-## 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
+#
+ # Polish base translation file
+ #
+ # Should you need to add new logical keys here is the proposed method
+ #
+ # 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 = messages_pl.properties
+
+ ! RocketActions
+ RocketActions.checkbox.Donotaskmeagain = Nie pytaj ponownie
+ RocketActions.lbl.Youcanchangedefop = Domy\u015Bln\u0105 operacj\u0119 mo\u017Cna zmieni\u0107 w ustawieniach.
+ RocketActions.showConfirmDialog.lbl1 = Usun\u0105\u0107 zaznaczone symulacje?
+ RocketActions.showConfirmDialog.lbl2 = <html><i>Tej operacji nie mo\u017Cna cofn\u0105\u0107.</i>
+ RocketActions.showConfirmDialog.title = Usu\u0144 symulacje
+ RocketActions.DelCompAct.Delete = Usu\u0144
+ RocketActions.DelCompAct.ttip.Delete = Usu\u0144 wybran\u0105 cz\u0119\u015B\u0107
+ RocketActions.DelSimuAct.Delete = Usu\u0144
+ RocketActions.DelSimuAct.ttip.Delete = Usu\u0144 zaznaczon\u0105 symulacj\u0119.
+ RocketActions.DelAct.Delete = Usu\u0144
+ RocketActions.DelAct.ttip.Delete = Usu\u0144 wybran\u0105 cz\u0119\u015B\u0107 lub symulacj\u0119
+ RocketActions.CutAction.Cut = Wytnij
+ RocketActions.CutAction.ttip.Cut = Wytnij do schowka wybran\u0105 cz\u0119\u015B\u0107 lub symulacj\u0119 i usu\u0144 z projektu
+ RocketActions.CopyAct.Copy = Kopiuj
+ RocketActions.CopyAct.ttip.Copy = Kopiuj do schowka wybran\u0105 cz\u0119\u015B\u0107 (oraz jej cz\u0119\u015Bci sk\u0142adowe)
+ RocketActions.PasteAct.Paste = Wklej
+ RocketActions.PasteAct.ttip.Paste = Wklej wybran\u0105 cz\u0119\u015B\u0107 lub symulacj\u0119 ze schowka do projektu.
+ RocketActions.EditAct.Edit = Edycja
+ RocketActions.EditAct.ttip.Edit = Edytuj zaznaczon\u0105 cz\u0119\u015B\u0107.
+ RocketActions.NewStageAct.Newstage = Nowy stopie\u0144
+ RocketActions.NewStageAct.ttip.Newstage = Dodaj stopie\u0144 do projektu rakiety.
+ RocketActions.ActBoosterstage = Stopie\u0144 startowy rakiety
+ RocketActions.MoveUpAct.Moveup = W gór\u0119
+ RocketActions.MoveUpAct.ttip.Moveup = Przesu\u0144 wybran\u0105 cz\u0119\u015B\u0107 w gór\u0119.
+ RocketActions.MoveDownAct.Movedown = W dó\u0142
+ RocketActions.MoveDownAct.ttip.Movedown = Przesu\u0144 wybran\u0105 cz\u0119\u015B\u0107 w dó\u0142.
+
+ ! RocketPanel
+ RocketPanel.FigTypeAct.Sideview = Widok z boku
+ RocketPanel.FigTypeAct.ttip.Sideview = Widok z boku
+ RocketPanel.FigTypeAct.Backview = Widok z ty\u0142u
+ RocketPanel.FigTypeAct.ttip.Backview = Widok tylny
+ RocketPanel.FigViewAct.2D = Widok 2D
+ RocketPanel.FigViewAct.ttip.2D = Widok 2D
+ RocketPanel.FigViewAct.3D = Widok 3D
+ RocketPanel.FigViewAct.ttip.3D = Widok 3D
+ RocketPanel.lbl.Motorcfg = Konfiguracja silnika:
+ RocketPanel.lbl.infoMessage = <html>Kliknij aby wybra\u0107 Shift+kliknij aby wybra\u0107 kolejny kliknij podwójnie aby edytowa\u0107 Kliknij+przeci\u0105gnij aby przesun\u0105\u0107
+
+
+ ! BasicFrame
+ BasicFrame.tab.Rocketdesign = Projekt rakiety
+ BasicFrame.tab.Flightsim = Symulacje lotu
+ BasicFrame.title.Addnewcomp = Dodaj now\u0105 cz\u0119\u015B\u0107
+ BasicFrame.dlg.lbl1 = Projekt '
+ BasicFrame.dlg.lbl2 = ' nie zosta\u0142 zapisany.
+ BasicFrame.dlg.lbl3 = Czy chcesz zapisa\u0107?
+ BasicFrame.dlg.title = Projekt nie zosta\u0142 zapisany
+ BasicFrame.StageName.Sustainer = Cz\u0142on g\u0142ówny
+ BasicFrame.WarningDialog.txt1 = Podczas próby otwarcia wyst\u0105pi\u0142y nast\u0119puj\u0105ce problemy:
+ BasicFrame.WarningDialog.txt2 = Niektóre z elementów projektu mog\u0142y zosta\u0107 b\u0142\u0119dnie za\u0142adowane.
+ BasicFrame.WarningDialog.title = Ostrze\u017Cenia podczas otwierania pliku
+
+
+ ! General error messages used in multiple contexts
+ error.fileExists.title = Plik ju\u017C istnieje
+ error.fileExists.desc = Plik '{filename}' ju\u017C istnieje Czy chcesz nadpisa\u0107?
+
+ error.writing.title = B\u0142\u0105d przy zapisie pliku
+ error.writing.desc = Wyst\u0105pi\u0142 b\u0142\u0105d podczas zapisu pliku:
+
+
+ ! Labels used in buttons of dialog windows
+ # TODO: Rename these to "btn.xxx"
+ button.ok = OK
+ button.cancel = Anuluj
+ button.close = Zamknij
+
+ ! Common labels used in buttons of dialog windows
+ dlg.but.ok = OK
+ dlg.but.cancel = Anuluj
+ dlg.but.close = Zamknij
+
+
+ ! General file type names
+ filetypes.pdf = Pliki PDF (*.pdf)
+ BasicFrame.SimpleFileFilter1 = Wszystkie projekty rakiet (*.ork; *.rkt)
+ BasicFrame.SimpleFileFilter2 = Projekty OpenRocket (*.ork; *.rkt)
+ BasicFrame.SimpleFileFilter3 = Projekty RockSim (*.rkt)
+ BasicFrame.SimpleFileFilter4 = Ustawienia OpenRocket (*.orc)
+ filetypes.images = Pliki obrazów
+
+
+ ! About Dialog
+ AboutDialog.lbl.version = Wersja
+ ! 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 = Polskie t\u0142umaczenie w wykonaniu:
+ AboutDialog.lbl.translator = PTR (\u0141ukasz & Alex)
+ AboutDialog.lbl.translatorWebsite =
+ AboutDialog.lbl.translatorIcon =
+
+
+ ! Print dialog
+ PrintDialog.title = Drukuj lub eksportuj
+ PrintDialog.but.previewAndPrint = Podgl\u0105d & wydruk
+ PrintDialog.checkbox.showByStage = Poka\u017C wg stopni
+ PrintDialog.lbl.selectElements = Wybierz elementy do za\u0142\u0105czenia:
+ printdlg.but.saveaspdf = Zapisz jako PDF
+ printdlg.but.preview = Podgl\u0105d
+ printdlg.but.settings = Ustawienia
+ PrintDialog.error.preview.title = Nie mo\u017Cna wy\u015Bwietli\u0107 podgl\u0105du
+ PrintDialog.error.preview.desc1 = Nie mo\u017Cna wy\u015Bwietli\u0107 podgl\u0105du PDF.
+ PrintDialog.error.preview.desc2 = Zamiast tego wybierz opcj\u0119 "zapisz jako PDF".
+
+ !PrintSettingsDialog
+ PrintSettingsDialog.title = Ustawienia drukowania
+ PrintSettingsDialog.lbl.Templatefillcolor = Kolor wype\u0142nienia szablonu:
+ PrintSettingsDialog.lbl.Templatebordercolor = Kolor ramki szablonu:
+ PrintSettingsDialog.lbl.Papersize = Wielko\u015B\u0107 arkusza:
+ PrintSettingsDialog.lbl.Paperorientation = Orientacja arkusza:
+ PrintSettingsDialog.but.Reset = Reset
+ PrintSettingsDialog.but.Close = Zamknij
+
+
+ ! Bug Report dialog
+ bugreport.dlg.title = Raport o b\u0142\u0119dach
+ bugreport.dlg.but.Sendbugreport = Wy\u015Blij raport o b\u0142\u0119dach
+ bugreport.dlg.but.Sendbugreport.Ttip = Wy\u015Blij raport z b\u0142\u0119dami automatycznie do deweloperów OpenRocket.
+ bugreport.dlg.successmsg1 = Raport z b\u0142\u0119dami zosta\u0142 wys\u0142any.
+ bugreport.dlg.successmsg2 = Dzi\u0119kujemy za Twój wk\u0142ad w rozwój OpenRocket!
+ bugreport.dlg.successmsg3 = Raport z b\u0142\u0119dami zosta\u0142 wys\u0142any.
+ bugreport.dlg.connectedInternet = <html>Je\u017Celi Internet jest pod\u0142\u0105czony, mo\u017Cesz klikn\u0105\u0107 <em>Wy\u015Blij raport z b\u0142\u0119dami</em>.
+ bugreport.dlg.otherwise = W przeciwnym wypadku wy\u015Blij poni\u017Cszy tekst na adres:
+ bugreport.lbl.Theinformation = Powy\u017Csze informacje mog\u0105 by\u0107 dodane do publicznego raportu b\u0142\u0119dów. Upewnij si\u0119, \u017Ce tekst nie zawiera \u017Cadnych informacji, których nie chcia\u0142(a)by\u015B upublicznia\u0107.
+ bugreport.dlg.failedmsg1 = OpenRocket nie by\u0142 w stanie wys\u0142a\u0107 raportu z b\u0142\u0119dami:
+ bugreport.dlg.failedmsg2 = Prosz\u0119 wys\u0142a\u0107 raport r\u0119cznie do
+ bugreport.dlg.failedmsg3 = B\u0142\u0105d podczas wysy\u0142ania raportu
+ bugreport.reportDialog.txt = <html><b>Mo\u017Cesz zg\u0142osi\u0107 b\u0142\u0105d w OpenRocket poprzez wype\u0142nienie oraz wys\u0142anie poni\u017Cszego formularza.</b><br>Mo\u017Cesz tak\u017Ce zg\u0142asza\u0107 b\u0142\u0119dy oraz dodawa\u0107 za\u0142\u0105czniki na stronie OpenRocket.
+ bugreport.reportDialog.txt2 = <html><b>Prosz\u0119 do\u0142\u0105czy\u0107 krótki opis czynno\u015Bci wykonywanych w momencie wyst\u0105pienia b\u0142\u0119du.</b>
+ bugreport.dlg.provideDescription = Prosz\u0119 najpierw wprowadzi\u0107 opis b\u0142\u0119du.
+ bugreport.dlg.provideDescription.title = Brak opisu b\u0142\u0119du
+
+
+ ! Debug log dialog
+ debuglogdlg.but.clear = Wyczy\u015B\u0107
+ debuglogdlg.OpenRocketdebuglog = Rejestr debuggera programu OpenRocket
+ debuglogdlg.Displayloglines = Wy\u015Bwietl wiersze rejestru:
+ debuglogdlg.Follow = \u015Aledzenie
+ debuglogdlg.col.Time = Czas
+ debuglogdlg.col.Level = Poziom
+ debuglogdlg.col.Location = Lokalizacja
+ debuglogdlg.col.Message = Komunikat
+ debuglogdlg.lbl.Loglinenbr = Numer wiersza rejestru:
+ debuglogdlg.lbl.Time = Czas:
+ debuglogdlg.lbl.Level = Poziom:
+ debuglogdlg.lbl.Location = Lokalizacja:
+ debuglogdlg.lbl.Logmessage = Komunikat:
+ debuglogdlg.lbl.Stacktrace = Zapis stosu wywo\u0142a\u0144:
+
+
+ ! Edit Motor configuration dialog
+ edtmotorconfdlg.but.removemotor = Usu\u0144 silnik
+ edtmotorconfdlg.but.Selectmotor = Wybierz silnik
+ edtmotorconfdlg.but.Removeconfiguration = Usu\u0144 konfiguracj\u0119
+ edtmotorconfdlg.but.Newconfiguration = Nowa konfiguracja
+ edtmotorconfdlg.lbl.Motormounts = <html><b>Gniazda silnikowe:</b>
+ edtmotorconfdlg.title.Editmotorconf = Edytuj konfiguracje silnika
+ edtmotorconfdlg.selectcomp = <html>Wybierz cz\u0119\u015Bci, które pe\u0142ni\u0105 funkcj\u0119 gniazd silnikowych:
+ edtmotorconfdlg.lbl.Motorconfig = <html><b>Konfiguracje silników:</b>
+ edtmotorconfdlg.lbl.Configname = Nazwa konfiguracji:
+ edtmotorconfdlg.lbl.Leavenamedefault = Pozostaw bez nazwy w celu u\u017Cycia nazwy domy\u015Blnej.
+
+ ! Example design dialog
+ exdesigndlg.but.open = Otwórz
+ exdesigndlg.lbl.Selectexample = Wybierz przyk\u0142adowe projekty do otwarcia:
+ exdesigndlg.lbl.Openexampledesign = Otwórz projekt przyk\u0142adowy
+ exdesigndlg.lbl.Exampledesignsnotfound = Projekt przyk\u0142adowy nie zosta\u0142 znaleziony.
+ exdesigndlg.lbl.Examplesnotfound = Nie znaleziono przyk\u0142adów
+
+
+ ! Material edit panel
+ matedtpan.but.new = Nowy
+ matedtpan.but.edit = Edytuj
+ matedtpan.but.delete = Usu\u0144
+ matedtpan.but.revertall = Cofnij wszystko
+ matedtpan.col.Material = Materia\u0142
+ matedtpan.col.Type = Typ
+ matedtpan.col.Density = G\u0119sto\u015B\u0107
+ matedtpan.col.but.ttip.New = Dodaj nowy materia\u0142
+ matedtpan.title.Addcustmaterial = Dodaj w\u0142asny materia\u0142
+ matedtpan.but.ttip.edit = Edytuj dodany materia\u0142
+ matedtpan.title.Editmaterial = Edytuj materia\u0142
+ matedtpan.title2.Editmaterial = Materia\u0142y wbudowane nie mog\u0105 by\u0107 modyfikowane.
+ matedtpan.but.ttip.delete = U\u017Cyj materia\u0142u
+ matedtpan.but.ttip.revertall = Usu\u0144 wszystkie materia\u0142y okre\u015Blone przez u\u017Cytkownika
+ matedtpan.title.Deletealluser-defined = Usun\u0105\u0107 wszystkie materia\u0142y okre\u015Blone przez u\u017Cytkownika?
+ matedtpan.title.Revertall = Cofn\u0105\u0107 wszystko?
+ matedtpan.lbl.edtmaterials = Edytowanie materia\u0142ów nie wp\u0142ynie na istniej\u0105ce projekty rakiet.
