflight = lot flightsimplotpanel.lbl.Axis = xis:simplotpanel.but.ttip.Removethisplot = emove this plotsimplotpanel.Desc = źćśłóńęą data will be plotted in time order even if żźćśłóńęą X axis type is not time.simplotpanel.OptionPane.lbl1 = źćśłóńęą maximum of 15 plots is allowed.simplotpanel.OptionPane.lbl2 = annot add plotsimplotpanel.AUTO_NAME = utosimplotpanel.LEFT_NAME = eftsimplotpanel.RIGHT_NAME = ightsimplotpanel.CUSTOM = ustomSimulationPlotPanel.error.noPlotSelected = lease add one or more variables to plot on żźćśłóńęą Y-axis.SimulationPlotPanel.error.noPlotSelected.title = othing to plot! Component add buttonscompaddbuttons.Bodycompandfinsets = ody components and fin setscompaddbuttons.Nosecone = ose conecompaddbuttons.Bodytube = ody tubecompaddbuttons.Transition = ransitioncompaddbuttons.Trapezoidal = rapezoidalcompaddbuttons.Elliptical = llipticalcompaddbuttons.Freeform = reeformcompaddbuttons.Launchlug = aunch lugcompaddbuttons.Innercomponent = nner componentcompaddbuttons.Innertube = nner tubecompaddbuttons.Coupler = ouplercompaddbuttons.Centeringring = entering\nringcompaddbuttons.Bulkhead = ulkheadcompaddbuttons.Engineblock = ngine\nblockcompaddbuttons.Massobjects = ass objectscompaddbuttons.Parachute = arachutecompaddbuttons.Streamer = treamercompaddbuttons.Shockcord = hock cordcompaddbuttons.Masscomponent = ass\ncomponentcompaddbuttons.Donotaskmeagain = o not ask me againcompaddbuttons.Selectcomppos = elect component positioncompaddbuttons.lbl.Youcanchange = ou can change żźćśłóńęą default operation in żźćśłóńęą preferences.compaddbuttons.lbl.insertcomp = nsert żźćśłóńęą component after żźćśłóńęą current component or as żźćśłóńęą last component?compaddbuttons.askPosition.Inserthere = nsert herecompaddbuttons.askPosition.Addtotheend = dd to żźćśłóńęą endcompaddbuttons.askPosition.Cancel = ancel! Component Analysis Dialogcomponentanalysisdlg.componentanalysis = omponent analysiscomponentanalysisdlg.lbl.winddir = ind direction:componentanalysisdlg.TitledBorder.warnings = arnings:componentanalysisdlg.ToggleBut.worst = orstcomponentanalysisdlg.lbl.angleofattack = ngle of attack:componentanalysisdlg.lbl.machnumber = ach number:componentanalysisdlg.lbl.rollrate = oll rate:componentanalysisdlg.lbl.activestages = ctive stages:componentanalysisdlg.lbl.motorconf = otor configuration:componentanalysisdlg.TabStability.Col = omponentcomponentanalysisdlg.TabStability = tabilitycomponentanalysisdlg.TabStability.ttip = tability informationcomponentanalysisdlg.dragTableModel.Col.Component = omponentcomponentanalysisdlg.dragTableModel.Col.Pressure = <html>Pressure C<sub>D</sub>componentanalysisdlg.dragTableModel.Col.Base = <html>Base C<sub>D</sub>componentanalysisdlg.dragTableModel.Col.friction = <html>Friction C<sub>D</sub>componentanalysisdlg.dragTableModel.Col.total = <html>Total C<sub>D</sub>componentanalysisdlg.dragTabchar = rag characteristicscomponentanalysisdlg.dragTabchar.ttip = rag characteristicscomponentanalysisdlg.rollTableModel.Col.component = omponentcomponentanalysisdlg.rollTableModel.Col.rollforc = oll forcing coefficientcomponentanalysisdlg.rollTableModel.Col.rolldamp = oll damping coefficientcomponentanalysisdlg.rollTableModel.Col.total = <html>Total C<sub>l</sub>componentanalysisdlg.rollTableModel = oll dynamicscomponentanalysisdlg.rollTableModel.ttip = oll dynamicscomponentanalysisdlg.println.closingmethod = losing method called:componentanalysisdlg.println.settingnam = ETTING NAN VALUEScomponentanalysisdlg.lbl.reflenght = eference length:componentanalysisdlg.lbl.refarea = eference area:!componentanalysisdlg.But.close = losecomponentanalysisdlg.TabStability.Col.Component = omponent! Custom Material dialogcustmatdlg.title.Custommaterial = ustom materialcustmatdlg.lbl.Materialname = aterial name:custmatdlg.lbl.Materialtype = aterial type:custmatdlg.lbl.Materialdensity = aterial density:custmatdlg.checkbox.Addmaterial = dd material to database! Ring Component Configringcompcfg.OuterRadius = uterRadiusringcompcfg.Automatic = utomaticringcompcfg.InnerRadius = nnerRadiusringcompcfg.Thickness = hicknessringcompcfg.Length = engthringcompcfg.Positionrelativeto = osition relative to:ringcompcfg.plus = lusringcompcfg.PositionValue = ositionValueringcompcfg.Radialdistance = adial distance:ringcompcfg.Distancefrom = istance from żźćśłóńęą rocket centerlineringcompcfg.Radialdirection = adial direction:ringcompcfg.radialdirectionfrom = źćśłóńęą radial direction from żźćśłóńęą rocket centerlineringcompcfg.but.Reset = esetringcompcfg.but.Resetcomponant = eset żźćśłóńęą component to żźćśłóńęą rocket centerlineringcompcfg.EngineBlock.desc = <html>An <b>engine block</b> stops żźćśłóńęą motor from moving forwards in żźćśłóńęą motor mount tube.<br><br>In order to add żźćśłóńęą motor, create żźćśłóńęą <b>body tube</b> or <b>inner tube</b> and mark it as żźćśłóńęą motor mount in żźćśłóńęą <em>Motor</em> tab.ringcompcfg.note.desc = ote: An inner tube will not affect żźćśłóńęą aerodynamics of żźćśłóńęą rocket even if it is located outside of żźćśłóńęą body tube.! Body Tube ConfigBodyTubecfg.lbl.Bodytubelength = ody tube length:BodyTubecfg.lbl.Outerdiameter = uter diameter:BodyTubecfg.lbl.Innerdiameter = nner diameter:BodyTubecfg.lbl.Wallthickness = all thickness:BodyTubecfg.tab.General = eneralBodyTubecfg.tab.Generalproperties = eneral propertiesBodyTubecfg.tab.Motor = otorBodyTubecfg.tab.Motormountconf = otor mount configurationBodyTubecfg.checkbox.Automatic = utomaticBodyTubecfg.checkbox.Filled = illed! FinSetConfigFinSetConfig.tab.Fintabs = in tabsFinSetConfig.tab.Through-the-wall = hrough-żźćśłóńęą-wall fin tabsFinSetConfig.but.Converttofreeform = onvert to freeformFinSetConfig.but.Converttofreeform.ttip = onvert this fin set into żźćśłóńęą freeform fin setFinSetConfig.Convertfinset = onvert fin setFinSetConfig.but.Splitfins = plit finsFinSetConfig.but.Splitfins.ttip = plit żźćśłóńęą fin set into separate finsFinSetConfig.but.AutoCalc = alculate automaticallyFinSetConfig.lbl.Through-the-wall = hrough-żźćśłóńęą-wall fin tabs:FinSetConfig.lbl.Tablength = ab length:FinSetConfig.ttip.Tablength = źćśłóńęą length of żźćśłóńęą fin tab.FinSetConfig.lbl.Tabheight = ab height:FinSetConfig.ttip.Tabheight = źćśłóńęą spanwise height of żźćśłóńęą fin tab.FinSetConfig.lbl.Tabposition = ab position:FinSetConfig.ttip.Tabposition = źćśłóńęą position of żźćśłóńęą fin tab.FinSetConfig.lbl.relativeto = elative to!FinMarkingGuideFinMarkingGuide.lbl.Front = ront! MotorDatabaseLoadingDialogMotorDbLoadDlg.title = oading motorsMotorDbLoadDlg.Loadingmotors = oading motors...! RocketConfigRocketCfg.lbl.Designname = esign name:RocketCfg.lbl.Designer = esigner:RocketCfg.lbl.Comments = omments:RocketCfg.lbl.Revisionhistory = evision history:RocketCfg.lbl.Material = aterial:! ShockCordConfigShockCordCfg.lbl.Shockcordlength = hock cord length:! RocketComponentConfigRocketCompCfg.lbl.Componentname = omponent name:RocketCompCfg.ttip.Thecomponentname = źćśłóńęą component name.RocketCompCfg.tab.Override = verrideRocketCompCfg.tab.MassandCGoverride = ass and CG override optionsRocketCompCfg.tab.Figure = igureRocketCompCfg.tab.Figstyleopt = igure style optionsRocketCompCfg.tab.Comment = ommentRocketCompCfg.tab.Specifyacomment = pecify żźćśłóńęą comment for żźćśłóńęą componentRocketCompCfg.lbl.Mass = ass:RocketCompCfg.lbl.Componentmass = omponent mass:RocketCompCfg.lbl.overriddento (overridden toRocketCompCfg.lbl.overriddenby (overridden byRocketCompCfg.lbl.Componentmaterial = omponent material:RocketCompCfg.lbl.Componentfinish = omponent finish:RocketCompCfg.lbl.ttip.componentmaterialaffects = źćśłóńęą component material affects żźćśłóńęą weight of żźćśłóńęą component.RocketCompCfg.combo.ttip.componentmaterialaffects = źćśłóńęą component material affects żźćśłóńęą weight of żźćśłóńęą component.RocketCompCfg.lbl.longA1 = <html>żźćśłóńęą component finish affects żźćśłóńęą aerodynamic drag of żźćśłóńęą component.