+
+ !MaterialModel
+ MaterialModel.title.Material = Materia\u0142
+ MaterialModel.title.Defcustmat = Zdefiniuj w\u0142asny materia\u0142
+
+
+ ! Preference dialog
+ pref.dlg.but.add = Dodaj
+ pref.dlg.but.reset = Reset
+ pref.dlg.but.checknow = Sprawd\u017A teraz
+ pref.dlg.but.defaultmetric = Domy\u015Blny system metryczny
+ pref.dlg.but.defaultimperial = Domy\u015Blny system Brytyjski
+ pref.dlg.title.Preferences = Ustawienia
+ pref.dlg.tab.Units = Jednostki
+ pref.dlg.tab.Defaultunits = Jednostki domy\u015Blne
+ pref.dlg.tab.Materials = Materia\u0142y
+ pref.dlg.tab.Custommaterials = Materia\u0142y niestandardowe
+ pref.dlg.tab.Options = Opcje
+ pref.dlg.tab.Miscellaneousoptions = Ró\u017Cne opcje
+ pref.dlg.lbl.Positiontoinsert = Miejsce wstawienia nowych cz\u0119\u015Bci sk\u0142adowych korpusu:
+ pref.dlg.lbl.Confirmdeletion = Potwierd\u017A usuni\u0119cie symulacji:
+ pref.dlg.lbl.User-definedthrust = Krzywe si\u0142y ci\u0105gu okre\u015Blone przez u\u017Cytkownika
+ pref.dlg.lbl.Windspeed = Pr\u0119dko\u015B\u0107 wiatru
+ pref.dlg.Allthrustcurvefiles = Wszystkie pliki krzywych si\u0142y ci\u0105gu (*.eng; *.rse; *.zip; foldery)
+ pref.dlg.RASPfiles = Pliki silnikowe RASP (*.eng)
+ pref.dlg.RockSimfiles = Pliki silnikowe RockSim (*.rse)
+ pref.dlg.ZIParchives = Archiwa ZIP (*.zip)
+ pref.dlg.checkbox.Checkupdates = Wyszukaj dost\u0119pne aktualizacje przy uruchomieniu programu
+ pref.dlg.ttip.Checkupdatesnow = Wyszukaj dost\u0119pne aktualizacje teraz
+ pref.dlg.lbl.Selectprefunits = Wybierz preferowane jednostki:
+ pref.dlg.lbl.Rocketdimensions = Wymiary rakiety:
+ pref.dlg.lbl.Linedensity = G\u0119sto\u015B\u0107 linii:
+ pref.dlg.lbl.Motordimensions = Wymiary silnika:
+ pref.dlg.lbl.Surfacedensity = G\u0119sto\u015B\u0107 powierzchniowa:
+ pref.dlg.lbl.Distance = Odleg\u0142o\u015B\u0107:
+ pref.dlg.lbl.Bulkdensity = Ca\u0142kowita g\u0119sto\u015B\u0107:
+ pref.dlg.lbl.Velocity = Pr\u0119dko\u015B\u0107:
+ pref.dlg.lbl.Surfaceroughness = Nierówno\u015B\u0107 powierzchni:
+ pref.dlg.lbl.Acceleration = Przyspieszenie:
+ pref.dlg.lbl.Area = Powierzchnia:
+ pref.dlg.lbl.Mass = Masa:
+ pref.dlg.lbl.Angle = K\u0105t:
+ pref.dlg.lbl.Force = Si\u0142a:
+ pref.dlg.lbl.Rollrate = Tempo obrotu:
+ pref.dlg.lbl.Totalimpulse = Ca\u0142kowity impuls:
+ pref.dlg.lbl.Temperature = Temperatura:
+ pref.dlg.lbl.Momentofinertia = Moment bezw\u0142adno\u015Bci:
+ pref.dlg.lbl.Pressure = Ci\u015Bnienie:
+ pref.dlg.lbl.Stability = Stabilno\u015B\u0107:
+ pref.dlg.lbl.FlightTime = Czas lotu:
+ pref.dlg.lbl.effect1 = Zmiany zostan\u0105 wprowadzone przy otwarciu kolejnego okna.
+ pref.dlg.lbl.Checkingupdates = Wyszukiwanie aktualizacji...
+ pref.dlg.lbl.msg1 = Wyst\u0105pi\u0142 b\u0142\u0105d podczas komunikacji z serwerem.
+ pref.dlg.lbl.msg2 = Nie mo\u017Cna uzyska\u0107 informacji o aktualizacji
+ pref.dlg.lbl.msg3 = Korzystasz z najnowszej wersji OpenRocket.
+ pref.dlg.lbl.msg4 = Brak dost\u0119pnych aktualizacji
+ pref.dlg.PrefChoiseSelector1 = Zawsze pytaj
+ pref.dlg.PrefChoiseSelector2 = Wstaw w \u015Brodku
+ pref.dlg.PrefChoiseSelector3 = Dodaj na ko\u0144cu
+ pref.dlg.PrefBooleanSelector1 = Usu\u0144
+ pref.dlg.PrefBooleanSelector2 = Potwierd\u017A
+ pref.dlg.Add = Dodaj
+ pref.dlg.DescriptionArea.Adddirectories = Dodaj katalogi, pliki silnikowe RASP (*.eng), Pliki silnikowe RockSim (*.rse) albo archiwa ZIP rozdzielone \u015Brednikiem (;) by za\u0142adowa\u0107 zewn\u0119trzne krzywe si\u0142y ci\u0105gu. Zmiany zostan\u0105 wprowadzone przy kolejnym uruchomieniu OpenRocket.
+
+ PreferencesDialog.lbl.language = J\u0119zyk programu:
+ PreferencesDialog.languages.default = Domy\u015Blny j\u0119zyk systemu
+ PreferencesDialog.lbl.languageEffect = Nowy j\u0119zyk zostanie ustawiony przy kolejnym uruchomieniu OpenRocket.
+
+ ! Simulation edit dialog
+ simedtdlg.but.runsimulation = Przeprowad\u017A symulacj\u0119
+ simedtdlg.but.resettodefault = Przywró\u0107 domy\u015Blny
+ simedtdlg.but.add = Dodaj
+ simedtdlg.but.remove = Usu\u0144
+ simedtdlg.title.Editsim = Edytuj symulacj\u0119
+ simedtdlg.lbl.Simname = Nazwa symulacji:
+ simedtdlg.tab.Launchcond = Warunki startowe
+ simedtdlg.tab.Simopt = Opcje symulacji
+ simedtdlg.tab.Plotdata = Poka\u017C wykres
+ simedtdlg.tab.Exportdata = Eksportuj dane
+ simedtdlg.lbl.Motorcfg = Konfiguracja silnika:
+ simedtdlg.lbl.ttip.Motorcfg = Wybierz konfiguracj\u0119 silnika.
+ simedtdlg.combo.ttip.motorconf = Wybierz konfiguracj\u0119 silnika.
+ simedtdlg.lbl.Wind = Wiatr
+ simedtdlg.lbl.Averwindspeed = \u015Arednia pr\u0119dko\u015B\u0107 wiatru:
+ simedtdlg.lbl.ttip.Averwindspeed = \u015Arednia pr\u0119dko\u015B\u0107 wiatru wzgl\u0119dem powierzchni.
+ simedtdlg.lbl.Stddeviation = Odchylenie standardowe:
+ simedtdlg.lbl.ttip.Stddeviation = <html>Odchylenie standardowe pr\u0119dko\u015Bci wiatru.<br>Pr\u0119dko\u015B\u0107 wiatru jest w zakresie dwukrotnego odchylenia standardowego od warto\u015Bci \u015Bredniej przez 95% czasu.
+ simedtdlg.lbl.Turbulenceintensity = Intensywno\u015B\u0107 turbulencji:
+ simedtdlg.lbl.ttip.Turbulenceintensity1 = <html>Intensywno\u015B\u0107 turbulencji = odchylenie standardowe podzielone przez \u015Bredni\u0105 pr\u0119dko\u015B\u0107 wiatru.<br>
+ simedtdlg.lbl.ttip.Turbulenceintensity2 = Typowe warto\u015Bci w zakresie od
+ simedtdlg.lbl.ttip.Turbulenceintensity3 = do
+ simedtdlg.border.Atmoscond = Warunki atmosferyczne
+ simedtdlg.checkbox.InterStdAtmosphere = Stosuj mi\u0119dzynarodowy standard modelu atmosferycznego
+ simedtdlg.checkbox.ttip.InterStdAtmosphere1 = <html>Wybierz, aby zastosowa\u0107 mi\u0119dzynarodowy standard modelu atmosferycznego.<br>Temperatura w tym modelu wynosi
+ simedtdlg.checkbox.ttip.InterStdAtmosphere2 = ; ci\u015Bnienie
+ simedtdlg.checkbox.ttip.InterStdAtmosphere3 = na poziomie morza.
+ simedtdlg.lbl.Temperature = Temperatura:
+ simedtdlg.lbl.ttip.Temperature = Temperatura w miejscu startu rakiety.
+ simedtdlg.lbl.Pressure = Ci\u015Bnienie:
+ simedtdlg.lbl.ttip.Pressure = Ci\u015Bnienie atmosferyczne punktu startowego.
+ simedtdlg.lbl.Launchsite = Punkt startowy
+ simedtdlg.lbl.Latitude = Szeroko\u015B\u0107 geograficzna:
+ simedtdlg.lbl.ttip.Latitude = <html>Od szeroko\u015Bci geograficznej miejsca startu zale\u017Cy wp\u0142yw przyci\u0105gania ziemskiego na rakiet\u0119.<br>Dodatnie warto\u015Bci znajduj\u0105 si\u0119 na pó\u0142kuli pó\u0142nocnej, ujemne warto\u015Bci na pó\u0142kuli po\u0142udniowej.
+
+ simedtdlg.lbl.Longitude = Dugo\u015B\u0107 geograficzna:
+ simedtdlg.lbl.ttip.Longitude = <html>Wymagane w w przypadku modeli przewiduj\u0105cych warunki pogodowe i modeli wzniesienia.
+
+ simedtdlg.lbl.Altitude = Wysoko\u015B\u0107:
+ simedtdlg.lbl.ttip.Altitude = <html>Wysoko\u015B\u0107 lokalizacji startowej ponad poziomem morza.<br>Wp\u0142ywa na po\u0142o\u017Cenie rakiety w modelu atmosferycznym.
+ simedtdlg.border.Launchrod = Pr\u0119t startowy
+ simedtdlg.lbl.Length = D\u0142ugo\u015B\u0107:
+ simedtdlg.lbl.ttip.Length = D\u0142ugo\u015B\u0107 pr\u0119ta startowego.
+ simedtdlg.lbl.Angle = K\u0105t:
+ simedtdlg.lbl.ttip.Angle = K\u0105t nachylenia pr\u0119ta startowego do pionu.
+ simedtdlg.lbl.Direction = Kierunek:
+ simedtdlg.lbl.ttip.Direction1 = <html>Orientacja pr\u0119ta startowego wzgl\u0119dem wiatru.<br>
+ simedtdlg.lbl.ttip.Direction2 =
+ simedtdlg.lbl.ttip.Direction3 =
+ simedtdlg.border.Simopt = Opcje symulatora
+ simedtdlg.lbl.Calcmethod = Metoda obliczeniowa:
+ simedtdlg.lbl.ttip.Calcmethod = <html>Rozszerzona metoda Barrowmana s\u0142u\u017Cy do obliczania si\u0142 aerodynamicznych zgodnie z <br>równaniami Barrowmana, rozszerzonymi w celu uj\u0119cia wi\u0119kszej liczby cz\u0119\u015Bci sk\u0142adowych modelu.
+ simedtdlg.lbl.ExtBarrowman = Rozszerzona metoda Barrowmana
+ simedtdlg.lbl.Simmethod = Metoda symulacji:
+ simedtdlg.lbl.ttip.Simmethod1 = <html>Symulator uwzgl\u0119dnia sze\u015B\u0107 stopni swobody, co zapewnia ca\u0142kowit\u0105 swobod\u0119 lotu rakiety.<br>
+ simedtdlg.lbl.ttip.Simmethod2 = Integracja jest dokonywana za pomoc\u0105 integracji numerycznej czwartego stopnia Rungego-Kutty 4.
+ simedtdlg.lbl.GeodeticMethod = Obliczenia geodezyjne:
+ simedtdlg.lbl.ttip.GeodeticMethodTip = Dotycz\u0105 obliczania wspó\u0142rz\u0119dnych na kuli ziemskiej. Ta funkcja umo\u017Cliwia równie\u017C obliczanie efektu Coriolisa.
+ simedtdlg.lbl.Timestep = Krok czasowy:
+ simedtdlg.lbl.ttip.Timestep1 = <html>Odst\u0119p czasu pomi\u0119dzy poszczególnymi krokami symulacji.<br>Mniejszy krok czasowy zwi\u0119ksza dok\u0142adno\u015B\u0107 symulacji, ale te\u017C zmniejsza jej szybko\u015B\u0107.<br>
+ simedtdlg.lbl.ttip.Timestep2 = Metoda symulacji czwartego stopnia jest dosy\u0107 dok\u0142adna przy kroku czasowym wynosz\u0105cym
+ simedtdlg.but.ttip.resettodefault = Przywró\u0107 domy\u015Blny krok czasowy (
+ simedtdlg.border.Simlist = Detektory symulacji
+ simedtdlg.txt.longA1 = <html><i>Detektory symulacji</i> s\u0105 zaawansowan\u0105 funkcj\u0105, umo\u017Cliwiaj\u0105c\u0105 U\u017Cytkownikowi zdefiniowanie w\u0142asnych kodów monitoruj\u0105cych proces symulacji i wchodz\u0105cych z ni\u0105 w interakcje.
+ simedtdlg.txt.longA2 = Szczegó\u0142owa instrukcja pisania detektorów symulacji znajduje si\u0119 w dokumentacji technicznej programu OpenRocket.
+ simedtdlg.lbl.Curlist = Bie\u017C\u0105ce detektory symulacji:
+ simedtdlg.lbl.Addsimlist = Dodaj detektor symulacji
+ simedtdlg.lbl.Noflightdata = Brak dost\u0119pnych danych o locie rakiety.
+ simedtdlg.lbl.runsimfirst = Prosz\u0119 najpierw przeprowadzi\u0107 symulacj\u0119.
+ simedtdlg.chart.Simflight = Lot symulowany
+ simedtdlg.dlg.Simres = Wyniki symulacji
+ simedtdlg.IntensityDesc.None = Brak
+ simedtdlg.IntensityDesc.Verylow = Bardzo niski
+ simedtdlg.IntensityDesc.Low = Niski
+ simedtdlg.IntensityDesc.Medium = \u015Aredni
+ simedtdlg.IntensityDesc.High = Wysoki
+ simedtdlg.IntensityDesc.Veryhigh = Bardzo Wysoki
+ simedtdlg.IntensityDesc.Extreme = Ekstremum
+
+ GeodeticComputationStrategy.flat.name = P\u0142aska ziemia
+ GeodeticComputationStrategy.flat.desc = Obliczenia przy za\u0142o\u017Ceniu, \u017Ce powierzchnia kuli ziemskiej jest p\u0142aska. Wystarczaj\u0105ce dolotów na niskie wysoko\u015Bci.
+ GeodeticComputationStrategy.spherical.name = Aproksymacja sferyczna
+ GeodeticComputationStrategy.spherical.desc = <html>Obliczenia geodezyjne przy za\u0142o\u017Ceniu, \u017Ce Ziemia ma kszta\u0142t sfery.<br>Ta metoda jest wystarczaj\u0105co dok\u0142adna niemal w ka\u017Cdym przypadku.
+ GeodeticComputationStrategy.wgs84.name = Elipsoida WGS-84
+ GeodeticComputationStrategy.wgs84.desc = <html>Obliczenia geodezyjne metod\u0105 Vincentego w uk\u0142adzie elipsoidalnym WGS-84.<br>Powolne i w wi\u0119kszo\u015Bci przypadków niepotrzebne.
+
+
+
+
+ ! Simulation Panel
+ simpanel.but.newsimulation = Nowa symulacja
+ simpanel.but.editsimulation = Edytuj symulacj\u0119
+ simpanel.but.runsimulations = Przeprowad\u017A symulacj\u0119
+ simpanel.but.deletesimulations = Usu\u0144 symulacje
+ simpanel.but.plotexport = Rysuj wykres / eksportuj
+ simpanel.but.ttip.newsimulation = Dodaj nowa symulacj\u0119
+ simpanel.but.ttip.editsim = Edytuj zaznaczon\u0105 symulacj\u0119
+ simpanel.but.ttip.runsimu = Powtórz zaznaczon\u0105 symulacj\u0119
+ simpanel.but.ttip.deletesim = Usu\u0144 zaznaczone symulacje
+ simpanel.checkbox.donotask = Nie pytaj ponownie
+ simpanel.lbl.defpref = Domy\u015Bln\u0105 operacj\u0119 mo\u017Cna zmieni\u0107 w ustawieniach.
+ simpanel.dlg.lbl.DeleteSim1 = Usun\u0105\u0107 zaznaczone symulacje?
+ simpanel.dlg.lbl.DeleteSim2 = <html><i>Tej operacji nie mo\u017Cna cofn\u0105\u0107.</i>
+ simpanel.dlg.lbl.DeleteSim3 = Usu\u0144 symulacje
+ simpanel.col.Name = Nazwa
+ simpanel.col.Motors = Silniki
+ simpanel.col.Velocityoffrod = Pr\u0119dko\u015B\u0107 zej\u015Bcia z wyrzutni
+ simpanel.col.Velocityatdeploy = Pr\u0119dko\u015B\u0107 w chwili aktywacji UWS
+ simpanel.col.Apogee = Apogeum
+ simpanel.col.Maxvelocity = Maksymalna pr\u0119dko\u015B\u0107
+ simpanel.col.Maxacceleration = Maksymalne przyspieszenie
+ simpanel.col.Timetoapogee = Czas do apogeum
+ simpanel.col.Flighttime = Czas lotu
+ simpanel.col.Groundhitvelocity = Pr\u0119dko\u015B\u0107 przyziemienia
+
+ ! SimulationRunDialog
+ SimuRunDlg.title.RunSim = Symulacje w trakcie...
+ SimuRunDlg.lbl.Running = Symulacja aktywna...
+ SimuRunDlg.lbl.Simutime = Czas symulacji:
+ SimuRunDlg.lbl.Altitude = Wysoko\u015B\u0107:
+ SimuRunDlg.lbl.Velocity = Pr\u0119dko\u015B\u0107:
+ SimuRunDlg.msg.Unabletosim = Nie mo\u017Cna przeprowadzi\u0107 symulacji:
+ SimuRunDlg.msg.errorOccurred = Wyst\u0105pi\u0142 b\u0142\u0105d podczas symulacji.
+ SimuRunDlg.msg.AnException1 = Wyst\u0105pi\u0142 wyj\u0105tek podczas symulacji:
+ SimuRunDlg.msg.AnException2 = Prosz\u0119 zg\u0142osi\u0107 to jako b\u0142\u0105d oraz poda\u0107 szczegó\u0142y.
+ SimuRunDlg.msg.AssertionError1 = Podczas symulacji wyst\u0105pi\u0142 b\u0142\u0105d obliczeniowy.
+ SimuRunDlg.msg.AssertionError2 = Prosz\u0119 zg\u0142osi\u0107 to jako b\u0142\u0105d oraz poda\u0107 szczegó\u0142y.
+ SimuRunDlg.msg.unknownerror1 = Podczas symulacji wyst\u0105pi\u0142 nieznany b\u0142\u0105d.
+ SimuRunDlg.msg.unknownerror2 = Program mo\u017Ce by\u0107 niestabilny. Zapisz wszystkie projekty i uruchom ponownie OpenRocket!
+
+
+ RK4SimulationStepper.error.valuesTooLarge = Warto\u015Bci w symulacji wykroczy\u0142y poza dopuszczalne granice. Spróbuj ustawi\u0107 mniejszy krok czasowy.
+
+
+ ! SimulationExportPanel
+ SimExpPan.desc = Pliki rozdzielone przecinkiem (*.csv)
+ SimExpPan.border.Vartoexport = Zmienne do wyeksportowania
+ SimExpPan.but.Selectall = Wybierz wszystko
+ SimExpPan.but.Selectnone = Odznacz wszystko
+ SimExpPan.border.Fieldsep = Separator pól
+ SimExpPan.lbl.Fieldsepstr = Ci\u0105g znaków - separator pól:
+ SimExpPan.lbl.longA1 = <html>Ci\u0105g znaków stosowany do oddzielania pól w eksportowanym pliku.<br>
+ SimExpPan.lbl.longA2 = W przypadku pliku CSV u\u017Cyj przecinka (",").
+ SimExpPan.checkbox.Includesimudesc = Dodaj opis symulacji
+ SimExpPan.checkbox.ttip.Includesimudesc = Dodaj komentarz opisuj\u0105cy symulacj\u0119 na pocz\u0105tku pliku.
+ SimExpPan.border.Comments = Komentarze
+ SimExpPan.checkbox.Includefielddesc = Dodaj opisy pól
+ SimExpPan.checkbox.ttip.Includefielddesc = Dodaj wiersz komentarza z opisem eksportowanych zmiennych.
+ SimExpPan.checkbox.Incflightevents = Dodaj zdarzenia lotu
+ SimExpPan.checkbox.ttip.Incflightevents = Dodaj wiersz komentarza do ka\u017Cdego zdarzenia lotu.
+ SimExpPan.lbl.Commentchar = Znak komentarza:
+ SimExpPan.lbl.ttip.Commentchar = Znak(i) sygnalizuj\u0105cy(e) komentarz.
+ SimExpPan.but.Exporttofile = Eksportuj do pliku...
+ SimExpPan.Fileexists.desc1 = Plik \"
+ SimExpPan.Fileexists.desc2 = \" istnieje. Nadpisa\u0107?
+ SimExpPan.Fileexists.title = Plik ju\u017C istnieje
+ SimExpPan.ExportingVar.desc1 = Eksportuj\u0119 1 zmienn\u0105 z
+ SimExpPan.ExportingVar.desc2 = Eksportuj\u0119
+ SimExpPan.ExportingVar.desc3 = zmienne z
+ SimExpPan.Col.Variable = Zmienna
+ SimExpPan.Col.Unit = Jednostka
+
+
+ CsvOptionPanel.separator.space = SPACJA
+ CsvOptionPanel.separator.tab = TABULATOR
+
+
+
+ ! MotorPlot
+ MotorPlot.title.Motorplot = Wykres silnika
+ MotorPlot.but.Select = Wybierz
+ MotorPlot.Chart.Motorthrustcurve = Krzywa si\u0142y ci\u0105gu silnika
+ MotorPlot.Chart.Time = Czas / s
+ MotorPlot.Chart.Thrust = Si\u0142a ci\u0105gu / N
+ MotorPlot.txt.Designation = Oznaczenie:
+ MotorPlot.txt.Manufacturer = Producent:
+ MotorPlot.txt.Type = Typ:
+ MotorPlot.txt.Delays = Opó\u017Anienia:
+ MotorPlot.txt.Comment = Komentarz:\n
+
+
+
+ ! Simulation plot panel
+ simplotpanel.lbl.Presetplotconf = Standardowe ustawienia wykresu:
+ simplotpanel.lbl.Xaxistype = Typ osi X:
+ simplotpanel.lbl.Unit = Jednostka:
+ simplotpanel.lbl.Yaxistypes = Typy osi Y:
+ simplotpanel.lbl.Flightevents = Wydarzenia lotu:
+ simplotpanel.but.All = Wszystkie
+ simplotpanel.but.None = \u017Badne
+ simplotpanel.but.NewYaxisplottype = Nowy typ osi Y
+ simplotpanel.but.Plotflight = Narysuj wykres lotu
+ simplotpanel.lbl.Axis = O\u015B:
+ simplotpanel.but.ttip.Removethisplot = Usu\u0144 ten wykres
+ simplotpanel.Desc = Dane zostan\u0105 umieszczone na wykresie w porz\u0105dku chronologicznym, nawet je\u017Celi o\u015B X nie jest typu czasowego.
+ simplotpanel.OptionPane.lbl1 = Maksymalna liczba wykresów to 15.
+ simplotpanel.OptionPane.lbl2 = Nie mo\u017Cna doda\u0107 wykresu
+ simplotpanel.AUTO_NAME = Auto
+ simplotpanel.LEFT_NAME = Lewo
+ simplotpanel.RIGHT_NAME = Prawo
+ simplotpanel.CUSTOM = Dowolny
+ SimulationPlotPanel.error.noPlotSelected = Dodaj co najmniej jedn\u0105 zmienn\u0105 do umieszczenia na osi Y.
+ SimulationPlotPanel.error.noPlotSelected.title = Brak danych nadaj\u0105cych si\u0119 do stworzenia wykresu
+
+
+ ! Component add buttons
+ compaddbuttons.Bodycompandfinsets = Cz\u0119\u015Bci sk\u0142adowe korpusu i zestawy stateczników
+ compaddbuttons.Nosecone = G\u0142owica
+ compaddbuttons.Bodytube = Korpus rakiety
+ compaddbuttons.Transition = Talia przej\u015Bciowa
+ compaddbuttons.Trapezoidal = Trapezoidalny
+ compaddbuttons.Elliptical = Eliptyczny
+ compaddbuttons.Freeform = Kszta\u0142t niestandardowy
+ compaddbuttons.Launchlug = Zaczep startowy
+ compaddbuttons.Innercomponent = Cz\u0119\u015B\u0107 wewn\u0119trzna
+ compaddbuttons.Innertube = Rura wewn\u0119trzna
+ compaddbuttons.Coupler = \u0141\u0105cznik
+ compaddbuttons.Centeringring = Pier\u015Bcie\u0144\ncentruj\u0105cy
+ compaddbuttons.Bulkhead = Przegroda
+ compaddbuttons.Engineblock = Blokada\nsilnika
+ compaddbuttons.Massobjects = Balasty
+ compaddbuttons.Parachute = Spadochron
+ compaddbuttons.Streamer = Ta\u015Bma
+ compaddbuttons.Shockcord = Linka amortyzuj\u0105ca
+ compaddbuttons.Masscomponent = Balast\n
+ compaddbuttons.Donotaskmeagain = Nie pytaj ponownie
+ compaddbuttons.Selectcomppos = Wybierz po\u0142o\u017Cenie cz\u0119\u015Bci
+ compaddbuttons.lbl.Youcanchange = Domy\u015Bln\u0105 operacj\u0119 mo\u017Cna zmieni\u0107 w ustawieniach.
+ compaddbuttons.lbl.insertcomp = Wstawi\u0107 cz\u0119\u015B\u0107 za obecn\u0105 cz\u0119\u015Bci\u0105, czy na ko\u0144cu?
+ compaddbuttons.askPosition.Inserthere = Wstaw tutaj
+ compaddbuttons.askPosition.Addtotheend = Dodaj na ko\u0144cu
+ compaddbuttons.askPosition.Cancel = Anuluj
+
+ ! Component Analysis Dialog
+ componentanalysisdlg.componentanalysis = Analiza cz\u0119\u015Bci
+ componentanalysisdlg.lbl.winddir = Kierunek wiatru:
+ componentanalysisdlg.TitledBorder.warnings = Ostrze\u017Cenia:
+ componentanalysisdlg.ToggleBut.worst = Najgorszy
+ componentanalysisdlg.lbl.angleofattack = K\u0105t natarcia:
+ componentanalysisdlg.lbl.machnumber = Liczba Macha:
+ componentanalysisdlg.lbl.rollrate = Tempo obrotu:
+ componentanalysisdlg.lbl.activestages = Aktywne stopnie:
+ componentanalysisdlg.lbl.motorconf = Konfiguracja silnika:
+ componentanalysisdlg.TabStability.Col = Cz\u0119\u015B\u0107
+ componentanalysisdlg.TabStability = Stabilno\u015B\u0107
+ componentanalysisdlg.TabStability.ttip = Informacje dotycz\u0105ce stabilno\u015Bci
+ componentanalysisdlg.dragTableModel.Col.Component = Cz\u0119\u015B\u0107
+ componentanalysisdlg.dragTableModel.Col.Pressure = <html>Ci\u015Bnienie C<sub>D</sub>
+ componentanalysisdlg.dragTableModel.Col.Base = <html>Baza C<sub>D</sub>
+ componentanalysisdlg.dragTableModel.Col.friction = <html>Tarcie C<sub>D</sub>
+ componentanalysisdlg.dragTableModel.Col.total = <html>Razem C<sub>D</sub>
+ componentanalysisdlg.dragTabchar = Charakterystyka oporu
+ componentanalysisdlg.dragTabchar.ttip = Charakterystyka oporu
+ componentanalysisdlg.rollTableModel.Col.component = Cz\u0119\u015B\u0107
+ componentanalysisdlg.rollTableModel.Col.rollforc = Wspó\u0142czynnik wymuszania obrotu
+ componentanalysisdlg.rollTableModel.Col.rolldamp = Wspó\u0142czynnik hamowania obrotu
+ componentanalysisdlg.rollTableModel.Col.total = <html>Razem C<sub>I</sub>
+ componentanalysisdlg.rollTableModel = Dynamika obrotu
+ componentanalysisdlg.rollTableModel.ttip = Dynamika obrotu
+ componentanalysisdlg.println.closingmethod = Metoda zamykania:
+ componentanalysisdlg.println.settingnam = USTAWIANIE WARTO\u015ACI NAN
+ componentanalysisdlg.lbl.reflenght = D\u0142ugo\u015B\u0107 wzorcowa:
+ componentanalysisdlg.lbl.refarea = Powierzchnia wzorcowa:
+ !componentanalysisdlg.But.close
+ componentanalysisdlg.TabStability.Col.Component = Cz\u0119\u015B\u0107
+
+ ! Custom Material dialog
+ custmatdlg.title.Custommaterial = Materia\u0142 niestandardowy
+ custmatdlg.lbl.Materialname = Nazwa materia\u0142u:
+ custmatdlg.lbl.Materialtype = Rodzaj materia\u0142u:
+ custmatdlg.lbl.Materialdensity = G\u0119sto\u015B\u0107 materia\u0142u:
+ custmatdlg.checkbox.Addmaterial = Dodaj materia\u0142 do bazy danych
+
+
+ ! Ring Component Config
+ ringcompcfg.OuterRadius = Promie\u0144 zewn\u0119trzny
+ ringcompcfg.Automatic = Automatyczne
+ ringcompcfg.InnerRadius = Promie\u0144 wewn\u0119trzny
+ ringcompcfg.Thickness = Grubo\u015B\u0107
+ ringcompcfg.Length = D\u0142ugo\u015B\u0107
+ ringcompcfg.Positionrelativeto = Po\u0142o\u017Cenie wzgl\u0119dem:
+ ringcompcfg.plus = plus
+ ringcompcfg.PositionValue = Warto\u015B\u0107 po\u0142o\u017Cenia
+ ringcompcfg.Radialdistance = Odleg\u0142o\u015B\u0107 wzgl\u0119dem \u015Brodka:
+ ringcompcfg.Distancefrom = Odleg\u0142o\u015B\u0107 od osi centralnej rakiety
+ ringcompcfg.Radialdirection = Kierunek wzgl\u0119dem \u015Brodka:
+ ringcompcfg.radialdirectionfrom = Kierunek prostopad\u0142y do osi centralnej rakiety
+ ringcompcfg.but.Reset = Reset
+ ringcompcfg.but.Resetcomponant = Resetuj po\u0142o\u017Cenie cz\u0119\u015Bci wzgl\u0119dem osi rakiety
+ ringcompcfg.EngineBlock.desc = <html><b>Blokada silnika</b> unieruchamia silnik wewn\u0105trz elementu pe\u0142ni\u0105cego funkcj\u0119 gniazda silnikowego.<br><br>Aby doda\u0107 silnik, stwórz najpierw <b>Korpus rakiety</b> lub <b>rur\u0119 wewn\u0119trzn\u0105</b> i oznacz j\u0105 jako gniazdo silnika w zak\u0142adce <em>Silnik</em>.
+ ringcompcfg.note.desc = Uwaga: Rura wewn\u0119trzna nie wp\u0142ywa na aerodynamik\u0119 rakiety, nawet je\u017Celi znajduje si\u0119 poza korpusem.