<br>RocketCompCfg.lbl.longA2 = źćśłóńęą value indicated is żźćśłóńęą average roughness height of żźćśłóńęą surface.RocketCompCfg.but.Setforall = et for allRocketCompCfg.but.ttip.Setforall = et this finish for all components of żźćśłóńęą rocket.RocketCompCfg.lbl.Overridemassorcenter = verride żźćśłóńęą mass or center of gravity of żźćśłóńęąRocketCompCfg.checkbox.Overridemass = verride mass:RocketCompCfg.checkbox.Overridecenterofgrav = verride center of gravity:RocketCompCfg.checkbox.OverridemassandCG = verride mass and CG of all subcomponentsRocketCompCfg.lbl.longB1 = <html>żźćśłóńęą overridden mass does not include motors.<br>RocketCompCfg.lbl.longB2 = źćśłóńęą center of gravity is measured from żźćśłóńęą front end of żźćśłóńęąRocketCompCfg.lbl.Commentsonthe = omments on żźćśłóńęąRocketCompCfg.lbl.Figurestyle = igure style:RocketCompCfg.lbl.Componentcolor = omponent color:RocketCompCfg.lbl.Choosecolor = hoose colorRocketCompCfg.checkbox.Usedefaultcolor = se default colorRocketCompCfg.lbl.Complinestyle = omponent line style:RocketCompCfg.but.Saveasdefstyle = ave as default styleRocketCompCfg.lbl.Diameter = iameter:RocketCompCfg.lbl.Length = ength:RocketCompCfg.lbl.Thickness = hickness:RocketCompCfg.checkbox.Endcapped = nd cappedRocketCompCfg.ttip.Endcapped = heżźćśłóńęąr żźćśłóńęą end of żźćśłóńęą shoulder is capped.RocketCompCfg.title.Noseconeshoulder = ose cone shoulderRocketCompCfg.title.Aftshoulder = ft shoulderRocketCompCfg.border.Foreshoulder = ore shoulder!RocketCompCfg.lbl.Length = ength:! BulkheadConfigBulkheadCfg.tab.Diameter = iameter:BulkheadCfg.tab.Thickness = hickness:BulkheadCfg.tab.General = eneralBulkheadCfg.tab.Generalproperties = eneral properties!CenteringRingConfigCenteringRingCfg.tab.Outerdiam = uter diameter:CenteringRingCfg.tab.Innerdiam = nner diameter:CenteringRingCfg.tab.Thickness = hickness:CenteringRingCfg.tab.General = eneralCenteringRingCfg.tab.Generalproperties = eneral properties!ComponentConfigDialogComponentCfgDlg.configuration = onfigurationComponentCfgDlg.configuration1 ComponentCfgDlg.Modify = odify!StageConfigStageConfig.tab.Separation = eparationStageConfig.tab.Separation.ttip = tage separation optionsStageConfig.separation.lbl.title = elect when this stage separates:StageConfig.separation.lbl.plus = lusStageConfig.separation.lbl.seconds = econds!EllipticalFinSetConfigEllipticalFinSetCfg.Nbroffins = umber of fins:EllipticalFinSetCfg.Rotation = otation:EllipticalFinSetCfg.Fincant = in cant:EllipticalFinSetCfg.Rootchord = oot chord:EllipticalFinSetCfg.Height = eight:EllipticalFinSetCfg.Positionrelativeto = osition relative to:EllipticalFinSetCfg.plus = lusEllipticalFinSetCfg.FincrossSection = in cross section:EllipticalFinSetCfg.Thickness = hickness:EllipticalFinSetCfg.General = eneralEllipticalFinSetCfg.Generalproperties = eneral propertiesEllipticalFinSetCfg.ttip.Fincant = źćśłóńęą angle that żźćśłóńęą fins are canted with respect to żźćśłóńęą rocket body.!FreeformFinSetConfigFreeformFinSetCfg.tab.General = eneralFreeformFinSetCfg.tab.ttip.General = eneral propertiesFreeformFinSetCfg.tab.Shape = hapeFreeformFinSetCfg.tab.ttip.Finshape = in shapeFreeformFinSetCfg.lbl.Numberoffins = umber of fins:FreeformFinSetCfg.lbl.Finrotation = in rotation:FreeformFinSetCfg.lbl.Fincant = in cant:FreeformFinSetCfg.lbl.ttip.Fincant = źćśłóńęą angle that żźćśłóńęą fins are canted with respect to żźćśłóńęą rocket body.FreeformFinSetCfg.lbl.Posrelativeto = osition relative to:FreeformFinSetCfg.lbl.plus = lusFreeformFinSetCfg.lbl.FincrossSection = in cross section:FreeformFinSetCfg.lbl.Thickness = hickness:"! doubleClick1 + 2 form the message ""Double-click to edit"", split approximately at the middle"FreeformFinSetConfig.lbl.doubleClick1 = ouble-clickFreeformFinSetConfig.lbl.doubleClick2 = o editFreeformFinSetConfig.lbl.clickDrag = lick+drag: Add and move pointsFreeformFinSetConfig.lbl.ctrlClick = trl+click: Remove pointFreeformFinSetConfig.lbl.scaleFin = cale Fin!InnerTubeConfigInnerTubeCfg.tab.Motor = otorInnerTubeCfg.tab.ttip.Motor = otor mount configurationInnerTubeCfg.tab.Cluster = lusterInnerTubeCfg.tab.ttip.Cluster = luster configurationInnerTubeCfg.tab.Radialpos = adial positionInnerTubeCfg.tab.ttip.Radialpos = adial positionInnerTubeCfg.lbl.Selectclustercfg = elect cluster configuration:InnerTubeCfg.lbl.TubeSep = ube separation:InnerTubeCfg.lbl.ttip.TubeSep = źćśłóńęą separation of żźćśłóńęą tubes, 1.0 = ouching each otherInnerTubeCfg.lbl.Rotation = otation:InnerTubeCfg.lbl.ttip.Rotation = otation angle of żźćśłóńęą cluster configurationInnerTubeCfg.lbl.Rotangle = otation angle of żźćśłóńęą cluster configurationInnerTubeCfg.but.Splitcluster = plit clusterInnerTubeCfg.lbl.longA1 = <html>Split żźćśłóńęą cluster into separate components.<br>InnerTubeCfg.lbl.longA2 = his also duplicates all components attached to this inner tube.InnerTubeCfg.but.Resetsettings = eset settingsInnerTubeCfg.but.ttip.Resetsettings = eset żźćśłóńęą separation and rotation to żźćśłóńęą default values! LaunchLugConfigLaunchLugCfg.lbl.Length = ength:LaunchLugCfg.lbl.Outerdiam = uter diameter:LaunchLugCfg.lbl.Innerdiam = nner diameter:LaunchLugCfg.lbl.Thickness = hickness:LaunchLugCfg.lbl.Radialpos = adial position:LaunchLugCfg.lbl.Posrelativeto = osition relative to:LaunchLugCfg.lbl.plus = lusLaunchLugCfg.tab.General = eneralLaunchLugCfg.tab.Generalprop = eneral properties! MassComponentConfigMassComponentCfg.lbl.Mass = ass:MassComponentCfg.lbl.Length = ength:MassComponentCfg.lbl.Diameter = iameter:MassComponentCfg.lbl.PosRelativeto = osition relative to:MassComponentCfg.lbl.plus = lusMassComponentCfg.tab.General = eneralMassComponentCfg.tab.ttip.General = eneral propertiesMassComponentCfg.tab.Radialpos = adial positionMassComponentCfg.tab.ttip.Radialpos = adial position configurationMassComponentCfg.lbl.Radialdistance = adial distance:MassComponentCfg.lbl.Radialdirection = adial direction:MassComponentCfg.but.Reset = eset! MotorConfigMotorCfg.checkbox.compmotormount = his component is żźćśłóńęą motor mountMotorCfg.lbl.Motorcfg = otor configuration:MotorCfg.but.New = ewMotorCfg.lbl.Currentmotor = urrent motor:MotorCfg.lbl.Motoroverhang = otor