+
+
+ ! Body Tube Config
+ BodyTubecfg.lbl.Bodytubelength = D\u0142ugo\u015B\u0107 korpusu:
+ BodyTubecfg.lbl.Outerdiameter = \u015Arednica zewn\u0119trzna:
+ BodyTubecfg.lbl.Innerdiameter = \u015Arednica wewn\u0119trzna:
+ BodyTubecfg.lbl.Wallthickness = Grubo\u015B\u0107 \u015Bciany:
+ BodyTubecfg.tab.General = Ogólne
+ BodyTubecfg.tab.Generalproperties = Ogólne w\u0142a\u015Bciwo\u015Bci
+ BodyTubecfg.tab.Motor = Silnik
+ BodyTubecfg.tab.Motormountconf = Konfiguracja gniazda silnika
+ BodyTubecfg.checkbox.Automatic = Auto
+ BodyTubecfg.checkbox.Filled = Wype\u0142nione
+
+ ! FinSetConfig
+ FinSetConfig.tab.Fintabs = Wypustki statecznika
+ FinSetConfig.tab.Through-the-wall = Wypustki przez\u015Bcienne stateczników
+ FinSetConfig.but.Converttofreeform = Zamie\u0144 na kszta\u0142t niestandardowy
+ FinSetConfig.but.Converttofreeform.ttip = Zmie\u0144 bie\u017C\u0105cy zestaw stateczników na niestandardowy
+ FinSetConfig.Convertfinset = Zmie\u0144 zestaw stateczników
+ FinSetConfig.but.Splitfins = Rozdziel stateczniki
+ FinSetConfig.but.Splitfins.ttip = Rozdziel zestaw stateczników na pojedyncze stateczniki
+ FinSetConfig.but.AutoCalc = Oblicz automatycznie
+ FinSetConfig.lbl.Through-the-wall = Wypustki przez\u015Bcienne stateczników:
+ FinSetConfig.lbl.Tablength = Dugo\u015B\u0107 wypustki
+ FinSetConfig.ttip.Tablength = D\u0142ugo\u015B\u0107 wypustki statecznika.
+ FinSetConfig.lbl.Tabheight = Wysoko\u015B\u0107 wypustki
+ FinSetConfig.ttip.Tabheight = Wysoko\u015B\u0107 wypustki statecznika w p\u0142aszczy\u017Anie prostopad\u0142ej do korpusu.
+ FinSetConfig.lbl.Tabposition = Po\u0142o\u017Cenie wypustki:
+ FinSetConfig.ttip.Tabposition = Po\u0142o\u017Cenie wypustki statecznika.
+ FinSetConfig.lbl.relativeto = w stosunku do
+
+ !FinMarkingGuide
+ FinMarkingGuide.lbl.Front = Przód
+
+ ! MotorDatabaseLoadingDialog
+ MotorDbLoadDlg.title = Wgrywanie silników
+ MotorDbLoadDlg.Loadingmotors = Wgrywanie silników...
+
+ ! RocketConfig
+ RocketCfg.lbl.Designname = Nazwa projektu:
+ RocketCfg.lbl.Designer = Projektant:
+ RocketCfg.lbl.Comments = Uwagi:
+ RocketCfg.lbl.Revisionhistory = Historia zmian:
+ RocketCfg.lbl.Material = Materia\u0142:
+
+ ! ShockCordConfig
+ ShockCordCfg.lbl.Shockcordlength = D\u0142ugo\u015B\u0107 linki amortyzuj\u0105cej
+
+ ! RocketComponentConfig
+ RocketCompCfg.lbl.Componentname = Nazwa cz\u0119\u015Bci:
+ RocketCompCfg.ttip.Thecomponentname = Nazwa cz\u0119\u015Bci sk\u0142adowej rakiety.
+ RocketCompCfg.tab.Override = Wymu\u015B
+ RocketCompCfg.tab.MassandCGoverride = Opcje wymuszenia ci\u0119\u017Caru oraz \u015Brodka ci\u0119\u017Cko\u015Bci
+ RocketCompCfg.tab.Figure = Wygl\u0105d
+ RocketCompCfg.tab.Figstyleopt = Styl kszta\u0142tu
+ RocketCompCfg.tab.Comment = Uwagi
+ RocketCompCfg.tab.Specifyacomment = Dodaj uwagi do cz\u0119\u015Bci
+ RocketCompCfg.lbl.Mass = Masa:
+ RocketCompCfg.lbl.Componentmass = Masa cz\u0119\u015Bci:
+ RocketCompCfg.lbl.overriddento = (wymuszone do
+ RocketCompCfg.lbl.overriddenby = (wymuszone przez
+ RocketCompCfg.lbl.Componentmaterial = Materia\u0142 cz\u0119\u015Bci:
+ RocketCompCfg.lbl.Componentfinish = Wyko\u0144czenie cz\u0119\u015Bci:
+ RocketCompCfg.lbl.ttip.componentmaterialaffects = Materia\u0142 cz\u0119\u015Bci ma wp\u0142yw na jej ci\u0119\u017Car.
+ RocketCompCfg.combo.ttip.componentmaterialaffects = Materia\u0142 cz\u0119\u015Bci ma wp\u0142yw na jej ci\u0119\u017Car.
+ RocketCompCfg.lbl.longA1 = <html>Wyko\u0144czenie cz\u0119\u015Bci ma wp\u0142yw na jej opór aerodynamiczny.<br>
+ RocketCompCfg.lbl.longA2 = Wskazana warto\u015B\u0107 okre\u015Bla przeci\u0119tn\u0105 chropowato\u015B\u0107 powierzchni.
+ RocketCompCfg.but.Setforall = Ustaw dla wszystkich
+ RocketCompCfg.but.ttip.Setforall = Nadaj to wyko\u0144czenie wszystkim cz\u0119\u015Bci\u0105 sk\u0142adow\u0105 rakiety.
+ RocketCompCfg.lbl.Overridemassorcenter = Wymu\u015B ci\u0119\u017Car b\u0105d\u017A \u015Brodek ci\u0119\u017Cko\u015Bci dla
+ RocketCompCfg.checkbox.Overridemass = Wymu\u015B ci\u0119\u017Car:
+ RocketCompCfg.checkbox.Overridecenterofgrav = Wymu\u015B \u015Brodek ci\u0119\u017Cko\u015Bci:
+ RocketCompCfg.checkbox.OverridemassandCG = Wymu\u015B ci\u0119\u017Car oraz \u015Brodek ci\u0119\u017Cko\u015Bci wszystkich dodatkowych cz\u0119\u015Bci sk\u0142adowych
+ RocketCompCfg.lbl.longB1 = <html>Wymuszony ci\u0119\u017Car nie uwzgl\u0119dnia silników.<br>
+ RocketCompCfg.lbl.longB2 = \u015Arodek ci\u0119\u017Cko\u015Bci jest mierzony od przodu
+ RocketCompCfg.lbl.Commentsonthe = Uwagi -
+ RocketCompCfg.lbl.Figurestyle = Styl wygl\u0105du:
+ RocketCompCfg.lbl.Componentcolor = Kolor cz\u0119\u015Bci:
+ RocketCompCfg.lbl.Choosecolor = Wybierz kolor
+ RocketCompCfg.checkbox.Usedefaultcolor = Ustaw kolor domy\u015Blny
+ RocketCompCfg.lbl.Complinestyle = Styl linii:
+ RocketCompCfg.but.Saveasdefstyle = Zapisz jako styl domy\u015Blny
+ RocketCompCfg.lbl.Diameter = \u015Arednica:
+ RocketCompCfg.lbl.Length = D\u0142ugo\u015B\u0107:
+ RocketCompCfg.lbl.Thickness = Grubo\u015B\u0107:
+ RocketCompCfg.checkbox.Endcapped = Zasklepiony koniec
+ RocketCompCfg.ttip.Endcapped = Czy koniec wpustu jest zasklepiony.
+ RocketCompCfg.title.Noseconeshoulder = Wpust g\u0142owicy
+ RocketCompCfg.title.Aftshoulder = Wpust tylny
+ RocketCompCfg.border.Foreshoulder = Wpust przedni
+ !RocketCompCfg.lbl.Length
+
+ ! BulkheadConfig
+ BulkheadCfg.tab.Diameter = \u015Arednica:
+ BulkheadCfg.tab.Thickness = Grubo\u015B\u0107:
+ BulkheadCfg.tab.General = Ogólne
+ BulkheadCfg.tab.Generalproperties = W\u0142a\u015Bciwo\u015Bci ogólne
+
+ !CenteringRingConfig
+ CenteringRingCfg.tab.Outerdiam = \u015Arednica zewn\u0119trzna:
+ CenteringRingCfg.tab.Innerdiam = \u015Arednica wewn\u0119trzna:
+ CenteringRingCfg.tab.Thickness = Grubo\u015B\u0107:
+ CenteringRingCfg.tab.General = Ogólne
+ CenteringRingCfg.tab.Generalproperties = W\u0142a\u015Bciwo\u015Bci ogólne
+
+ !ComponentConfigDialog
+ ComponentCfgDlg.configuration = konfiguracja
+ ComponentCfgDlg.configuration1 =
+ ComponentCfgDlg.Modify = Zmodyfikuj
+
+ !StageConfig
+ StageConfig.tab.Separation = Separacja
+ StageConfig.tab.Separation.ttip = Opcje oddzielenia cz\u0142onu
+ StageConfig.separation.lbl.title = Ustal moment oddzielenia cz\u0142onu:
+ StageConfig.separation.lbl.plus = plus
+ StageConfig.separation.lbl.seconds = sek.
+
+ !EllipticalFinSetConfig
+ EllipticalFinSetCfg.Nbroffins = Liczba stateczników:
+ EllipticalFinSetCfg.Rotation = Rotacja:
+ EllipticalFinSetCfg.Fincant = Nachylenie stateczników:
+ EllipticalFinSetCfg.Rootchord = Kraw\u0119d\u017A podstawy:
+ EllipticalFinSetCfg.Height = Wysoko\u015B\u0107:
+ EllipticalFinSetCfg.Positionrelativeto = Po\u0142o\u017Cenie wzgl\u0119dem:
+ EllipticalFinSetCfg.plus = plus
+ EllipticalFinSetCfg.FincrossSection = Przekrój statecznika:
+ EllipticalFinSetCfg.Thickness = Grubo\u015B\u0107:
+ EllipticalFinSetCfg.General = Ogólne
+ EllipticalFinSetCfg.Generalproperties = W\u0142a\u015Bciwo\u015Bci ogólne
+ EllipticalFinSetCfg.ttip.Fincant = K\u0105t nachylenia stateczników wzgl\u0119dem korpusu.
+
+ !FreeformFinSetConfig
+ FreeformFinSetCfg.tab.General = Ogólne
+ FreeformFinSetCfg.tab.ttip.General = W\u0142a\u015Bciwo\u015Bci ogólne
+ FreeformFinSetCfg.tab.Shape = Kszta\u0142t
+ FreeformFinSetCfg.tab.ttip.Finshape = Kszta\u0142t stateczników
+ FreeformFinSetCfg.lbl.Numberoffins = Liczba stateczników:
+ FreeformFinSetCfg.lbl.Finrotation = Rotacja stateczników:
+ FreeformFinSetCfg.lbl.Fincant = Nachylenie stateczników:
+ FreeformFinSetCfg.lbl.ttip.Fincant = K\u0105t nachylenia stateczników wzgl\u0119dem korpusu.
+ FreeformFinSetCfg.lbl.Posrelativeto = Po\u0142o\u017Cenie wzgl\u0119dem:
+ FreeformFinSetCfg.lbl.plus = plus
+ FreeformFinSetCfg.lbl.FincrossSection = Przekrój statecznika:
+ FreeformFinSetCfg.lbl.Thickness = Grubo\u015B\u0107:
+ ! doubleClick1 + 2 form the message "Double-click to edit", split approximately at the middle
+ FreeformFinSetConfig.lbl.doubleClick1 = Kliknij dwukrotnie
+ FreeformFinSetConfig.lbl.doubleClick2 = aby edytowa\u0107
+ FreeformFinSetConfig.lbl.clickDrag = Kliknij i przeci\u0105gnij: Dodaj i przesuwaj punkty
+ FreeformFinSetConfig.lbl.ctrlClick = Ctrl+klik: Usu\u0144 punkt
+ FreeformFinSetConfig.lbl.scaleFin = Skaluj statecznik
+
+
+ !InnerTubeConfig
+ InnerTubeCfg.tab.Motor = Silnik
+ InnerTubeCfg.tab.ttip.Motor = Konfiguracja gniazda silnika
+ InnerTubeCfg.tab.Cluster = Grupa
+ InnerTubeCfg.tab.ttip.Cluster = Konfiguracja grupy
+ InnerTubeCfg.tab.Radialpos = Po\u0142o\u017Cenie wzgl\u0119dem \u015Brodka
+ InnerTubeCfg.tab.ttip.Radialpos = Po\u0142o\u017Cenie wzgl\u0119dem \u015Brodka
+ InnerTubeCfg.lbl.Selectclustercfg = Wybierz konfiguracj\u0119 grupy:
+ InnerTubeCfg.lbl.TubeSep = Separacja rur:
+ InnerTubeCfg.lbl.ttip.TubeSep = Separacja rur, 1,0
+ InnerTubeCfg.lbl.Rotation = Rotacja:
+ InnerTubeCfg.lbl.ttip.Rotation = Konfiguracja k\u0105ta rotacji grupy
+ InnerTubeCfg.lbl.Rotangle = Konfiguracja k\u0105ta rotacji grupy
+ InnerTubeCfg.but.Splitcluster = Rozdziel grup\u0119
+ InnerTubeCfg.lbl.longA1 = <html>Rozdziel grup\u0119 na oddzielne cz\u0119\u015Bci.<br>
+ InnerTubeCfg.lbl.longA2 = To polecenie powoduje równie\u017C duplikacj\u0119 wszystkich cz\u0119\u015Bci do\u0142\u0105czonych do danej rury wewn\u0119trznej.
+ InnerTubeCfg.but.Resetsettings = Przywró\u0107 ustawienia domy\u015Blne
+ InnerTubeCfg.but.ttip.Resetsettings = Przywró\u0107 oddzielenie oraz rotacje do ich warto\u015Bci domy\u015Blnych
+
+ ! LaunchLugConfig
+ LaunchLugCfg.lbl.Length = D\u0142ugo\u015B\u0107:
+ LaunchLugCfg.lbl.Outerdiam = \u015Arednica zewn\u0119trzna:
+ LaunchLugCfg.lbl.Innerdiam = \u015Arednica wewn\u0119trzna:
+ LaunchLugCfg.lbl.Thickness = Grubo\u015B\u0107:
+ LaunchLugCfg.lbl.Radialpos = Po\u0142o\u017Cenie wzgl\u0119dem \u015Brodka:
+ LaunchLugCfg.lbl.Posrelativeto = Po\u0142o\u017Cenie wzgl\u0119dem:
+ LaunchLugCfg.lbl.plus = plus
+ LaunchLugCfg.tab.General = Ogólne
+ LaunchLugCfg.tab.Generalprop = W\u0142a\u015Bciwo\u015Bci ogólne
+
+ ! MassComponentConfig
+ MassComponentCfg.lbl.Mass = Masa:
+ MassComponentCfg.lbl.Length = D\u0142ugo\u015B\u0107:
+ MassComponentCfg.lbl.Diameter = \u015Arednica:
+ MassComponentCfg.lbl.PosRelativeto = Po\u0142o\u017Cenie wzgl\u0119dem:
+ MassComponentCfg.lbl.plus = plus
+ MassComponentCfg.tab.General = Ogólne
+ MassComponentCfg.tab.ttip.General = W\u0142a\u015Bciwo\u015Bci ogólne
+ MassComponentCfg.tab.Radialpos = Po\u0142o\u017Cenie wzgl\u0119dem \u015Brodka
+ MassComponentCfg.tab.ttip.Radialpos = Konfiguracja po\u0142o\u017Cenia wzgl\u0119dem \u015Brodka
+ MassComponentCfg.lbl.Radialdistance = Odleg\u0142o\u015B\u0107 wzgl\u0119dem \u015Brodka:
+ MassComponentCfg.lbl.Radialdirection = Kierunek wzgl\u0119dem \u015Brodka:
+ MassComponentCfg.but.Reset = Reset
+
+ ! MotorConfig
+ MotorCfg.checkbox.compmotormount = Ta cz\u0119\u015B\u0107 jest gniazdem silnika
+ MotorCfg.lbl.Motorcfg = Konfiguracja silnika:
+ MotorCfg.but.New = Nowy
+ MotorCfg.lbl.Currentmotor = Obecny silnik:
+ MotorCfg.lbl.Motoroverhang = Wysuni\u0119cie silnika:
+ MotorCfg.lbl.Ignitionat = Zap\u0142on w chwili:
+ MotorCfg.lbl.plus = plus
+ MotorCfg.lbl.seconds = sek.
+ MotorCfg.lbl.longA1 = Obecny model ma tylko jeden stopie\u0144.
+ MotorCfg.lbl.longA2 = Stopnie mog\u0105 by\u0107 dodawane poprzez klikni\u0119cie \"Nowy stopie\u0144\".
+ MotorCfg.lbl.longB1 = Obecny model ma
+ MotorCfg.lbl.longB2 = stopnie.
+ MotorCfg.but.Selectmotor = Wybierz silnik
+ MotorCfg.but.Removemotor = Usu\u0144 silnik
+ MotorCfg.lbl.motorLabel = \u017Badne
+
+ ! NoseConeConfig
+ NoseConeCfg.lbl.Noseconeshape = Kszta\u0142t g\u0142owicy:
+ NoseConeCfg.lbl.Shapeparam = Parametr kszta\u0142tu
+ NoseConeCfg.lbl.Noseconelength = D\u0142ugo\u015B\u0107 g\u0142owicy:
+ NoseConeCfg.lbl.Basediam = \u015Arednica podstawy:
+ NoseConeCfg.checkbox.Automatic = Auto
+ NoseConeCfg.lbl.Wallthickness = Grubo\u015B\u0107 \u015Bciany:
+ NoseConeCfg.checkbox.Filled = Wype\u0142nione
+ NoseConeCfg.tab.General = Ogólne
+ NoseConeCfg.tab.ttip.General = W\u0142a\u015Bciwo\u015Bci ogólne
+ NoseConeCfg.tab.Shoulder = Wpust
+ NoseConeCfg.tab.ttip.Shoulder = Parametry wpustu
+
+ ! ParachuteConfig
+ ParachuteCfg.lbl.Canopy = Czasza:
+ ParachuteCfg.lbl.Diameter = \u015Arednica:
+ ParachuteCfg.lbl.Material = Materia\u0142:
+ ParachuteCfg.combo.MaterialModel = Materia\u0142 cz\u0119\u015Bci ma wp\u0142yw na jej ci\u0119\u017Car.
+ ParachuteCfg.lbl.longA1 = <html>Wspó\u0142czynnik oporu C<sub>D</sub>
+ ParachuteCfg.lbl.longB1 = <html>Wspó\u0142czynnik oporu na jednostk\u0119 powierzchni ta\u015Bmy.<br>
+ ParachuteCfg.lbl.longB2 = Du\u017Cy wspó\u0142czynnik oporu skutkuje zmniejszeniem szybko\u015Bci opadania.
+ ParachuteCfg.lbl.longB3 = Standardowa wielko\u015B\u0107 dla spadochronów wynosi 0.8.
+ ParachuteCfg.but.Reset = Reset
+ ParachuteCfg.lbl.Shroudlines = Linki no\u015Bne:
+ ParachuteCfg.lbl.Numberoflines = Liczba linek:
+ ParachuteCfg.lbl.Linelength = D\u0142ugo\u015B\u0107 linek:
+ ParachuteCfg.lbl.Material = Materia\u0142:
+ ParachuteCfg.lbl.Posrelativeto = Po\u0142o\u017Cenie wzgl\u0119dem:
+ ParachuteCfg.lbl.plus = plus
+ ParachuteCfg.lbl.Packedlength = D\u0142ugo\u015B\u0107 po zwini\u0119ciu:
+ ParachuteCfg.lbl.Packeddiam = \u015Arednica po zwini\u0119ciu:
+ ParachuteCfg.lbl.Deploysat = Aktywacja w chwili:
+ ParachuteCfg.lbl.seconds = sek.
+ ParachuteCfg.lbl.Altitude = Wysoko\u015B\u0107:
+ ParachuteCfg.tab.General = Ogólne
+ ParachuteCfg.tab.ttip.General = W\u0142a\u015Bciwo\u015Bci ogólne
+ ParachuteCfg.tab.Radialpos = Po\u0142o\u017Cenie wzgl\u0119dem \u015Brodka
+ ParachuteCfg.tab.ttip.Radialpos = Konfiguracja po\u0142o\u017Cenia wzgl\u0119dem \u015Brodka
+ ParachuteCfg.lbl.Radialdistance = Odleg\u0142o\u015B\u0107 od \u015Brodka:
+ ParachuteCfg.lbl.Radialdirection = Kierunek wzgl\u0119dem \u015Brodka:
+ ParachuteCfg.but.Reset = Reset
+ ParachuteCfg.lbl.plusdelay = plus
+
+ ! ShockCordConfig
+ ShockCordCfg.lbl.Shockcordlength = D\u0142ugo\u015B\u0107 linki amortyzuj\u0105cej
+ ShockCordCfg.lbl.Shockcordmaterial = Materia\u0142 linki amortyzuj\u0105cej:
+ ShockCordCfg.lbl.Posrelativeto = Po\u0142o\u017Cenie wzgl\u0119dem:
+ ShockCordCfg.lbl.plus = plus
+ ShockCordCfg.lbl.Packedlength = D\u0142ugo\u015B\u0107 po zwini\u0119ciu:
+ ShockCordCfg.lbl.Packeddiam = \u015Arednica po zwini\u0119ciu:
+ ShockCordCfg.tab.General = Ogólne
+ ShockCordCfg.tab.ttip.General = W\u0142a\u015Bciwo\u015Bci ogólne
+
+ !SleeveConfig
+ SleeveCfg.tab.Outerdiam = \u015Arednica zewn\u0119trzna:
+ SleeveCfg.tab.Innerdiam = \u015Arednica wewn\u0119trzna:
+ SleeveCfg.tab.Wallthickness = Grubo\u015B\u0107 \u015Bciany:
+ SleeveCfg.tab.Length = D\u0142ugo\u015B\u0107:
+ SleeveCfg.tab.General = Ogólne
+ SleeveCfg.tab.Generalproperties = W\u0142a\u015Bciwo\u015Bci ogólne
+
+ ! StreamerConfig
+ StreamerCfg.lbl.Striplength = D\u0142ugo\u015B\u0107 paska:
+ StreamerCfg.lbl.Stripwidth = Szeroko\u015B\u0107 paska:
+ StreamerCfg.lbl.Striparea = Powierzchnia paska:
+ StreamerCfg.lbl.Aspectratio = Format:
+ StreamerCfg.lbl.Material = Materia\u0142:
+ StreamerCfg.combo.ttip.MaterialModel = Materia\u0142 cz\u0119\u015Bci ma wp\u0142yw na jej ci\u0119\u017Car.
+ StreamerCfg.lbl.longA1 = <html>Wspó\u0142czynnik oporu C<sub>D</sub>
+ StreamerCfg.lbl.longB1 = <html>Wspó\u0142czynnik oporu na jednostk\u0119 powierzchni ta\u015Bmy.<br>
+ StreamerCfg.lbl.longB2 = Du\u017Cy wspó\u0142czynnik oporu skutkuje zmniejszeniem szybko\u015Bci opadania.
+ StreamerCfg.lbl.Automatic = Auto
+ StreamerCfg.lbl.longC1 = Wspó\u0142czynnik oporu zale\u017Cy od powierzchni ta\u015Bmy.
+ StreamerCfg.lbl.Posrelativeto = Po\u0142o\u017Cenie wzgl\u0119dem:
+ StreamerCfg.lbl.plus = plus
+ StreamerCfg.lbl.Packedlength = D\u0142ugo\u015B\u0107 po zwini\u0119ciu:
+ StreamerCfg.lbl.Packeddiam = \u015Arednica po zwini\u0119ciu:
+ StreamerCfg.lbl.Deploysat = Aktywacja w chwili:
+ StreamerCfg.lbl.seconds = sek.
+ StreamerCfg.lbl.Altitude = Wysoko\u015B\u0107:
+ StreamerCfg.tab.General = Ogólne
+ StreamerCfg.tab.ttip.General = W\u0142a\u015Bciwo\u015Bci ogólne
+ StreamerCfg.tab.Radialpos = Po\u0142o\u017Cenie wzgl\u0119dem \u015Brodka
+ StreamerCfg.tab.ttip.Radialpos = Konfiguracja po\u0142o\u017Cenia wzgl\u0119dem \u015Brodka
+ StreamerCfg.lbl.Radialdistance = Odleg\u0142o\u015B\u0107 od \u015Brodka:
+ StreamerCfg.lbl.Radialdirection = Kierunek wzgl\u0119dem \u015Brodka:
+ StreamerCfg.but.Reset = Reset
+ StreamerCfg.lbl.plusdelay = plus
+
+ ! ThicknessRingComponentConfig
+ ThicknessRingCompCfg.tab.Outerdiam = \u015Arednica zewn\u0119trzna:
+ ThicknessRingCompCfg.tab.Innerdiam = \u015Arednica wewn\u0119trzna:
+ ThicknessRingCompCfg.tab.Wallthickness = Grubo\u015B\u0107 \u015Bciany:
+ ThicknessRingCompCfg.tab.Length = D\u0142ugo\u015B\u0107:
+ ThicknessRingCompCfg.tab.General = Ogólne
+ ThicknessRingCompCfg.tab.Generalprop = W\u0142a\u015Bciwo\u015Bci ogólne
+
+ ! TransitionConfig
+ TransitionCfg.lbl.Transitionshape = Kszta\u0142t talii przej\u015Bciowej
+ TransitionCfg.checkbox.Clipped = Przyci\u0119ta
+ TransitionCfg.lbl.Shapeparam = Parametr kszta\u0142tu
+ TransitionCfg.lbl.Transitionlength = D\u0142ugo\u015B\u0107 przej\u015Bciówki:
+ TransitionCfg.lbl.Forediam = \u015Arednica przednia:
+ TransitionCfg.checkbox.Automatic = Auto
+ TransitionCfg.lbl.Aftdiam = \u015Arednica tylna:
+ TransitionCfg.lbl.Wallthickness = Grubo\u015B\u0107 \u015Bciany:
+ TransitionCfg.checkbox.Filled = Wype\u0142nione
+ TransitionCfg.tab.General = Ogólne
+ TransitionCfg.tab.Generalproperties = W\u0142a\u015Bciwo\u015Bci ogólne
+ TransitionCfg.tab.Shoulder = Wpust
+ TransitionCfg.tab.Shoulderproperties = Parametry wpustu
+
+ ! TrapezoidFinSetConfig
+ TrapezoidFinSetCfg.lbl.Nbroffins = Liczba stateczników:
+ TrapezoidFinSetCfg.lbl.ttip.Nbroffins = Liczba stateczników w zestawie.
+ TrapezoidFinSetCfg.lbl.Finrotation = Rotacja stateczników:
+ TrapezoidFinSetCfg.lbl.ttip.Finrotation = K\u0105t nachylenia pierwszego statecznika w zestawie.
+ TrapezoidFinSetCfg.lbl.Fincant = Nachylenie stateczników:
+ TrapezoidFinSetCfg.lbl.ttip.Fincant = K\u0105t nachylenia stateczników wzgl\u0119dem korpusu.
+ TrapezoidFinSetCfg.lbl.Rootchord = Kraw\u0119d\u017A podstawy:
+ TrapezoidFinSetCfg.lbl.Tipchord = Kraw\u0119d\u017A zewn\u0119trzna:
+ TrapezoidFinSetCfg.lbl.Height = Wysoko\u015B\u0107:
+ TrapezoidFinSetCfg.lbl.Sweeplength = D\u0142ugo\u015B\u0107 przesuni\u0119cia:
+ TrapezoidFinSetCfg.lbl.Sweepangle = K\u0105t przesuni\u0119cia:
+ TrapezoidFinSetCfg.lbl.FincrossSection = Przekrój statecznika:
+ TrapezoidFinSetCfg.lbl.Thickness = Grubo\u015B\u0107:
+ TrapezoidFinSetCfg.lbl.Posrelativeto = Po\u0142o\u017Cenie wzgl\u0119dem:
+ TrapezoidFinSetCfg.lbl.plus = plus
+ TrapezoidFinSetCfg.tab.General = Ogólne
+ TrapezoidFinSetCfg.tab.Generalproperties = W\u0142a\u015Bciwo\u015Bci ogólne
+
+ !MotorConfigurationModel
+ MotorCfgModel.Editcfg = Edytuj konfiguracje
+
+ ! StorageOptionChooser
+ StorageOptChooser.lbl.Simdatatostore = Dane symulacji do zapisania:
+ StorageOptChooser.rdbut.Allsimdata = Wszystkie dane symulacji:
+ StorageOptChooser.lbl.longA1 = <html>Zapisz wszystkie dane z symulacji.<br>
+ StorageOptChooser.lbl.longA2 = To mo\u017Ce bardzo zwi\u0119kszy\u0107 rozmiar plików!
+ StorageOptChooser.rdbut.Every = Co
+ StorageOptChooser.lbl.longB1 = <html>Zapisz warto\u015Bci daj\u0105ce si\u0119 przedstawi\u0107 na wykresie w powy\u017Cszych odst\u0119pach.<br>
+ StorageOptChooser.lbl.longB2 = Wi\u0119ksze warto\u015Bci przek\u0142adaj\u0105 si\u0119 na mniejsze pliki.
+ StorageOptChooser.lbl.seconds = sek.
+ StorageOptChooser.rdbut.Onlyprimfig = Tylko dane podstawowe
+ StorageOptChooser.lbl.longC1 = <html>Zapisz tylko warto\u015Bci ukazane w tabeli podsumowuj\u0105cej symulacj\u0119.<br>
+ StorageOptChooser.lbl.longC2 = Przy tym ustawieniu pliki s\u0105 najmniejsze.
+ StorageOptChooser.checkbox.Compfile = Kompresuj plik
+ StorageOptChooser.lbl.UsingComp = Kompresowanie pliku zmniejsza znacznie jego rozmiar.
+ StorageOptChooser.lbl.longD1 = Szacunkowy rozmiar pliku przy bie\u017C\u0105cych ustawieniach.
+ StorageOptChooser.ttip.Saveopt = Zapisz opcje
+ StorageOptChooser.lbl.Estfilesize = Przybli\u017Cony rozmiar pliku:
+ StorageOptChooser.lbl.Saveopt = Zapisz opcje
+
+ ! ThrustCurveMotorSelectionPanel
+ TCMotorSelPan.lbl.Selrocketmotor = Wybierz silnik rakiety:
+ TCMotorSelPan.checkbox.hideSimilar = Ukryj bardzo podobne krzywe ci\u0105gu.
+ TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Poka\u017C wszystkie silniki
+ TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Poka\u017C silniki ze \u015Brednic\u0105 mniejsza ni\u017C \u015Brednica gniazda silnika
+ TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Poka\u017C silniki ze \u015Brednic\u0105 równa \u015Brednicy gniazda silnika
+ TCMotorSelPan.lbl.Motormountdia = \u015Arednica gniazda silnika:
+ TCMotorSelPan.lbl.Search = Szukaj:
+ TCMotorSelPan.lbl.Selectthrustcurve = Wybierz krzyw\u0105 si\u0142y ci\u0105gu:
+ TCMotorSelPan.lbl.Ejectionchargedelay = Opó\u017Anienie odpalenia \u0142adunku odrzucaj\u0105cego:
+ TCMotorSelPan.equalsIgnoreCase.None = \u017Badne
+ TCMotorSelPan.lbl.NumberofsecondsorNone = (liczba sekund lub \"Brak\")
+ TCMotorSelPan.lbl.Totalimpulse = Ca\u0142kowity impuls:
+ TCMotorSelPan.lbl.Avgthrust = \u015Arednia si\u0142a ci\u0105gu:
+ TCMotorSelPan.lbl.Maxthrust = Maks. si\u0142a ci\u0105gu:
+ TCMotorSelPan.lbl.Burntime = Czas spalania paliwa w silniku:
+ TCMotorSelPan.lbl.Launchmass = Masa startowa:
+ TCMotorSelPan.lbl.Emptymass = Masa pustej rakiety:
+ TCMotorSelPan.lbl.Datapoints = Punkty pomiarowe:
+ TCMotorSelPan.lbl.Digest = Podsumowanie:
+ TCMotorSelPan.title.Thrustcurve = Krzywa si\u0142y ci\u0105gu:
+ TCMotorSelPan.title.Thrust = Ci\u0105g
+ TCMotorSelPan.delayBox.None = \u017Badne
+
+
+ ! PlotDialog
+ PlotDialog.title.Flightdataplot = Wykres danych lotu
+ PlotDialog.Chart.Simulatedflight = Lot symulowany
+ PlotDialog.CheckBox.Showdatapoints = Poka\u017C punkty pomiarowe
+ PlotDialog.lbl.Chart = Kliknij i przeci\u0105gnij w dó\u0142 + prawo aby powi\u0119kszy\u0107; góra + lewo aby pomniejszy\u0107
+
+
+ ! "main" prefix is used for the main application dialog
+
+ # FIXME: Rename the description keys
+
+ main.menu.file = Plik
+ main.menu.file.desc = Czynno\u015Bci zwi\u0105zane z obs\u0142ug\u0105 plików
+ main.menu.file.new = Nowy
+ main.menu.file.new.desc = Stwórz nowy projekt rakiety
+ main.menu.file.open = Otwórz...