overhang:MotorCfg.lbl.Ignitionat = gnition at:MotorCfg.lbl.plus = lusMotorCfg.lbl.seconds = econdsMotorCfg.lbl.longA1 = źćśłóńęą current design has only one stage.MotorCfg.lbl.longA2 " Stages can be added by clicking \""New stage\""."MotorCfg.lbl.longB1 = źćśłóńęą current design hasMotorCfg.lbl.longB2 = tages.MotorCfg.but.Selectmotor = elect motorMotorCfg.but.Removemotor = emove motorMotorCfg.lbl.motorLabel = one! NoseConeConfigNoseConeCfg.lbl.Noseconeshape = ose cone shape:NoseConeCfg.lbl.Shapeparam = hape parameter:NoseConeCfg.lbl.Noseconelength = ose cone length:NoseConeCfg.lbl.Basediam = ase diameter:NoseConeCfg.checkbox.Automatic = utomaticNoseConeCfg.lbl.Wallthickness = all thickness:NoseConeCfg.checkbox.Filled = illedNoseConeCfg.tab.General = eneralNoseConeCfg.tab.ttip.General = eneral propertiesNoseConeCfg.tab.Shoulder = houlderNoseConeCfg.tab.ttip.Shoulder = houlder properties! ParachuteConfigParachuteCfg.lbl.Canopy = anopy:ParachuteCfg.lbl.Diameter = iameter:ParachuteCfg.lbl.Material = aterial:ParachuteCfg.combo.MaterialModel = źćśłóńęą component material affects żźćśłóńęą weight of żźćśłóńęą component.ParachuteCfg.lbl.longA1 = <html>Drag coefficient C<sub>D</sub>:ParachuteCfg.lbl.longB1 = <html>żźćśłóńęą drag coefficient relative to żźćśłóńęą total area of żźćśłóńęą parachute.<br>ParachuteCfg.lbl.longB2 = źćśłóńęą larger drag coefficient yields żźćśłóńęą slowed descent rate.ParachuteCfg.lbl.longB3 = źćśłóńęą typical value for parachutes is 0.8.ParachuteCfg.but.Reset = esetParachuteCfg.lbl.Shroudlines = hroud lines:ParachuteCfg.lbl.Numberoflines = umber of lines:ParachuteCfg.lbl.Linelength = ine length:ParachuteCfg.lbl.Material = aterial:ParachuteCfg.lbl.Posrelativeto = osition relative to:ParachuteCfg.lbl.plus = lusParachuteCfg.lbl.Packedlength = acked length:ParachuteCfg.lbl.Packeddiam = acked diameter:ParachuteCfg.lbl.Deploysat = eploys at:ParachuteCfg.lbl.seconds = econdsParachuteCfg.lbl.Altitude = ltitude:ParachuteCfg.tab.General = eneralParachuteCfg.tab.ttip.General = eneral propertiesParachuteCfg.tab.Radialpos = adial positionParachuteCfg.tab.ttip.Radialpos = adial position configurationParachuteCfg.lbl.Radialdistance = adial distance:ParachuteCfg.lbl.Radialdirection = adial direction:ParachuteCfg.but.Reset = esetParachuteCfg.lbl.plusdelay = lus! ShockCordConfigShockCordCfg.lbl.Shockcordlength = hock cord length:ShockCordCfg.lbl.Shockcordmaterial = hock cord material:ShockCordCfg.lbl.Posrelativeto = osition relative to:ShockCordCfg.lbl.plus = lusShockCordCfg.lbl.Packedlength = acked length:ShockCordCfg.lbl.Packeddiam = acked diameter:ShockCordCfg.tab.General = eneralShockCordCfg.tab.ttip.General = eneral properties!SleeveConfigSleeveCfg.tab.Outerdiam = uter diameter:SleeveCfg.tab.Innerdiam = nner diameter:SleeveCfg.tab.Wallthickness = all thickness:SleeveCfg.tab.Length = ength:SleeveCfg.tab.General = eneralSleeveCfg.tab.Generalproperties = eneral properties! StreamerConfigStreamerCfg.lbl.Striplength = trip length:StreamerCfg.lbl.Stripwidth = trip width:StreamerCfg.lbl.Striparea = trip area:StreamerCfg.lbl.Aspectratio = spect ratio:StreamerCfg.lbl.Material = aterial:StreamerCfg.combo.ttip.MaterialModel = źćśłóńęą component material affects żźćśłóńęą weight of żźćśłóńęą component.StreamerCfg.lbl.longA1 = <html>Drag coefficient C<sub>D</sub>:StreamerCfg.lbl.longB1 = <html>żźćśłóńęą drag coefficient relative to żźćśłóńęą total area of żźćśłóńęą streamer.<br>StreamerCfg.lbl.longB2 = źćśłóńęą larger drag coefficient yields żźćśłóńęą slowed descent rate.StreamerCfg.lbl.Automatic = utomaticStreamerCfg.lbl.longC1 = źćśłóńęą drag coefficient is relative to żźćśłóńęą area of żźćśłóńęą streamer.StreamerCfg.lbl.Posrelativeto = osition relative to:StreamerCfg.lbl.plus = lusStreamerCfg.lbl.Packedlength = acked length:StreamerCfg.lbl.Packeddiam = acked diameter:StreamerCfg.lbl.Deploysat = eploys at:StreamerCfg.lbl.seconds = econdsStreamerCfg.lbl.Altitude = ltitude:StreamerCfg.tab.General = eneralStreamerCfg.tab.ttip.General = eneral propertiesStreamerCfg.tab.Radialpos = adial positionStreamerCfg.tab.ttip.Radialpos = adial position configurationStreamerCfg.lbl.Radialdistance = adial distance:StreamerCfg.lbl.Radialdirection = adial direction:StreamerCfg.but.Reset = esetStreamerCfg.lbl.plusdelay = lus! ThicknessRingComponentConfigThicknessRingCompCfg.tab.Outerdiam = uter diameter:ThicknessRingCompCfg.tab.Innerdiam = nner diameter:ThicknessRingCompCfg.tab.Wallthickness = all thickness:ThicknessRingCompCfg.tab.Length = ength:ThicknessRingCompCfg.tab.General = eneralThicknessRingCompCfg.tab.Generalprop = eneral properties! TransitionConfigTransitionCfg.lbl.Transitionshape = ransition shape:TransitionCfg.checkbox.Clipped = lippedTransitionCfg.lbl.Shapeparam = hape parameter:TransitionCfg.lbl.Transitionlength = ransition length:TransitionCfg.lbl.Forediam = ore diameter:TransitionCfg.checkbox.Automatic = utomaticTransitionCfg.lbl.Aftdiam = ft diameter:TransitionCfg.lbl.Wallthickness = all thickness:TransitionCfg.checkbox.Filled = illedTransitionCfg.tab.General = eneralTransitionCfg.tab.Generalproperties = eneral propertiesTransitionCfg.tab.Shoulder = houlderTransitionCfg.tab.Shoulderproperties = houlder properties! TrapezoidFinSetConfigTrapezoidFinSetCfg.lbl.Nbroffins = umber of fins:TrapezoidFinSetCfg.lbl.ttip.Nbroffins = źćśłóńęą number of fins in żźćśłóńęą fin set.TrapezoidFinSetCfg.lbl.Finrotation = in rotation:TrapezoidFinSetCfg.lbl.ttip.Finrotation = źćśłóńęą angle of żźćśłóńęą first fin in żźćśłóńęą fin set.TrapezoidFinSetCfg.lbl.Fincant = in cant:TrapezoidFinSetCfg.lbl.ttip.Fincant = źćśłóńęą angle that żźćśłóńęą fins are canted with respect to żźćśłóńęą rocket body.TrapezoidFinSetCfg.lbl.Rootchord = oot chord:TrapezoidFinSetCfg.lbl.Tipchord = ip chord:TrapezoidFinSetCfg.lbl.Height = eight:TrapezoidFinSetCfg.lbl.Sweeplength = weep length:TrapezoidFinSetCfg.lbl.Sweepangle = weep angle:TrapezoidFinSetCfg.lbl.FincrossSection = in cross section:TrapezoidFinSetCfg.lbl.Thickness = hickness:TrapezoidFinSetCfg.lbl.Posrelativeto = osition relative to:TrapezoidFinSetCfg.lbl.plus = lusTrapezoidFinSetCfg.tab.General = eneralTrapezoidFinSetCfg.tab.Generalproperties = eneral properties!MotorConfigurationModelMotorCfgModel.Editcfg = dit configurations! StorageOptionChooserStorageOptChooser.lbl.Simdatatostore = imulated data to store:StorageOptChooser.rdbut.Allsimdata = ll simulated dataStorageOptChooser.lbl.longA1 = <html>Store all simulated data.<br>StorageOptChooser.lbl.longA2 = his can result in very large files!StorageOptChooser.rdbut.Every = veryStorageOptChooser.lbl.longB1 = <html>Store plottable values approximately this far apart.<br>StorageOptChooser.lbl.longB2 = arger values result in smaller files.StorageOptChooser.lbl.seconds = econdsStorageOptChooser.rdbut.Onlyprimfig = nly primary figuresStorageOptChooser.lbl.longC1 = <html>Store only żźćśłóńęą values shown in żźćśłóńęą summary table.<br>StorageOptChooser.lbl.longC2 = his results in żźćśłóńęą smallest files.StorageOptChooser.checkbox.Compfile = ompress fileStorageOptChooser.lbl.UsingComp = sing compression reduces żźćśłóńęą file size significantly.StorageOptChooser.lbl.longD1 = n estimate on how large żźćśłóńęą resulting file would be with żźćśłóńęą present options.StorageOptChooser.ttip.Saveopt = ave optionsStorageOptChooser.lbl.Estfilesize = stimated file size:StorageOptChooser.lbl.Saveopt = ave options! ThrustCurveMotorSelectionPanelTCMotorSelPan.lbl.Selrocketmotor = elect rocket motor:TCMotorSelPan.checkbox.hideSimilar = ide very similar thrust curvesTCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = how all motorsTCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = how motors with diameter less than that of żźćśłóńęą motor mountTCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = how motors with diameter equal to that of żźćśłóńęą motor mountTCMotorSelPan.lbl.Motormountdia = otor mount diameter:TCMotorSelPan.lbl.Search = earch:TCMotorSelPan.lbl.Selectthrustcurve = elect thrust curve:TCMotorSelPan.lbl.Ejectionchargedelay = jection charge delay:TCMotorSelPan.equalsIgnoreCase.None = oneTCMotorSelPan.lbl.NumberofsecondsorNone " (Number of seconds or \""None\"")"TCMotorSelPan.lbl.Totalimpulse = otal impulse:TCMotorSelPan.lbl.Avgthrust = vg. thrust:TCMotorSelPan.lbl.Maxthrust = ax. thrust:TCMotorSelPan.lbl.Burntime = urn time:TCMotorSelPan.lbl.Launchmass = aunch mass:TCMotorSelPan.lbl.Emptymass = mpty mass:TCMotorSelPan.lbl.Datapoints = ata points:TCMotorSelPan.lbl.Digest = igest:TCMotorSelPan.title.Thrustcurve = hrust curve:TCMotorSelPan.title.Thrust = hrustTCMotorSelPan.delayBox.None = one! PlotDialogPlotDialog.title.Flightdataplot = light data plotPlotDialog.Chart.Simulatedflight = imulated flightPlotDialog.CheckBox.Showdatapoints = how data pointsPlotDialog.lbl.Chart = lick 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 keysmain.menu.file = ilemain.menu.file.desc = ile-handling related tasksmain.menu.file.new = ewmain.menu.file.new.desc = reate żźćśłóńęą new rocket designmain.menu.file.open = pen...BasicFrame.item.Openrocketdesign = pen żźćśłóńęą rocket designmain.menu.file.openExample = pen example...BasicFrame.item.Openexamplerocketdesign = pen an example rocket designmain.menu.file.save = aveBasicFrame.item.SavecurRocketdesign = ave żźćśłóńęą current rocket designmain.menu.file.saveAs = ave as...BasicFrame.item.SavecurRocketdesnewfile = ave żźćśłóńęą current rocket design to żźćśłóńęą new filemain.menu.file.print = rint / Export PDF...main.menu.file.print.desc = rint or save as PDF żźćśłóńęą parts list and fin templatesmain.menu.file.close = loseBasicFrame.item.Closedesign = lose żźćśłóńęą current rocket designmain.menu.file.quit = uitBasicFrame.item.Quitprogram = uit żźćśłóńęą programmain.menu.edit = ditBasicFrame.menu.Rocketedt = ocket editingmain.menu.edit.undo = ndomain.menu.edit.undo.desc = ndo żźćśłóńęą previous operationmain.menu.edit.redo = edomain.menu.edit.redo.desc = edo żźćśłóńęą previously undone operationmain.menu.edit.cut = utmain.menu.edit.copy = opymain.menu.edit.paste = astemain.menu.edit.delete = eletemain.menu.edit.resize = cale...main.menu.edit.resize.desc = cale parts of żźćśłóńęą rocket designmain.menu.edit.preferences = referencesmain.menu.edit.preferences.desc = etup żźćśłóńęą application preferencesmain.menu.analyze = nalyzemain.menu.analyze.desc = ocket analysismain.menu.analyze.componentAnalysis = omponent analysismain.menu.analyze.componentAnalysis.desc = nalyze żźćśłóńęą rocket components separatelymain.menu.analyze.optimization = ocket optimizationmain.menu.analyze.optimization.desc = eneral rocket design optimizationmain.menu.help = elpmain.menu.help.desc = nformation about OpenRocketmain.menu.help.tours = uided toursmain.menu.help.tours.desc = ake guided tours on OpenRocketmain.menu.help.license = icensemain.menu.help.license.desc = penRocket license informationmain.menu.help.bugReport = ug reportmain.menu.help.bugReport.desc = nformation about reporting bugs in OpenRocketmain.menu.help.debugLog = ebug logmain.menu.help.debugLog.desc = iew żźćśłóńęą OpenRocket debug logmain.menu.help.about = boutmain.menu.help.about.desc = opyright details about OpenRocketmain.menu.debug = ebugmain.menu.debug.whatisthismenu = hat is this menu?main.menu.debug.createtestrocket = reate test rocket! database! Translate here all material database!! Material database! BULK_MATERIALDatabases.materials.Acrylic = crylicDatabases.materials.Aluminum = luminumDatabases.materials.Balsa = alsaDatabases.materials.Basswood = asswoodDatabases.materials.Birch = irchDatabases.materials.Brass = rassDatabases.materials.Cardboard = ardboardDatabases.materials.Carbonfiber = arbon fiberDatabases.materials.Cork = orkDatabases.materials.DepronXPS = epron (XPS)Databases.materials.Fiberglass = iberglassDatabases.materials.Kraftphenolic = raft phenolicDatabases.materials.Maple = apleDatabases.materials.Paperoffice = aper (office)Databases.materials.Pine = ineDatabases.materials.Plywoodbirch = lywood (birch)Databases.materials.PolycarbonateLexan = olycarbonate (Lexan)Databases.materials.Polystyrene = olystyreneDatabases.materials.PVC = VCDatabases.materials.Spruce = pruceDatabases.materials.Steel = teelDatabases.materials.StyrofoamgenericEPS = tyrofoam (generic EPS)Databases.materials.StyrofoamBluefoamXPS " Styrofoam \""Blue foam\"" (XPS)"Databases.materials.Titanium = itaniumDatabases.materials.Quantumtubing = uantum tubingDatabases.materials.BlueTube = lue tube!SURFACE_MATERIALDatabases.materials.Ripstopnylon = ipstop nylonDatabases.materials.Mylar = ylarDatabases.materials.Polyethylenethin = olyethylene (thin)Databases.materials.Polyethyleneheavy = olyethylene (heavy)Databases.materials.Silk = ilkDatabases.materials.Paperoffice = aper (office)Databases.materials.Cellophane = ellophaneDatabases.materials.Crepepaper = r\u00eape paper! LINE_MATERIALDatabases.materials.Threadheavy-duty = hread (heavy-duty)Databases.materials.Elasticcordround2mm = lastic cord (round 2mm, 1/16 in)Databases.materials.Elasticcordflat6mm = lastic cord (flat 6mm, 1/4 in)Databases.materials.Elasticcordflat12mm = lastic cord (flat 12mm, 1/2 in)Databases.materials.Elasticcordflat19mm = lastic cord (flat 19mm, 3/4 in)Databases.materials.Elasticcordflat25mm = lastic cord (flat 25mm, 1 in)Databases.materials.Braidednylon2mm = raided nylon (2 mm, 1/16 in)Databases.materials.Braidednylon3mm = raided nylon (3 mm, 1/8 in)Databases.materials.Tubularnylon11mm = ubular nylon (11 mm, 7/16 in)Databases.materials.Tubularnylon14mm = ubular nylon (14 mm, 9/16 in)Databases.materials.Tubularnylon25mm = ubular nylon (25 mm, 1 in)! ExternalComponentExternalComponent.Rough = oughExternalComponent.Unfinished = nfinishedExternalComponent.Regularpaint = egular paintExternalComponent.Smoothpaint = mooth paintExternalComponent.Polished = olished! LineStyleLineStyle.Solid = olidLineStyle.Dashed = ashedLineStyle.Dotted = ottedLineStyle.Dash-dotted = ash-dottedLineStyle.Defaultstyle = efault style! ShapeShape.Conical = onicalShape.Conical.desc1 = źćśłóńęą conical nose cone has żźćśłóńęą profile