+ BasicFrame.item.Openrocketdesign = Otwórz projekt rakiety
+ main.menu.file.openExample = Otwórz przyk\u0142ad...
+ BasicFrame.item.Openexamplerocketdesign = Otwórz przyk\u0142adowy projekt rakiety
+ main.menu.file.save = Zapisz
+ BasicFrame.item.SavecurRocketdesign = Zapisz obecny projekt rakiety
+ main.menu.file.saveAs = Zapisz jako...
+ BasicFrame.item.SavecurRocketdesnewfile = Zapisz obecny projekt rakiety w nowym pliku
+ main.menu.file.print = Drukuj / Eksportuj do PDF...
+ main.menu.file.print.desc = Drukuj lub zapisz jako PDF list\u0119 cz\u0119\u015Bci i szablony stateczników.
+ main.menu.file.close = Zamknij
+ BasicFrame.item.Closedesign = Zamknij bie\u017C\u0105cy projekt rakiety
+ main.menu.file.quit = Wyjd\u017A
+ BasicFrame.item.Quitprogram = Wyjd\u017A z programu
+
+ main.menu.edit = Edycja
+ BasicFrame.menu.Rocketedt = Edytowanie rakiety
+ main.menu.edit.undo = Cofnij
+ main.menu.edit.undo.desc = Cofnij poprzedni\u0105 czynno\u015B\u0107
+ main.menu.edit.redo = Powtórz
+ main.menu.edit.redo.desc = Powtórz poprzednio cofni\u0119t\u0105 czynno\u015B\u0107
+ main.menu.edit.cut = Wytnij
+ main.menu.edit.copy = Kopiuj
+ main.menu.edit.paste = Wklej
+ main.menu.edit.delete = Usu\u0144
+ main.menu.edit.resize = Skaluj...
+ main.menu.edit.resize.desc = Skaluj cz\u0119\u015Bci modelu rakiety...
+ main.menu.edit.preferences = Ustawienia
+ main.menu.edit.preferences.desc = Edytuj ustawienia programu
+
+ main.menu.analyze = Analiza
+ main.menu.analyze.desc = Analiza rakiety
+ main.menu.analyze.componentAnalysis = Analiza cz\u0119\u015Bci
+ main.menu.analyze.componentAnalysis.desc = Analizuj oddzielnie poszczególne cz\u0119\u015Bci sk\u0142adóe rakiety
+ main.menu.analyze.optimization = Optymalizacja rakiety
+ main.menu.analyze.optimization.desc = Ogólna optymalizacja projektu rakiety
+
+ main.menu.help = Pomoc
+ main.menu.help.desc = Informacje o programie OpenRocket
+ main.menu.help.tours = Instrukcje krok po kroku
+ main.menu.help.tours.desc = Przejd\u017A przez instrukcje krok po kroku w programie OpenRocket
+ main.menu.help.license = Licencja
+ main.menu.help.license.desc = Informacja o licencji programu OpenRocket
+ main.menu.help.bugReport = Raport o b\u0142\u0119dach
+ main.menu.help.bugReport.desc = Informacja o zg\u0142aszaniu problemów, b\u0142\u0119dów i usterek w programie OpenRocket
+ main.menu.help.debugLog = Rejestr debuggera
+ main.menu.help.debugLog.desc = Przegl\u0105daj rejestr debuggera programu OpenRocket
+ main.menu.help.about = Informacja
+ main.menu.help.about.desc = Informacja o prawach autorskich do programu OpenRocket
+
+ main.menu.debug = Debugowanie
+ main.menu.debug.whatisthismenu = Co to za okno?
+ main.menu.debug.createtestrocket = Stwórz rakiet\u0119 testow\u0105
+
+ ! database
+ ! Translate here all material database
+ !
+
+ ! Material database
+ ! BULK_MATERIAL
+ Databases.materials.Acrylic = Akryl
+ Databases.materials.Aluminum = Aluminium
+ Databases.materials.Balsa = Balsa
+ Databases.materials.Basswood = Lipa
+ Databases.materials.Birch = Brzoza
+ Databases.materials.Brass = Mosi\u0105dz
+ Databases.materials.Cardboard = Karton
+ Databases.materials.Carbonfiber = W\u0142ókno w\u0119glowe
+ Databases.materials.Cork = Korek
+ Databases.materials.DepronXPS = Depron (XPS)
+ Databases.materials.Fiberglass = W\u0142ókno szklane
+ Databases.materials.Kraftphenolic = Kraft fenolowy
+ Databases.materials.Maple = Klon
+ Databases.materials.Paperoffice = Papier (biurowy)
+ Databases.materials.Pine = Sosna
+ Databases.materials.Plywoodbirch = Sklejka (brzoza)
+ Databases.materials.PolycarbonateLexan = Poliw\u0119glan (Lexan)
+ Databases.materials.Polystyrene = Polistyren
+ Databases.materials.PVC = PVC
+ Databases.materials.Spruce = \u015Awierk
+ Databases.materials.Steel = Stal
+ Databases.materials.StyrofoamgenericEPS = Styropian (zwyk\u0142y EPS)
+ Databases.materials.StyrofoamBluefoamXPS = Styropian \"kolorowy\" (XPS)
+ Databases.materials.Titanium = Tytan
+ Databases.materials.Quantumtubing = Tuby kwantowe
+ Databases.materials.BlueTube = Blue tube
+ !SURFACE_MATERIAL
+ Databases.materials.Ripstopnylon = Nylon Rip-stop
+ Databases.materials.Mylar = Mylar
+ Databases.materials.Polyethylenethin = Polietylen (cienki)
+ Databases.materials.Polyethyleneheavy = Polietylen (ci\u0119\u017Cki)
+ Databases.materials.Silk = Jedwab
+ Databases.materials.Paperoffice = Papier (biurowy)
+ Databases.materials.Cellophane = Celofan
+ Databases.materials.Crepepaper = Papier marszczony, krepina
+ ! LINE_MATERIAL
+ Databases.materials.Threadheavy-duty = Ni\u0107 (wytrzyma\u0142a)
+ Databases.materials.Elasticcordround2mm = Przewód elastyczny (okr\u0105g\u0142y 2mm)
+ Databases.materials.Elasticcordflat6mm = Przewód elastyczny (p\u0142aski 6mm)
+ Databases.materials.Elasticcordflat12mm = Przewód elastyczny (p\u0142aski 12 mm)
+ Databases.materials.Elasticcordflat19mm = Przewód elastyczny (p\u0142aski 19 mm)
+ Databases.materials.Elasticcordflat25mm = Przewód elastyczny (p\u0142aski 25mm)
+ Databases.materials.Braidednylon2mm = Nylon spleciony (2 mm)
+ Databases.materials.Braidednylon3mm = Nylon spleciony (3 mm)
+ Databases.materials.Tubularnylon11mm = Nylon rurkowy (11 mm)
+ Databases.materials.Tubularnylon14mm = Nylon rurkowy (14 mm)
+ Databases.materials.Tubularnylon25mm = Nylon rurkowy (25 mm)
+
+ ! ExternalComponent
+ ExternalComponent.Rough = Chropowate
+ ExternalComponent.Unfinished = Niewyko\u0144czone
+ ExternalComponent.Regularpaint = Zwyk\u0142a farba
+ ExternalComponent.Smoothpaint = G\u0142adka farba
+ ExternalComponent.Polished = Wypolerowany
+
+ ! LineStyle
+ LineStyle.Solid = Ci\u0105g\u0142a
+ LineStyle.Dashed = Kreskowana
+ LineStyle.Dotted = Kropkowana
+ LineStyle.Dash-dotted = Kreska-kropka
+ LineStyle.Defaultstyle = Domy\u015Blny
+
+ ! Shape
+ Shape.Conical = Sto\u017Ckowy
+ Shape.Conical.desc1 = G\u0142owica sto\u017Ckowa ma przekrój w kszta\u0142cie trójk\u0105ta.
+ Shape.Conical.desc2 = Sto\u017Ckowa talia przej\u015Bciowa ma proste boki.
+ Shape.Ogive = Ostro\u0142uk
+ Shape.Ogive.desc1 = G\u0142owica w kszta\u0142cie ostro\u0142uku ma przekrój b\u0119d\u0105cy fragmentem okr\u0119gu. Warto\u015B\u0107 parametru kszta\u0142tu równa 1 tworzy <b>ostro\u0142uk styczny</b>, który zapewnia g\u0142adkie po\u0142\u0105czenie g\u0142owicy z korpusem rakiety. Warto\u015Bci poni\u017Cej 1 tworz\u0105 <b>ostro\u0142uki sieczne</b>.
+ Shape.Ogive.desc2 = Talia przej\u015Bciowa w kszta\u0142cie ostro\u0142uku ma przekrój b\u0119d\u0105cy fragmentem okr\u0119gu.
+ Shape.Ellipsoid = Elipsoida
+ Shape.Ellipsoid.desc1 = G\u0142owica elipsoidalna ma przekrój w kszta\u0142cie pó\u0142elipsy o osiach g\u0142ównych o d\u0142ugo\u015Bci 2×<i>d\u0142ugo\u015B\u0107</i> i <i>\u015Brednica</i>.
+ Shape.Ellipsoid.desc2 = Elipsoidalna talia przej\u015Bciowa ma przekrój w kszta\u0142cie pó\u0142elipsy o osiach g\u0142ównych o d\u0142ugo\u015Bci 2×<i>d\u0142ugo\u015B\u0107</i> i <i>\u015Brednica</i>. Je\u017Celi talia przej\u015Bciowa nie jest przyci\u0119ta, to \u015Brodek przekroju jest wybrzuszony przez promie\u0144 tworz\u0105cy.
+ Shape.Powerseries = Seria pot\u0119gowa
+ Shape.Powerseries.desc1 = G\u0142owica serii pot\u0119gowej ma przekrój w kszta\u0142cie: <i>promie\u0144</i> × (<i>x</i> / <i>d\u0142ugo\u015B\u0107</i>)<sup><i>k</i></sup> gdzie<i>k</i> jest parametrem kszta\u0142tu. Dla <i>k</i> równego 0,5 mamy pot\u0119g\u0119 o stopniu 1/2, co nam daje g\u0142owic\u0119 paraboliczn\u0105. Dla <i>k</i> wynosz\u0105cego 0,75 dostajemy pot\u0119g\u0119 stopnia 3/4, za\u015B dla k wynosz\u0105cego 1 otrzymujemy g\u0142owic\u0119 sto\u017Ckow\u0105.
+ Shape.Powerseries.desc2 = Talia przej\u015Bciowa serii pot\u0119gowej ma przekrój w kszta\u0142cie: <i>promie\u0144</i> × (<i>x</i> / <i>d\u0142ugo\u015B\u0107</i>)<sup><i>k</i></sup> gdzie<i>k</i> jest parametrem kszta\u0142tu. Dla <i>k</i> równego 0,5 mamy pot\u0119g\u0119 o stopniu 1/2, co nam daje paraboliczn\u0105 tali\u0119 orzej\u015Bciow\u0105. Dla <i>k</i> wynosz\u0105cego 0,75 dostajemy pot\u0119g\u0119 stopnia 3/4, za\u015B dla k wynosz\u0105cego 1 otrzymujemy sto\u017Ckow\u0105 tali\u0119 przej\u015Bciow\u0105.
+ Shape.Parabolicseries = Seria paraboliczna
+ Shape.Parabolicseries.desc1 = G\u0142owica paraboliczna ma przekrój w kszta\u0142cie paraboli. Parametr kszta\u0142tu okre\u015Bla odcinek paraboli, który zostanie u\u017Cyty. Warto\u015B\u0107 parametru kszta\u0142tu równa 1 tworzy <b>pe\u0142n\u0105 parabol\u0119</b>, która jest styczna do korpusu rakiety, 0,75 tworzy <b> 3/4 paraboli</b>, 0,5 tworzy <b>1/2 paraboli</b> oraz 0 tworzy g\u0142owic\u0119 <b>sto\u017Ckow\u0105</b>rakiety.
+ Shape.Parabolicseries.desc2 = Talia przej\u015Bciowa paraboliczna ma przekrój w kszta\u0142cie paraboli. Parametr kszta\u0142tu okre\u015Bla odcinek paraboli, który zostanie u\u017Cyty. Warto\u015B\u0107 parametru kszta\u0142tu równa 1 tworzy <b>pe\u0142n\u0105 parabole</b>, która jest styczna do tylnego ko\u0144ca, 0,75 tworzy <b> 3/4 paraboli</b>, 0,5 tworzy <b>1/2 paraboli</b> oraz 0 tworzy <b>sto\u017Ckow\u0105</b> tali\u0119 przej\u015Bciow\u0105
+ Shape.Haackseries = Seria Haacka
+ Shape.Haackseries.desc1 = Seria g\u0142owic Haacka zosta\u0142a tak zaprojektowana, aby osi\u0105gn\u0105\u0107 minimalny opór. Warto\u015B\u0107 parametru kszta\u0142tu równa 0 tworzy g\u0142owic\u0119 <b>LD-Haack</b> lub <b>Von Karman</b>, która minimalizuje opór przy ustalonej d\u0142ugo\u015Bci i \u015Brednicy g\u0142owicy. Warto\u015B\u0107 parametru kszta\u0142tu równa 0.333 tworzy g\u0142owic\u0119 <b>LV-Haack</b> która minimalizuje opór przy ustalonej d\u0142ugo\u015Bci i obj\u0119to\u015Bci g\u0142owicy.
+ Shape.Haackseries.desc2 = Seria <i>g\u0142owic</i> Haacka zosta\u0142a tak zaprojektowana, aby osi\u0105gn\u0105\u0107 minimalny opór. Talie przej\u015Bciowe zaprojektowane wed\u0142ug tej metody maj\u0105 podobny kszta\u0142t, ale niekoniecznie zapewniaj\u0105 optymalny opór talii przej\u015Bciowej. Warto\u015B\u0107 parametru kszta\u0142tu równa 0 tworzy kszta\u0142t <b>LD-Haack</b> lub <b>Von Karman</b>, za\u015B warto\u015B\u0107 równa 0,333 tworzy kszta\u0142t <b>LV-Haack</b>.
+
+
+ ! RocketComponent
+ RocketComponent.Position.TOP = Góra cz\u0119\u015Bci podstawowej
+ RocketComponent.Position.MIDDLE = \u015Arodek cz\u0119\u015Bci podstawowej
+ RocketComponent.Position.BOTTOM = Dó\u0142 cz\u0119\u015Bci podstawowej
+ RocketComponent.Position.AFTER = Za cz\u0119\u015Bci\u0105 podstawow\u0105
+ RocketComponent.Position.ABSOLUTE = Czubek g\u0142owicy
+
+ ! LaunchLug
+ LaunchLug.Launchlug = Zaczep startowy
+ ! NoseCone
+ NoseCone.NoseCone = G\u0142owica
+ ! Transition
+ Transition.Transition = Talia przej\u015Bciowa
+ !Stage
+ Stage.Stage = Stopie\u0144
+
+ Stage.SeparationEvent.UPPER_IGNITION = Zap\u0142on silnika wy\u017Cszego stopnia
+ Stage.SeparationEvent.IGNITION = Zap\u0142on silnika bie\u017C\u0105cego stopnia
+ Stage.SeparationEvent.BURNOUT = Wyga\u015Bni\u0119cie silnika bie\u017C\u0105cego stopnia
+ Stage.SeparationEvent.EJECTION = \u0141adunek odrzucaj\u0105cy bie\u017C\u0105cego stopnia
+ Stage.SeparationEvent.LAUNCH = Start
+ Stage.SeparationEvent.NEVER = Nigdy
+
+ ! BodyTube
+ BodyTube.BodyTube = Korpus rakiety
+ ! TubeCoupler
+ TubeCoupler.TubeCoupler = \u0141\u0105cznik rur
+ !InnerTube
+ InnerTube.InnerTube = Rura wewn\u0119trzna
+ ! TrapezoidFinSet
+ TrapezoidFinSet.TrapezoidFinSet = Zestaw stateczników trapezoidalnych
+ ! FreeformFinSet
+ FreeformFinSet.FreeformFinSet = Zestaw stateczników o niestandardowym kszta\u0142cie
+ !MassComponent
+ MassComponent.MassComponent = Balast
+ ! Parachute
+ Parachute.Parachute = Spadochron
+ ! ShockCord
+ ShockCord.ShockCord = Linka amortyzuj\u0105ca
+ ! Bulkhead
+ Bulkhead.Bulkhead = Przegroda
+
+ !Rocket
+ Rocket.motorCount.Nomotor = [bez silników]
+ Rocket.compname.Rocket = Rakieta
+
+ !MotorMount
+ MotorMount.IgnitionEvent.AUTOMATIC = Rakieta
+ MotorMount.IgnitionEvent.LAUNCH = Start
+ MotorMount.IgnitionEvent.EJECTION_CHARGE = Pierwszy \u0142adunek odrzucaj\u0105cy poprzedniego stopnia
+ MotorMount.IgnitionEvent.BURNOUT = Pierwsze wypalenie poprzedniego stopnia
+ MotorMount.IgnitionEvent.NEVER = Nigdy
+
+ !ComponentIcons
+ ComponentIcons.Nosecone = G\u0142owica
+ ComponentIcons.Bodytube = Korpus rakiety
+ ComponentIcons.Transition = Talia przej\u015Bciowa
+ ComponentIcons.Trapezoidalfinset = Zestaw stateczników trapezoidalnych
+ ComponentIcons.Ellipticalfinset = Zestaw stateczników o kszta\u0142cie eliptycznym
+ ComponentIcons.Freeformfinset = Zestaw stateczników o niestandardowym kszta\u0142cie
+ ComponentIcons.Launchlug = Zaczep startowy
+ ComponentIcons.Innertube = Rura wewn\u0119trzna
+ ComponentIcons.Tubecoupler = \u0141\u0105cznik rur
+ ComponentIcons.Centeringring = Pier\u015Bcie\u0144 centruj\u0105cy
+ ComponentIcons.Bulkhead = Przegroda
+ ComponentIcons.Engineblock = Blokada silnika
+ ComponentIcons.Parachute = Spadochron
+ ComponentIcons.Streamer = Ta\u015Bma
+ ComponentIcons.Shockcord = Linka amortyzuj\u0105ca
+ ComponentIcons.Masscomponent = Balast
+ ComponentIcons.disabled = (nieaktywny)
+
+ ! StageAction
+ StageAction.Stage = Stopie\u0144
+
+ ! RecoveryDevice
+ RecoveryDevice.DeployEvent.LAUNCH = Start (plus NN sekund)
+ RecoveryDevice.DeployEvent.EJECTION = Pierwszy \u0142adunek odrzucaj\u0105cy poprzedniego stopnia
+ RecoveryDevice.DeployEvent.APOGEE = Apogeum
+ RecoveryDevice.DeployEvent.ALTITUDE = Wysoko\u015B\u0107 bezwzgl\u0119dna podczas opadania
+ RecoveryDevice.DeployEvent.CURRENT_STAGE_SEPARATION = Oddzielenie bie\u017C\u0105cego stopnia
+ RecoveryDevice.DeployEvent.LOWER_STAGE_SEPARATION = Oddzielenie ni\u017Cszego stopnia
+ RecoveryDevice.DeployEvent.NEVER = Nigdy
+
+ ! FlightEvent
+ FlightEvent.Type.LAUNCH = Start
+ FlightEvent.Type.IGNITION = Zap\u0142on silnika
+ FlightEvent.Type.LIFTOFF = Start
+ FlightEvent.Type.LAUNCHROD = Opuszczenie pr\u0119ta startowego
+ FlightEvent.Type.BURNOUT = Wypalenie silnika
+ FlightEvent.Type.EJECTION_CHARGE = \u0141adunek odrzucaj\u0105cy
+ FlightEvent.Type.STAGE_SEPARATION = Separacja stopnia
+ FlightEvent.Type.APOGEE = Apogeum
+ FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Aktywacja uk\u0142adu odzysku
+ FlightEvent.Type.GROUND_HIT = Uderzenie w ziemi\u0119
+ FlightEvent.Type.SIMULATION_END = Koniec symulacji
+ FlightEvent.Type.ALTITUDE = Zmiana wysoko\u015Bci
+
+ ! ThrustCurveMotorColumns
+ TCurveMotorCol.MANUFACTURER = Producent
+ TCurveMotorCol.DESIGNATION = Oznaczenie
+ TCurveMotorCol.TYPE = Typ
+ TCurveMotorCol.DIAMETER = \u015Arednica
+ TCurveMotorCol.LENGTH = D\u0142ugo\u015B\u0107
+
+ ! RocketInfo
+ RocketInfo.lengthLine.Length = D\u0142ugo\u015B\u0107
+ RocketInfo.lengthLine.maxdiameter = , maks. \u015Brednica
+ RocketInfo.massText1 = Masa z silnikami
+ RocketInfo.massText2 = Masa bez silników
+ RocketInfo.at = przy M
+ RocketInfo.cgText = \u015AC:
+ RocketInfo.cpText = \u015AP:
+ RocketInfo.stabText = Stabilno\u015B\u0107:
+ RocketInfo.Warning = Ostrze\u017Cenie:
+ RocketInfo.Calculating = Obliczanie...
+ RocketInfo.Apogee = Apogeum:
+ RocketInfo.Maxvelocity = Max. pr\u0119dko\u015B\u0107:
+ RocketInfo.Maxacceleration = Max. przy\u015Bpieszenie:
+ RocketInfo.apogeeValue = N/D
+ RocketInfo.Mach = ( Mach
+ RocketInfo.velocityValue = N/D
+ RocketInfo.accelerationValue = N/D
+
+ ! FinSet
+ FinSet.CrossSection.SQUARE = Kwadratowy
+ FinSet.CrossSection.ROUNDED = Zaokr\u0105glony
+ FinSet.CrossSection.AIRFOIL = Profil lotniczy
+ FinSet.TabRelativePosition.FRONT = Przedni kraniec kraw\u0119dzi podstawy
+ FinSet.TabRelativePosition.CENTER = \u015Arodek kraw\u0119dzi podstawy
+ FinSet.TabRelativePosition.END = Tylny kraniec kraw\u0119dzi podstawy
+
+ ! FlightDataType
+ FlightDataType.TYPE_TIME = Czas
+ FlightDataType.TYPE_ALTITUDE = Wysoko\u015B\u0107
+ FlightDataType.TYPE_VELOCITY_Z = Pr\u0119dko\u015B\u0107 pionowa
+ FlightDataType.TYPE_ACCELERATION_Z = Przyspieszenie pionowe
+ FlightDataType.TYPE_VELOCITY_TOTAL = Pr\u0119dko\u015B\u0107 ca\u0142kowita
+ FlightDataType.TYPE_ACCELERATION_TOTAL = Przyspieszenie ca\u0142kowite
+ FlightDataType.TYPE_POSITION_X = Pozycja do nawietrznej
+ FlightDataType.TYPE_POSITION_Y = Pozycja równoleg\u0142a do wiatru
+ FlightDataType.TYPE_POSITION_XY = Odleg\u0142o\u015B\u0107 boczna
+ FlightDataType.TYPE_POSITION_DIRECTION = Kierunek boczny
+ FlightDataType.TYPE_VELOCITY_XY = Pr\u0119dko\u015B\u0107 boczna
+ FlightDataType.TYPE_ACCELERATION_XY = Przyspieszenie boczne
+ FlightDataType.TYPE_AOA = K\u0105t natarcia
+ FlightDataType.TYPE_ROLL_RATE = Tempo obrotu
+ FlightDataType.TYPE_PITCH_RATE = Tempo nachylenia
+ FlightDataType.TYPE_YAW_RATE = Tempo przesuni\u0119cia
+ FlightDataType.TYPE_MASS = Masa
+ FlightDataType.TYPE_LONGITUDINAL_INERTIA = Wzd\u0142u\u017Cny moment bezw\u0142adno\u015Bci
+ FlightDataType.TYPE_ROTATIONAL_INERTIA = Rotacyjny moment bezw\u0142adno\u015Bci
+ FlightDataType.TYPE_CP_LOCATION = Po\u0142o\u017Cenie \u015AP
+ FlightDataType.TYPE_CG_LOCATION = Po\u0142o\u017Cenie \u015AC
+ FlightDataType.TYPE_STABILITY = Zapas stabilno\u015Bci w kalibrach
+ FlightDataType.TYPE_MACH_NUMBER = Liczba Macha
+ FlightDataType.TYPE_REYNOLDS_NUMBER = Liczba Reynoldsa
+ FlightDataType.TYPE_THRUST_FORCE = Si\u0142a si\u0105gu
+ FlightDataType.TYPE_DRAG_FORCE = Si\u0142a oporu
+ FlightDataType.TYPE_DRAG_COEFF = Wspó\u0142czynnik oporu
+ FlightDataType.TYPE_AXIAL_DRAG_COEFF = Osiowy wspó\u0142czynnik oporu
+ FlightDataType.TYPE_FRICTION_DRAG_COEFF = Wspó\u0142czynnik oporu w wyniku tarcia
+ FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Wspó\u0142czynnik oporu w wyniku ci\u015Bnienia
+ FlightDataType.TYPE_BASE_DRAG_COEFF = Bazowy wspó\u0142czynnik oporu
+ FlightDataType.TYPE_NORMAL_FORCE_COEFF = Wspó\u0142czynnik si\u0142y normalnej
+ FlightDataType.TYPE_PITCH_MOMENT_COEFF = Wspó\u0142czynnik momentu nachylenia
+ FlightDataType.TYPE_YAW_MOMENT_COEFF = Wspó\u0142czynnik momentu przesuni\u0119cia
+ FlightDataType.TYPE_SIDE_FORCE_COEFF = Wspó\u0142czynnik si\u0142y bocznej
+ FlightDataType.TYPE_ROLL_MOMENT_COEFF = Wspó\u0142czynnik momentu obrotu
+ FlightDataType.TYPE_ROLL_FORCING_COEFF = Wspó\u0142czynnik wymuszania obrotu
+ FlightDataType.TYPE_ROLL_DAMPING_COEFF = Wspó\u0142czynnik hamowania obrotu
+ FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Wspó\u0142czynnik hamowania nachylenia
+ FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Wspó\u0142czynnik hamowania przesuni\u0119cia
+ FlightDataType.TYPE_REFERENCE_LENGTH = D\u0142ugo\u015B\u0107 odniesienia
+ FlightDataType.TYPE_REFERENCE_AREA = Powierzchnia odniesienia
+ FlightDataType.TYPE_ORIENTATION_THETA = Orientacja pionowa (zenit)
+ FlightDataType.TYPE_ORIENTATION_PHI = Orientacja boczna (azymut)
+ FlightDataType.TYPE_WIND_VELOCITY = Pr\u0119dko\u015B\u0107 wiatru
+ FlightDataType.TYPE_AIR_TEMPERATURE = Temperatura powietrza
+ FlightDataType.TYPE_AIR_PRESSURE = Ci\u015Bnienie powietrza
+ FlightDataType.TYPE_SPEED_OF_SOUND = Pr\u0119dko\u015B\u0107 d\u017Awi\u0119ku
+ FlightDataType.TYPE_TIME_STEP = Krok czasowy symulacji
+ FlightDataType.TYPE_COMPUTATION_TIME = Czas obliczania
+ FlightDataType.TYPE_LATITUDE = Szeroko\u015B\u0107 geograficzna
+ FlightDataType.TYPE_LONGITUDE = Dugo\u015B\u0107 geograficzna
+ FlightDataType.TYPE_CORIOLIS_ACCELERATION = Przyspieszenie Coriolisa
+
+ ! PlotConfiguration
+ PlotConfiguration.Verticalmotion = Ruch pionowy w funkcji czasu
+ PlotConfiguration.Totalmotion = Ruch ca\u0142kowity w funkcji czasu
+ PlotConfiguration.Flightside = Profil boczny lotu
+ PlotConfiguration.Stability = Stabilno\u015B\u0107 w funkcji czasu
+ PlotConfiguration.Dragcoef = Wspó\u0142czynnik oporu wzgl\u0119dem liczby Macha
+ PlotConfiguration.Rollcharacteristics = Charakterystyka obrotu
+ PlotConfiguration.Angleofattack = K\u0105t natarcia i orientacja w funkcji czasu
+ PlotConfiguration.Simulationtime = Krok czasowy symulacji i czas obliczania
+
+ ! Warning
+ Warning.LargeAOA.str1 = Wyst\u0105pi\u0142 du\u017Cy k\u0105t natarcia.
+ Warning.LargeAOA.str2 = Wyst\u0105pi\u0142 du\u017Cy k\u0105t natarcia (
+ Warning.DISCONTINUITY = Nieci\u0105g\u0142o\u015B\u0107 \u015Brednicy rakiety.
+ Warning.THICK_FIN = Grube stateczniki mog\u0105 nie by\u0107 modelowane dok\u0142adnie.
+ Warning.JAGGED_EDGED_FIN = Stateczniki o nieregularnych kraw\u0119dziach mog\u0105 zmniejszy\u0107 dok\u0142adno\u015B\u0107 prognoz.
+ Warning.LISTENERS_AFFECTED = Detektory zmodyfikowa\u0142y symulacj\u0119 lotu
+ Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Uk\u0142ad odzysku zosta\u0142 aktywowany przy wci\u0105\u017C pracuj\u0105cym silniku.
+ Warning.FILE_INVALID_PARAMETER = Wyst\u0105pi\u0142 niew\u0142a\u015Bciwy parametr - zignorowano.
+
+
+ ! Scale dialog
+ ScaleDialog.lbl.scaleRocket = Ca\u0142a rakieta
+ ScaleDialog.lbl.scaleSubselection = Zaznaczenie i cz\u0119\u015Bci dodatkowe
+ ScaleDialog.lbl.scaleSelection = Tylko wybrana cz\u0119\u015B\u0107
+ ScaleDialog.title = Skaluj model
+ ScaleDialog.lbl.scale = Skala:
+ ScaleDialog.lbl.scale.ttip = Wybierz, czy chcesz skalowa\u0107 ca\u0142y model, czy tylko wybran\u0105 cz\u0119\u015B\u0107
+ ScaleDialog.lbl.scaling = Skalowanie do zastosowania:
+ ScaleDialog.lbl.scaling.ttip = Rozmiar wynikowy, warto\u015Bci powy\u017Cej 100% powi\u0119kszaj\u0105, za\u015B warto\u015Bci poni\u017Cej 100% zmniejszaj\u0105 model.
+ ! The scaleFrom/scaleTo pair creates a phrase "Scale from [...] to [...]"
+ ScaleDialog.lbl.scaleFrom = Skaluj od
+ ScaleDialog.lbl.scaleTo = do
+ ScaleDialog.lbl.scaleFromTo.ttip = Okre\u015Bl skalowanie w oparciu o d\u0142ugo\u015B\u0107 oryginaln\u0105 i wynikow\u0105.