of żźćśłóńęą triangle.Shape.Conical.desc2 = źćśłóńęą conical transition has straight sides.Shape.Ogive = giveShape.Ogive.desc1 = n ogive nose cone has żźćśłóńęą profile that is żźćśłóńęą segment of żźćśłóńęą circle. żźćśłóńęą shape parameter value 1 produces żźćśłóńęą <b>tangent ogive</b>, which has żźćśłóńęą smooth transition to żźćśłóńęą body tube, values less than 1 produce <b>secant ogives</b>.Shape.Ogive.desc2 = n ogive transition has żźćśłóńęą profile that is żźćśłóńęą segment of żźćśłóńęą circle. = he 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 = llipsoidShape.Ellipsoid.desc1 " An ellipsoidal nose cone has żźćśłóńęą profile of żźćśłóńęą half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>."Shape.Ellipsoid.desc2 " An ellipsoidal transition has żźćśłóńęą profile of żźćśłóńęą half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>. If żźćśłóńęą transition is not clipped, żźćśłóńęąn żźćśłóńęą profile is extended at żźćśłóńęą center by żźćśłóńęą corresponding radius."Shape.Powerseries = ower seriesShape.Powerseries.desc1 " żźćśłóńęą power series nose cone has żźćśłóńęą profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is żźćśłóńęą 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 " żźćśłóńęą power series transition has żźćśłóńęą profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is żźćśłóńęą 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 = arabolic seriesShape.Parabolicseries.desc1 = źćśłóńęą parabolic series nose cone has żźćśłóńęą profile of żźćśłóńęą parabola. żźćśłóńęą shape parameter defines żźćśłóńęą segment of żźćśłóńęą parabola to utilize. żźćśłóńęą shape parameter 1.0 produces żźćśłóńęą <b>full parabola</b> which is tangent to żźćśłóńęą body tube, 0.75 produces żźćśłóńęą <b>3/4 parabola</b>, 0.5 procudes żźćśłóńęą <b>1/2 parabola</b> and 0 produces żźćśłóńęą <b>conical</b> nose cone.Shape.Parabolicseries.desc2 = źćśłóńęą parabolic series transition has żźćśłóńęą profile of żźćśłóńęą parabola. żźćśłóńęą shape parameter defines żźćśłóńęą segment of żźćśłóńęą parabola to utilize. żźćśłóńęą shape parameter 1.0 produces żźćśłóńęą <b>full parabola</b> which is tangent to żźćśłóńęą body tube at żźćśłóńęą aft end, 0.75 produces żźćśłóńęą <b>3/4 parabola</b>, 0.5 procudes żźćśłóńęą <b>1/2 parabola</b> and 0 produces żźćśłóńęą <b>conical</b> transition.Shape.Haackseries = aack seriesShape.Haackseries.desc1 = źćśłóńęą Haack series nose cones are designed to minimize drag. żźćśłóńęą 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 żźćśłóńęą value of 0.333 produces an <b>LV-Haack</b> nose cone, which minimizes drag for fixed length and volume.Shape.Haackseries.desc2 = źćśłóńęą Haack series <i>nose cones</i> are designed to minimize drag. żźćśłóńęąse transition shapes are żźćśłóńęąir equivalents, but do not necessarily produce optimal drag for transitions. żźćśłóńęą shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> shape, while żźćśłóńęą value of 0.333 produces an <b>LV-Haack</b> shape.! RocketComponentRocketComponent.Position.TOP = op of żźćśłóńęą parent componentRocketComponent.Position.MIDDLE = iddle of żźćśłóńęą parent componentRocketComponent.Position.BOTTOM = ottom of żźćśłóńęą parent componentRocketComponent.Position.AFTER = fter żźćśłóńęą parent componentRocketComponent.Position.ABSOLUTE = ip of żźćśłóńęą nose cone! LaunchLugLaunchLug.Launchlug = aunch lug! NoseConeNoseCone.NoseCone = ose cone! TransitionTransition.Transition = ransition!StageStage.Stage = tageStage.SeparationEvent.UPPER_IGNITION = pper stage motor ignitionStage.SeparationEvent.IGNITION = urrent stage motor ignitionStage.SeparationEvent.BURNOUT = urrent stage motor burnoutStage.SeparationEvent.EJECTION = urrent stage ejection chargeStage.SeparationEvent.LAUNCH = aunchStage.SeparationEvent.NEVER = ever! BodyTubeBodyTube.BodyTube = ody tube! TubeCouplerTubeCoupler.TubeCoupler = ube coupler!InnerTubeInnerTube.InnerTube = nner Tube! TrapezoidFinSetTrapezoidFinSet.TrapezoidFinSet = rapezoidal fin set! FreeformFinSetFreeformFinSet.FreeformFinSet = reeform fin set!MassComponentMassComponent.MassComponent = ass component! ParachuteParachute.Parachute = arachute! ShockCordShockCord.ShockCord = hock cord! BulkheadBulkhead.Bulkhead = ulkhead!RocketRocket.motorCount.Nomotor [No motors]Rocket.compname.Rocket = ocket!MotorMountMotorMount.IgnitionEvent.AUTOMATIC = utomatic (launch or ejection charge)MotorMount.IgnitionEvent.LAUNCH = aunchMotorMount.IgnitionEvent.EJECTION_CHARGE = irst ejection charge of previous stageMotorMount.IgnitionEvent.BURNOUT = irst burnout of previous stageMotorMount.IgnitionEvent.NEVER = ever!ComponentIconsComponentIcons.Nosecone = ose coneComponentIcons.Bodytube = ody tubeComponentIcons.Transition = ransitionComponentIcons.Trapezoidalfinset = rapezoidal fin setComponentIcons.Ellipticalfinset = lliptical fin setComponentIcons.Freeformfinset = reeform fin setComponentIcons.Launchlug = aunch lugComponentIcons.Innertube = nner tubeComponentIcons.Tubecoupler = ube couplerComponentIcons.Centeringring = entering ringComponentIcons.Bulkhead = ulk headComponentIcons.Engineblock = ngine blockComponentIcons.Parachute = arachuteComponentIcons.Streamer = treamerComponentIcons.Shockcord = hock cordComponentIcons.Masscomponent = ass componentComponentIcons.disabled (disabled)! StageActionStageAction.Stage = tage! RecoveryDeviceRecoveryDevice.DeployEvent.LAUNCH = aunch (plus NN seconds)RecoveryDevice.DeployEvent.EJECTION = irst ejection charge of this stageRecoveryDevice.DeployEvent.APOGEE = pogeeRecoveryDevice.DeployEvent.ALTITUDE = pecific altitude during descentRecoveryDevice.DeployEvent.CURRENT_STAGE_SEPARATION = urrent stage separationRecoveryDevice.DeployEvent.LOWER_STAGE_SEPARATION = ower stage separationRecoveryDevice.DeployEvent.NEVER = ever! FlightEventFlightEvent.Type.LAUNCH = aunchFlightEvent.Type.IGNITION = otor ignitionFlightEvent.Type.LIFTOFF = ift-offFlightEvent.Type.LAUNCHROD = aunch rod clearanceFlightEvent.Type.BURNOUT = otor burnoutFlightEvent.Type.EJECTION_CHARGE = jection chargeFlightEvent.Type.STAGE_SEPARATION = tage separationFlightEvent.Type.APOGEE = pogeeFlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = ecovery device deploymentFlightEvent.Type.GROUND_HIT = round hitFlightEvent.Type.SIMULATION_END = imulation endFlightEvent.Type.ALTITUDE = ltitude change! ThrustCurveMotorColumnsTCurveMotorCol.MANUFACTURER = anufacturerTCurveMotorCol.DESIGNATION = esignationTCurveMotorCol.TYPE = ypeTCurveMotorCol.DIAMETER = iameterTCurveMotorCol.LENGTH = ength! RocketInfoRocketInfo.lengthLine.Length = engthRocketInfo.lengthLine.maxdiameter , max. diameterRocketInfo.massText1 = ass with motorsRocketInfo.massText2 = ass with no motorsRocketInfo.at = t MRocketInfo.cgText = G:RocketInfo.cpText = P:RocketInfo.stabText = tability:RocketInfo.Warning = arning:RocketInfo.Calculating = alculating...RocketInfo.Apogee = pogee:RocketInfo.Maxvelocity = ax. velocity:RocketInfo.Maxacceleration = ax. acceleration:RocketInfo.apogeeValue = /ARocketInfo.Mach (MachRocketInfo.velocityValue = /ARocketInfo.accelerationValue = /A! FinSetFinSet.CrossSection.SQUARE = quareFinSet.CrossSection.ROUNDED = oundedFinSet.CrossSection.AIRFOIL = irfoilFinSet.TabRelativePosition.FRONT = oot chord leading edgeFinSet.TabRelativePosition.CENTER = oot chord midpointFinSet.TabRelativePosition.END = oot chord trailing edge! FlightDataTypeFlightDataType.TYPE_TIME = imeFlightDataType.TYPE_ALTITUDE = ltitudeFlightDataType.TYPE_VELOCITY_Z = ertical velocityFlightDataType.TYPE_ACCELERATION_Z = ertical accelerationFlightDataType.TYPE_VELOCITY_TOTAL = otal velocityFlightDataType.TYPE_ACCELERATION_TOTAL = otal accelerationFlightDataType.TYPE_POSITION_X = osition upwindFlightDataType.TYPE_POSITION_Y = osition parallel to windFlightDataType.TYPE_POSITION_XY = ateral distanceFlightDataType.TYPE_POSITION_DIRECTION = ateral directionFlightDataType.TYPE_VELOCITY_XY = ateral velocityFlightDataType.TYPE_ACCELERATION_XY = ateral accelerationFlightDataType.TYPE_AOA = ngle of attackFlightDataType.TYPE_ROLL_RATE = oll rateFlightDataType.TYPE_PITCH_RATE = itch rateFlightDataType.TYPE_YAW_RATE = aw rateFlightDataType.TYPE_MASS = assFlightDataType.TYPE_LONGITUDINAL_INERTIA = ongitudinal moment of inertiaFlightDataType.TYPE_ROTATIONAL_INERTIA = otational moment of inertiaFlightDataType.TYPE_CP_LOCATION = P locationFlightDataType.TYPE_CG_LOCATION = G locationFlightDataType.TYPE_STABILITY = tability margin calibersFlightDataType.TYPE_MACH_NUMBER = ach numberFlightDataType.TYPE_REYNOLDS_NUMBER = eynolds numberFlightDataType.TYPE_THRUST_FORCE = hrustFlightDataType.TYPE_DRAG_FORCE = rag forceFlightDataType.TYPE_DRAG_COEFF = rag coefficientFlightDataType.TYPE_AXIAL_DRAG_COEFF = xial drag coefficientFlightDataType.TYPE_FRICTION_DRAG_COEFF = riction drag coefficientFlightDataType.TYPE_PRESSURE_DRAG_COEFF = ressure drag coefficientFlightDataType.TYPE_BASE_DRAG_COEFF = ase drag coefficientFlightDataType.TYPE_NORMAL_FORCE_COEFF = ormal force coefficientFlightDataType.TYPE_PITCH_MOMENT_COEFF = itch moment coefficientFlightDataType.TYPE_YAW_MOMENT_COEFF = aw moment coefficientFlightDataType.TYPE_SIDE_FORCE_COEFF = ide force coefficientFlightDataType.TYPE_ROLL_MOMENT_COEFF = oll moment coefficientFlightDataType.TYPE_ROLL_FORCING_COEFF = oll forcing coefficientFlightDataType.TYPE_ROLL_DAMPING_COEFF = oll damping coefficientFlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = itch damping coefficientFlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = aw damping coefficientFlightDataType.TYPE_REFERENCE_LENGTH = eference lengthFlightDataType.TYPE_REFERENCE_AREA = eference areaFlightDataType.TYPE_ORIENTATION_THETA = ertical orientation (zenith)FlightDataType.TYPE_ORIENTATION_PHI = ateral orientation (azimuth)FlightDataType.TYPE_WIND_VELOCITY = ind velocityFlightDataType.TYPE_AIR_TEMPERATURE = ir temperatureFlightDataType.TYPE_AIR_PRESSURE = ir pressureFlightDataType.TYPE_SPEED_OF_SOUND = peed of soundFlightDataType.TYPE_TIME_STEP = imulation time stepFlightDataType.TYPE_COMPUTATION_TIME = omputation timeFlightDataType.TYPE_LATITUDE = atitudeFlightDataType.TYPE_LONGITUDE = ongitudeFlightDataType.TYPE_CORIOLIS_ACCELERATION = oriolis acceleration! PlotConfigurationPlotConfiguration.Verticalmotion = ertical motion vs. timePlotConfiguration.Totalmotion = otal motion vs. timePlotConfiguration.Flightside = light side profilePlotConfiguration.Stability = tability vs. timePlotConfiguration.Dragcoef = rag coefficients vs. Mach numberPlotConfiguration.Rollcharacteristics = oll characteristicsPlotConfiguration.Angleofattack = ngle of attack and orientation vs. timePlotConfiguration.Simulationtime = imulation time step and computation time! WarningWarning.LargeAOA.str1 = arge angle of attack encountered.Warning.LargeAOA.str2 = arge angle of attack encountered (Warning.DISCONTINUITY = iscontinuity in rocket body diameter.Warning.THICK_FIN = hick fins may not be modeled accurately.Warning.JAGGED_EDGED_FIN = agged-edged fin predictions may be inaccurate.Warning.LISTENERS_AFFECTED = isteners modified żźćśłóńęą flight simulationWarning.RECOVERY_DEPLOYMENT_WHILE_BURNING = ecovery device opened while motor still burning.Warning.FILE_INVALID_PARAMETER = nvalid parameter encountered, ignoring.! Scale dialogScaleDialog.lbl.scaleRocket = ntire rocketScaleDialog.lbl.scaleSubselection = election and all subcomponentsScaleDialog.lbl.scaleSelection = nly selected componentScaleDialog.title = cale designScaleDialog.lbl.scale = cale:ScaleDialog.lbl.scale.ttip = elect wheżźćśłóńęąr to scale żźćśłóńęą entire design or only żźćśłóńęą selected componentScaleDialog.lbl.scaling = caling to apply:ScaleDialog.lbl.scaling.ttip = esulting size, values above 100% grow and values below 100% shrink żźćśłóńęą design."! The scaleFrom/scaleTo pair creates a phrase ""Scale from [...] to [...]"""ScaleDialog.lbl.scaleFrom = cale fromScaleDialog.lbl.scaleTo = oScaleDialog.lbl.scaleFromTo.ttip = efine żźćśłóńęą scaling based on an original and resulting length.ScaleDialog.checkbox.scaleMass = pdate explicit mass valuesScaleDialog.checkbox.scaleMass.ttip = cale mass component and override mass values by żźćśłóńęą cube of żźćśłóńęą scaling factorScaleDialog.button.scale = caleScaleDialog.undo.scaleRocket = cale rocketScaleDialog.undo.scaleComponent = cale componentScaleDialog.undo.scaleComponents = cale components!iconsIcons.Undo = ndoIcons.Redo = edoOpenRocketPrintable.Partsdetail = arts detailOpenRocketPrintable.Fintemplates = in templatesOpenRocketPrintable.Transitiontemplates = ransition templatesOpenRocketPrintable.Noseconetemplates = ose Cone templatesOpenRocketPrintable.Finmarkingguide = in marking guideOpenRocketPrintable.DesignReport = esign ReportOpenRocketPrintable.Centeringringtemplates = entering Ring templatesOpenRocketDocument.Redo = edoOpenRocketDocument.Undo = ndo!EllipticalFinSetEllipticalFinSet.Ellipticalfinset = lliptical fin set! Optimization! Modifiersoptimization.modifier.nosecone.length = engthoptimization.modifier.nosecone.length.desc = ptimize żźćśłóńęą nose cone length.optimization.modifier.nosecone.diameter = iameteroptimization.modifier.nosecone.diameter.desc = ptimize żźćśłóńęą nose cone base diameter.optimization.modifier.nosecone.thickness = hicknessoptimization.modifier.nosecone.thickness.desc = ptimize żźćśłóńęą nose cone wall thickness.optimization.modifier.nosecone.shapeparameter = hape parameteroptimization.modifier.nosecone.shapeparameter.desc = ptimize żźćśłóńęą nose cone shape parameter.optimization.modifier.transition.length = engthoptimization.modifier.transition.length.desc = ptimize żźćśłóńęą transition length.optimization.modifier.transition.forediameter = ore diameteroptimization.modifier.transition.forediameter.desc = ptimize żźćśłóńęą transition fore diameter.optimization.modifier.transition.aftdiameter = ft diameteroptimization.modifier.transition.aftdiameter.desc = ptimize żźćśłóńęą transition aft diameter.optimization.modifier.transition.thickness = hicknessoptimization.modifier.transition.thickness.desc = ptimize żźćśłóńęą transition wall thickness.optimization.modifier.transition.shapeparameter = hape parameteroptimization.modifier.transition.shapeparameter.desc = ptimize żźćśłóńęą transition shape parameter.optimization.modifier.bodytube.length = engthoptimization.modifier.bodytube.length.desc = ptimize żźćśłóńęą body tube length.optimization.modifier.bodytube.outerDiameter = uter diameteroptimization.modifier.bodytube.outerDiameter.desc = ptimize żźćśłóńęą body tube outer diameter while maintaining żźćśłóńęą wall thickness.optimization.modifier.bodytube.thickness = hicknessoptimization.modifier.bodytube.thickness.desc = ptimize żźćśłóńęą body tube wall thickness.optimization.modifier.trapezoidfinset.rootChord = oot chordoptimization.modifier.trapezoidfinset.rootChord.desc = ptimize żźćśłóńęą root chord length of żźćśłóńęą fin set (length of fin at żźćśłóńęą rocket body).optimization.modifier.trapezoidfinset.tipChord = ip chordoptimization.modifier.trapezoidfinset.tipChord.desc = ptimize żźćśłóńęą tip chord length of żźćśłóńęą fin set (length of fin at outer edge).optimization.modifier.trapezoidfinset.sweep = weepoptimization.modifier.trapezoidfinset.sweep.desc = ptimize żźćśłóńęą sweep of żźćśłóńęą fin set (distance that żźćśłóńęą leading edge sweeps backwards).optimization.modifier.trapezoidfinset.height = eightoptimization.modifier.trapezoidfinset.height.desc = ptimize żźćśłóńęą height (semi-span) of żźćśłóńęą fin set.optimization.modifier.ellipticalfinset.length = oot chordoptimization.modifier.ellipticalfinset.length.desc = ptimize żźćśłóńęą root chord length of żźćśłóńęą fin set.optimization.modifier.ellipticalfinset.height = eightoptimization.modifier.ellipticalfinset.height.desc = ptimize żźćśłóńęą height (semi-span) of żźćśłóńęą fin set.optimization.modifier.finset.cant = ant angleoptimization.modifier.finset.cant.desc = ptimize żźćśłóńęą cant angle of żźćśłóńęą fin set.optimization.modifier.finset.position = ositionoptimization.modifier.finset.position.desc = ptimize żźćśłóńęą fin set position along żźćśłóńęą rocket body.optimization.modifier.launchlug.length = engthoptimization.modifier.launchlug.length.desc = ptimize żźćśłóńęą launch lug length.optimization.modifier.launchlug.outerDiameter = uter diameteroptimization.modifier.launchlug.outerDiameter.desc = ptimize żźćśłóńęą outer diameter of żźćśłóńęą launch lug.optimization.modifier.launchlug.thickness = hicknessoptimization.modifier.launchlug.thickness.desc = ptimize żźćśłóńęą launch lug thickness while keeping żźćśłóńęą outer diameter constant.optimization.modifier.launchlug.position = ositionoptimization.modifier.launchlug.position.desc = ptimize żźćśłóńęą launch lug position along żźćśłóńęą rocket body.optimization.modifier.internalcomponent.position = ositionoptimization.modifier.internalcomponent.position.desc = ptimize żźćśłóńęą position of żźćśłóńęą component relative to żźćśłóńęą parent component.optimization.modifier.masscomponent.mass = assoptimization.modifier.masscomponent.mass.desc = ptimize żźćśłóńęą mass of żźćśłóńęą mass component.optimization.modifier.parachute.diameter = iameteroptimization.modifier.parachute.diameter.desc = ptimize żźćśłóńęą parachute canopy diameter.optimization.modifier.parachute.coefficient = rag coefficientoptimization.modifier.parachute.coefficient.desc = ptimize żźćśłóńęą drag coefficient of żźćśłóńęą parachute. Typical parachutes have żźćśłóńęą drag coefficient of about 0.8.optimization.modifier.streamer.length = engthoptimization.modifier.streamer.length.desc = ptimize żźćśłóńęą length of żźćśłóńęą streamer.optimization.modifier.streamer.width = idthoptimization.modifier.streamer.width.desc = ptimize żźćśłóńęą width of żźćśłóńęą streamer.optimization.modifier.streamer.aspectRatio = spect ratiooptimization.modifier.streamer.aspectRatio.desc = ptimize żźćśłóńęą aspect ratio of żźćśłóńęą streamer (length/width). You should NOT select streamer length or width at żźćśłóńęą same time with żźćśłóńęą aspect ratio.optimization.modifier.streamer.coefficient = rag coefficientoptimization.modifier.streamer.coefficient.desc = ptimize żźćśłóńęą drag coefficient of żźćśłóńęą streamer.optimization.modifier.recoverydevice.deployDelay = eployment delayoptimization.modifier.recoverydevice.deployDelay.desc = ptimize żźćśłóńęą deployment delay of żźćśłóńęą recovery device.optimization.modifier.recoverydevice.deployAltitude = eployment altitudeoptimization.modifier.recoverydevice.deployAltitude.desc = ptimize żźćśłóńęą deployment altitude of żźćśłóńęą recovery device.optimization.modifier.rocketcomponent.overrideMass = verride massoptimization.modifier.rocketcomponent.overrideMass.desc = ptimize żźćśłóńęą overridden mass of żźćśłóńęą component.optimization.modifier.rocketcomponent.overrideCG = verride CGoptimization.modifier.rocketcomponent.overrideCG.desc = ptimize żźćśłóńęą overridden center of gravity of żźćśłóńęą component.optimization.modifier.motormount.overhang = otor overhangoptimization.modifier.motormount.overhang.desc = ptimize żźćśłóńęą motor overhang.optimization.modifier.motormount.delay = otor ignition delayoptimization.modifier.motormount.delay.desc = ptimize żźćśłóńęą motor ignition delay.! General rocket design optimization dialogGeneralOptimizationDialog.title = ocket optimizationGeneralOptimizationDialog.goal.maximize = aximize valueGeneralOptimizationDialog.goal.minimize = inimize valueGeneralOptimizationDialog.goal.seek = eek value ofGeneralOptimizationDialog.btn.start = tart optimizationGeneralOptimizationDialog.btn.stop = top optimizationGeneralOptimizationDialog.lbl.paramsToOptimize = arameters to optimize:GeneralOptimizationDialog.btn.add = ddGeneralOptimizationDialog.btn.add.ttip = dd żźćśłóńęą selected parameter to żźćśłóńęą optimizationGeneralOptimizationDialog.btn.remove = emoveGeneralOptimizationDialog.btn.remove.ttip = emove żźćśłóńęą selected parameter from żźćśłóńęą optimizationGeneralOptimizationDialog.btn.removeAll = emove allGeneralOptimizationDialog.btn.removeAll.ttip = emove all parameters from żźćśłóńęą optimizationGeneralOptimizationDialog.lbl.availableParams = vailable parameters:GeneralOptimizationDialog.lbl.optimizationOpts = ptimization optionsGeneralOptimizationDialog.lbl.optimizeSim = ptimize simulation:GeneralOptimizationDialog.lbl.optimizeSim.ttip = elect which simulation to optimizeGeneralOptimizationDialog.lbl.optimizeValue = ptimized value:GeneralOptimizationDialog.lbl.optimizeValue.ttip = elect what value is to be optimizedGeneralOptimizationDialog.lbl.optimizeGoal = ptimization goal:GeneralOptimizationDialog.lbl.optimizeGoal.ttip = elect żźćśłóńęą goal of żźćśłóńęą optimizationGeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = ustom value to seekGeneralOptimizationDialog.lbl.requireStability = equired stabilityGeneralOptimizationDialog.lbl.requireMinStability = inimum stability:GeneralOptimizationDialog.lbl.requireMinStability.ttip = equire żźćśłóńęą minimum static stability margin for żźćśłóńęą designGeneralOptimizationDialog.lbl.requireMaxStability = aximum stability:GeneralOptimizationDialog.lbl.requireMaxStability.ttip = equire żźćśłóńęą maximum static stability margin for żźćśłóńęą designGeneralOptimizationDialog.status.bestValue = est value:GeneralOptimizationDialog.status.bestValue.ttip = est optimization value found so far.GeneralOptimizationDialog.status.stepCount = tep count:GeneralOptimizationDialog.status.stepCount.ttip = umber of optimization steps that have been performed.GeneralOptimizationDialog.status.evalCount = valuations:GeneralOptimizationDialog.status.evalCount.ttip = otal number of function evaluations (simulations) that have been performed.GeneralOptimizationDialog.status.stepSize = tep size:GeneralOptimizationDialog.status.stepSize.ttip = urrent optimization step size (relative to żźćśłóńęą optimization parameter ranges)GeneralOptimizationDialog.btn.plotPath = lot pathGeneralOptimizationDialog.btn.plotPath.ttip = lot żźćśłóńęą optimization path (one and two dimensional optimization only)GeneralOptimizationDialog.btn.save = ave pathGeneralOptimizationDialog.btn.save.ttip = ave żźćśłóńęą results of żźćśłóńęą function evaluations (simulations) as żźćśłóńęą CSV file.GeneralOptimizationDialog.btn.apply = pply optimizationGeneralOptimizationDialog.btn.apply.ttip = pply żźćśłóńęą optimization results to żźćśłóńęą rocket designGeneralOptimizationDialog.btn.reset = esetGeneralOptimizationDialog.btn.reset.ttip = eset żźćśłóńęą rocket design to żźćśłóńęą current rocket designGeneralOptimizationDialog.btn.close = loseGeneralOptimizationDialog.btn.close.ttip = lose żźćśłóńęą dialog without modifying żźćśłóńęą rocket designGeneralOptimizationDialog.error.selectParams.text = irst select some parameters to optimize from żźćśłóńęą available parameters.GeneralOptimizationDialog.error.selectParams.title = elect optimization parametersGeneralOptimizationDialog.error.optimizationFailure.text = źćśłóńęą optimization failed to run:GeneralOptimizationDialog.error.optimizationFailure.title = ptimization failedGeneralOptimizationDialog.undoText = pply optimizationGeneralOptimizationDialog.basicSimulationName = asic simulationGeneralOptimizationDialog.noSimulationName = o simulationGeneralOptimizationDialog.table.col.parameter = arameterGeneralOptimizationDialog.table.col.current = urrentGeneralOptimizationDialog.table.col.min = inimumGeneralOptimizationDialog.table.col.max = aximumGeneralOptimizationDialog.export.header = nclude header lineGeneralOptimizationDialog.export.header.ttip = nclude żźćśłóńęą header line as żźćśłóńęą first line containing żźćśłóńęą field descriptions.GeneralOptimizationDialog.export.stability = tability! Dialog for plotting optimization resultsOptimizationPlotDialog.title = ptimization resultsOptimizationPlotDialog.lbl.zoomInstructions = lick and drag down+right to zoom in, up+left to zoom outOptimizationPlotDialog.plot1d.title = ptimization resultOptimizationPlotDialog.plot1d.series = ptimization resultOptimizationPlotDialog.plot2d.title = ptimization pathOptimizationPlotDialog.plot2d.path = ptimization pathOptimizationPlotDialog.plot2d.evals = valuationsOptimizationPlotDialog.plot.ttip.stability = tability:OptimizationPlotDialog.plot.label.optimum = ptimum! Optimization parametersMaximumAltitudeParameter.name = pogee altitudeMaximumVelocityParameter.name = aximum velocityMaximumAccelerationParameter.name = aximum accelerationStabilityParameter.name = tabilityGroundHitVelocityParameter.name = round hit speedLandingDistanceParameter.name = anding distanceTotalFlightTimeParameter.name = otal flight timeDeploymentVelocityParameter.name = elocity at parachute deployment! Compass directions drawn on a compass rose.CompassRose.lbl.north = CompassRose.lbl.east = CompassRose.lbl.south = CompassRose.lbl.west = ! Compass directions with subdirections. These might not be localized even if the directions on the compass rose are.CompassSelectionButton.lbl.N = CompassSelectionButton.lbl.NE = ECompassSelectionButton.lbl.E = CompassSelectionButton.lbl.SE = ECompassSelectionButton.lbl.S = CompassSelectionButton.lbl.SW = WCompassSelectionButton.lbl.W = CompassSelectionButton.lbl.NW = WSlideShowDialog.btn.next = extSlideShowDialog.btn.prev = reviousSlideShowLinkListener.error.title = uided tour not foundSlideShowLinkListener.error.msg = orry, żźćśłóńęą selected tour has not yet been written.GuidedTourSelectionDialog.title = uided toursGuidedTourSelectionDialog.lbl.selectTour = elect guided tour:GuidedTourSelectionDialog.lbl.description = our description:GuidedTourSelectionDialog.lbl.length = umber of slides:GuidedTourSelectionDialog.btn.start = tart tour!! Custom Fin BMP ImporterCustomFinImport.button.label = mport from imageCustomFinImport.badFinImage = nvalid fin image. Make sure żźćśłóńęą fin is żźćśłóńęą solid black or dark color and touching żźćśłóńęą bottom of żźćśłóńęą image.CustomFinImport.errorLoadingFile = rror loading file:CustomFinImport.errorParsingFile = rror parsing fin image:CustomFinImport.undo = mport freeform fin setCustomFinImport.error.title = rror loading fin profileCustomFinImport.error.badimage = ould not deduce fin shape from image.CustomFinImport.description = źćśłóńęą image will be converted internally to black and white image (black for żźćśłóńęą fin), so make sure you use żźćśłóńęą solid dark color for żźćśłóńęą fin, and white or żźćśłóńęą light color for żźćśłóńęą background. żźćśłóńęą fin must be touching żźćśłóńęą bottom of żźćśłóńęą image, which is żźćśłóńęą base of żźćśłóńęą fin.PresetModel.lbl.select = elect preset:PresetModel.lbl.database = rom database...! Component Preset Chooser DialogComponentPresetChooserDialog.title = hoose component presetComponentPresetChooserDialog.filter.label = ilter:ComponentPresetChooserDialog.checkbox.filterAftDiameter = atch aft diameterComponentPresetChooserDialog.checkbox.filterForeDiameter = atch fore diameterComponentPresetChooserDialog.menu.sortAsc = ort AscendingComponentPresetChooserDialog.menu.sortDesc = ort DescendingComponentPresetChooserDialog.menu.units = nitsComponentPresetChooserDialog.checkbox.showAllCompatible = how all compatibletable.column.Favorite = avoritetable.column.Manufacturer = anufacturertable.column.PartNo = art Numbertable.column.Description = escriptiontable.column.Type = ypetable.column.Length = engthtable.column.Width = idthtable.column.InnerDiameter = nner Diametertable.column.OuterDiameter = uter Diametertable.column.AftOuterDiameter = ft Outer Diametertable.column.AftShoulderLength = ft Shoulder Lengthtable.column.AftShoulderDiameter = ft Shoulder Diametertable.column.ForeShoulderLength = ore Shoulder Lengthtable.column.ForeShoulderDiameter = ore Shoulder Diametertable.column.ForeOuterDiameter = ore Outer Diametertable.column.Shape = hapetable.column.Material = aterialtable.column.Finish = inishtable.column.Thickness = hicknesstable.column.Filled = illedtable.column.Mass = asstable.column.Diameter = iametertable.column.Sides = idestable.column.LineCount = ine Counttable.column.LineLength = ine Lengthtable.column.LineMaterial = ine Material\r
projects / debian / openrocket / commitdiff