+ ScaleDialog.checkbox.scaleMass = Aktualizuj warto\u015B\u0107 masy nominalnej
+ ScaleDialog.checkbox.scaleMass.ttip = Skaluj balast, mno\u017C\u0105c ci\u0119\u017Car przez wspó\u0142czynnik skali podniesiony do sze\u015Bcianu
+ ScaleDialog.button.scale = Skala
+ ScaleDialog.undo.scaleRocket = Skaluj rakiet\u0119
+ ScaleDialog.undo.scaleComponent = Skaluj cz\u0119\u015B\u0107
+
+ ScaleDialog.undo.scaleComponents = Skaluj cz\u0119\u015Bci
+
+ !icons
+ Icons.Undo = Cofnij
+ Icons.Redo = Powtórz
+
+ OpenRocketPrintable.Partsdetail = Szczegó\u0142y cz\u0119\u015Bci
+ OpenRocketPrintable.Fintemplates = Szablony stateczników
+ OpenRocketPrintable.Transitiontemplates = Szablony talii przej\u015Bciowych
+ OpenRocketPrintable.Noseconetemplates = Szablony g\u0142owic
+ OpenRocketPrintable.Finmarkingguide = Instrukcja oznaczania stateczników
+ OpenRocketPrintable.DesignReport = Raport projektu
+ OpenRocketPrintable.Centeringringtemplates = Pier\u015Bcie\u0144 centruj\u0105cy
+
+ OpenRocketDocument.Redo = Powtórz
+ OpenRocketDocument.Undo = Cofnij
+
+ !EllipticalFinSet
+ EllipticalFinSet.Ellipticalfinset = Zestaw stateczników o kszta\u0142cie eliptycznym
+
+ ! Optimization
+
+ ! Modifiers
+
+ optimization.modifier.nosecone.length = D\u0142ugo\u015B\u0107
+ optimization.modifier.nosecone.length.desc = Optymalizuj d\u0142ugo\u015B\u0107 g\u0142owicy.
+ optimization.modifier.nosecone.diameter = \u015Arednica
+ optimization.modifier.nosecone.diameter.desc = Optymalizuj \u015Brednice podstawy g\u0142owicy.
+ optimization.modifier.nosecone.thickness = Grubo\u015B\u0107
+ optimization.modifier.nosecone.thickness.desc = Optymalizuj grubo\u015B\u0107 \u015Bcian g\u0142owicy.
+ optimization.modifier.nosecone.shapeparameter = Parametr kszta\u0142tu
+ optimization.modifier.nosecone.shapeparameter.desc = Optymalizuj parametr kszta\u0142tu g\u0142owicy.
+
+ optimization.modifier.transition.length = D\u0142ugo\u015B\u0107
+ optimization.modifier.transition.length.desc = Optymalizuj d\u0142ugo\u015B\u0107 talii przej\u015Bciowej.
+ optimization.modifier.transition.forediameter = \u015Arednica przednia:
+ optimization.modifier.transition.forediameter.desc = Optymalizuj przedni\u0105 \u015Brednic\u0119 talii przej\u015Bciowej.
+ optimization.modifier.transition.aftdiameter = \u015Arednica tylna:
+ optimization.modifier.transition.aftdiameter.desc = Optymalizuj tylna \u015Brednic\u0119 talii przej\u015Bciowej.
+ optimization.modifier.transition.thickness = Grubo\u015B\u0107
+ optimization.modifier.transition.thickness.desc = Optymalizuj grubo\u015B\u0107 \u015Bcian talii przej\u015Bciowej.
+ optimization.modifier.transition.shapeparameter = Parametr kszta\u0142tu
+ optimization.modifier.transition.shapeparameter.desc = Optymalizuj parametr kszta\u0142tu talii przej\u015Bciowej.
+
+ optimization.modifier.bodytube.length = D\u0142ugo\u015B\u0107
+ optimization.modifier.bodytube.length.desc = Optymalizuj d\u0142ugo\u015B\u0107 korpusu.
+ optimization.modifier.bodytube.outerDiameter = \u015Arednica zewn\u0119trzna
+ optimization.modifier.bodytube.outerDiameter.desc = Optymalizuj zewn\u0119trzn\u0105 \u015Brednic\u0119 korpusu zachowuj\u0105c grubo\u015B\u0107 \u015Bcian.
+ optimization.modifier.bodytube.thickness = Grubo\u015B\u0107
+ optimization.modifier.bodytube.thickness.desc = Optymalizuj grubo\u015B\u0107 \u015Bcian korpusu.
+
+ optimization.modifier.trapezoidfinset.rootChord = Kraw\u0119d\u017A podstawy
+ optimization.modifier.trapezoidfinset.rootChord.desc = Optymalizuj d\u0142ugo\u015B\u0107 kraw\u0119dzi podstawy zestawu stateczników (d\u0142ugo\u015B\u0107 kraw\u0119dzi statecznika przylegaj\u0105cej do korpusu rakiety).
+ optimization.modifier.trapezoidfinset.tipChord = Kraw\u0119d\u017A zewn\u0119trzna
+ optimization.modifier.trapezoidfinset.tipChord.desc = Optymalizuj d\u0142ugo\u015B\u0107 kraw\u0119dzi zewn\u0119trznej zestawu stateczników (d\u0142ugo\u015B\u0107 zewn\u0119trznej kraw\u0119dzi statecznika)
+ optimization.modifier.trapezoidfinset.sweep = Przesuni\u0119cie
+ optimization.modifier.trapezoidfinset.sweep.desc = Optymalizuj przesuni\u0119cie zestawu stateczników (przesuni\u0119cie zewn\u0119trznego kra\u0144ca kraw\u0119dzi natarcia wzgl\u0119dem kra\u0144ca przylegaj\u0105cego do korpusu rakiety).
+ optimization.modifier.trapezoidfinset.height = Wysoko\u015B\u0107
+ optimization.modifier.trapezoidfinset.height.desc = Optymalizuj wysoko\u015B\u0107 zestawu stateczników (po\u0142owa rozpi\u0119to\u015Bci).
+
+ optimization.modifier.ellipticalfinset.length = Kraw\u0119d\u017A podstawy
+ optimization.modifier.ellipticalfinset.length.desc = Optymalizuj d\u0142ugo\u015B\u0107 kraw\u0119dzi podstawy zestawu stateczników.
+ optimization.modifier.ellipticalfinset.height = Wysoko\u015B\u0107
+ optimization.modifier.ellipticalfinset.height.desc = Optymalizuj wysoko\u015B\u0107 zestawu stateczników (po\u0142owa rozpi\u0119to\u015Bci).
+
+ optimization.modifier.finset.cant = K\u0105t nachylenia
+ optimization.modifier.finset.cant.desc = Optymalizuj k\u0105t nachylenia zestawu stateczników.
+ optimization.modifier.finset.position = Pozycja
+ optimization.modifier.finset.position.desc = Optymalizuj po\u0142o\u017Cenie zestawu stateczników wzd\u0142u\u017C korpusu rakiety.
+
+ optimization.modifier.launchlug.length = D\u0142ugo\u015B\u0107
+ optimization.modifier.launchlug.length.desc = Optymalizuj d\u0142ugo\u015B\u0107 zaczepu startowego.
+ optimization.modifier.launchlug.outerDiameter = \u015Arednica zewn\u0119trzna
+ optimization.modifier.launchlug.outerDiameter.desc = Optymalizuj \u015Brednic\u0119 zewn\u0119trzn\u0105 zaczepu startowego.
+ optimization.modifier.launchlug.thickness = Grubo\u015B\u0107
+ optimization.modifier.launchlug.thickness.desc = Optymalizuj grubo\u015B\u0107 zaczepu startowego zachowuj\u0105c sta\u0142\u0105 \u015Brednic\u0119 zewn\u0119trzn\u0105.
+ optimization.modifier.launchlug.position = Pozycja
+ optimization.modifier.launchlug.position.desc = Optymalizuj po\u0142o\u017Cenie zaczepu startowego wzd\u0142u\u017C korpusu rakiety.
+
+
+ optimization.modifier.internalcomponent.position = Pozycja
+ optimization.modifier.internalcomponent.position.desc = Optymalizuj po\u0142o\u017Cenie wzgl\u0119dem cz\u0119\u015Bci podstawowej.
+
+ optimization.modifier.masscomponent.mass = Masa
+ optimization.modifier.masscomponent.mass.desc = Optymalizuj ci\u0119\u017Car balastu.
+
+ optimization.modifier.parachute.diameter = \u015Arednica
+ optimization.modifier.parachute.diameter.desc = Optymalizuj \u015Brednic\u0119 czaszy spadochronu.
+ optimization.modifier.parachute.coefficient = Wspó\u0142czynnik oporu
+ optimization.modifier.parachute.coefficient.desc = Optymalizuj wspó\u0142czynnik oporu spadochronu. Standardowe spadochrony maj\u0105 wspó\u0142czynnik oporu oko\u0142o 0,8.
+
+ optimization.modifier.streamer.length = D\u0142ugo\u015B\u0107
+ optimization.modifier.streamer.length.desc = Optymalizuj d\u0142ugo\u015B\u0107 ta\u015Bmy.
+ optimization.modifier.streamer.width = Szeroko\u015B\u0107
+ optimization.modifier.streamer.width.desc = Optymalizuj szeroko\u015B\u0107 ta\u015Bmy.
+ optimization.modifier.streamer.aspectRatio = Format
+ optimization.modifier.streamer.aspectRatio.desc = Optymalizuj format ta\u015Bmy (d\u0142ugo\u015B\u0107/szeroko\u015B\u0107). NIE nale\u017Cy jednocze\u015Bnie ustawia\u0107 poszczególnych wymiarów ta\u015Bmy oraz jej formatu.
+ optimization.modifier.streamer.coefficient = Wspó\u0142czynnik oporu
+ optimization.modifier.streamer.coefficient.desc = Optymalizuj wspó\u0142czynnik oporu ta\u015Bmy.
+
+ optimization.modifier.recoverydevice.deployDelay = Opó\u017Anienie aktywacji
+ optimization.modifier.recoverydevice.deployDelay.desc = Optymalizuj opó\u017Anienie aktywacji uk\u0142adu odzysku.
+ optimization.modifier.recoverydevice.deployAltitude = Wysoko\u015B\u0107 aktywacji
+ optimization.modifier.recoverydevice.deployAltitude.desc = Optymalizuj wysoko\u015B\u0107 aktywacji uk\u0142adu odzysku.
+
+ optimization.modifier.rocketcomponent.overrideMass = Wymu\u015B ci\u0119\u017Car
+ optimization.modifier.rocketcomponent.overrideMass.desc = Optymalizuj wymuszony ci\u0119\u017Car cz\u0119\u015Bci.
+ optimization.modifier.rocketcomponent.overrideCG = Wymu\u015B \u015AC
+ optimization.modifier.rocketcomponent.overrideCG.desc = Optymalizuj wymuszony \u015Brodek ci\u0119\u017Cko\u015Bci cz\u0119\u015Bci.
+
+ optimization.modifier.motormount.overhang = Wysuni\u0119cie silnika
+ optimization.modifier.motormount.overhang.desc = Optymalizuj wysuni\u0119cie silnika.
+ optimization.modifier.motormount.delay = Opó\u017Anienie zap\u0142onu silnika
+ optimization.modifier.motormount.delay.desc = Optymalizuj opó\u017Anienie zap\u0142onu silnika.
+
+
+
+
+ ! General rocket design optimization dialog
+
+ GeneralOptimizationDialog.title = Optymalizacja rakiety
+ GeneralOptimizationDialog.goal.maximize = Maksymalizuj warto\u015B\u0107
+ GeneralOptimizationDialog.goal.minimize = Minimalizuj warto\u015B\u0107
+ GeneralOptimizationDialog.goal.seek = D\u0105\u017C do warto\u015Bci
+ GeneralOptimizationDialog.btn.start = Rozpocznij optymalizacj\u0119
+ GeneralOptimizationDialog.btn.stop = Zatrzymaj optymalizacj\u0119
+ GeneralOptimizationDialog.lbl.paramsToOptimize = Parametry do optymalizacji:
+ GeneralOptimizationDialog.btn.add = Dodaj
+ GeneralOptimizationDialog.btn.add.ttip = Dodaj wybrany parametr do optymalizacji
+ GeneralOptimizationDialog.btn.remove = Usu\u0144
+ GeneralOptimizationDialog.btn.remove.ttip = Usu\u0144 wybrany parametr z listy do optymalizacji
+ GeneralOptimizationDialog.btn.removeAll = Usu\u0144 wszystko
+ GeneralOptimizationDialog.btn.removeAll.ttip = Usu\u0144 wszystkie parametry z listy do optymalizacji
+ GeneralOptimizationDialog.lbl.availableParams = Dost\u0119pne parametry:
+ GeneralOptimizationDialog.lbl.optimizationOpts = Opcje optymalizacji:
+ GeneralOptimizationDialog.lbl.optimizeSim = Optymalizuj symulacj\u0119:
+ GeneralOptimizationDialog.lbl.optimizeSim.ttip = Wybierz symulacj\u0119 do optymalizacji
+ GeneralOptimizationDialog.lbl.optimizeValue = Warto\u015B\u0107 optymalizowana:
+ GeneralOptimizationDialog.lbl.optimizeValue.ttip = Wybierz warto\u015B\u0107, która ma zosta\u0107 poddana optymalizacji
+ GeneralOptimizationDialog.lbl.optimizeGoal = Cel optymalizacji:
+ GeneralOptimizationDialog.lbl.optimizeGoal.ttip = Wybierz cel optymalizacji
+ GeneralOptimizationDialog.lbl.optimizeGoalValue.ttip = Dowolna warto\u015B\u0107, do której ma d\u0105\u017Cy\u0107 proces optymalizacji
+ GeneralOptimizationDialog.lbl.requireStability = Wymagana stabilno\u015B\u0107
+ GeneralOptimizationDialog.lbl.requireMinStability = Stabilno\u015B\u0107 minimalna:
+ GeneralOptimizationDialog.lbl.requireMinStability.ttip = Ustal minimalny zapas stabilno\u015Bci modelu
+ GeneralOptimizationDialog.lbl.requireMaxStability = Stabilno\u015B\u0107 maksymalna:
+ GeneralOptimizationDialog.lbl.requireMaxStability.ttip = Ustal maksymalny zapas stabilno\u015Bci modelu
+ GeneralOptimizationDialog.status.bestValue = Najlepsza warto\u015B\u0107:
+ GeneralOptimizationDialog.status.bestValue.ttip = Najlepsza dotychczas znaleziona warto\u015B\u0107 optymalizacji.
+ GeneralOptimizationDialog.status.stepCount = Liczba kroków:
+ GeneralOptimizationDialog.status.stepCount.ttip = Liczba przeprowadzonych kroków optymalizacji.
+ GeneralOptimizationDialog.status.evalCount = Ewaluacje:
+ GeneralOptimizationDialog.status.evalCount.ttip = Ca\u0142kowita liczba wykonanych ewaluacji funkcji (dla symulacji).
+ GeneralOptimizationDialog.status.stepSize = Wielko\u015B\u0107 kroku:
+ GeneralOptimizationDialog.status.stepSize.ttip = Wielko\u015B\u0107 bie\u017C\u0105cego kroku optymalizacji (w stosunku do zakresów parametru optymalizacji)
+ GeneralOptimizationDialog.btn.plotPath = Rysuj \u015Bcie\u017Ck\u0119 optymalizacji
+ GeneralOptimizationDialog.btn.plotPath.ttip = Rysuj wykres \u015Bcie\u017Cki optymalizacji (tylko jedno- i dwuwymiarowa optymalizacja)
+ GeneralOptimizationDialog.btn.save = Zapisz \u015Bcie\u017Ck\u0119
+ GeneralOptimizationDialog.btn.save.ttip = Zapisz wyniki ewaluacji funkcji (dla symulacji) jako plik CSV.
+ GeneralOptimizationDialog.btn.apply = Zastosuj optymalizacj\u0119
+ GeneralOptimizationDialog.btn.apply.ttip = Zastosuj wyniki optymalizacji do projektu rakiety
+ GeneralOptimizationDialog.btn.reset = Reset
+ GeneralOptimizationDialog.btn.reset.ttip = Przywró\u0107 projekt rakiety do stanu obecnego
+ GeneralOptimizationDialog.btn.close = Zamknij
+ GeneralOptimizationDialog.btn.close.ttip = Zamknij okno bez wprowadzania zmian do projektu rakiety
+ GeneralOptimizationDialog.error.selectParams.text = Wybierz parametry do optymalizowania spo\u015Bród dost\u0119pnych parametrów.
+ GeneralOptimizationDialog.error.selectParams.title = Wybierz parametry optymalizacji
+ GeneralOptimizationDialog.error.optimizationFailure.text = Optymalizacja nie zosta\u0142a przeprowadzona:
+ GeneralOptimizationDialog.error.optimizationFailure.title = Optymalizacja zako\u0144czy\u0142a si\u0119 niepowodzeniem
+ GeneralOptimizationDialog.undoText = Zastosuj optymalizacj\u0119
+ GeneralOptimizationDialog.basicSimulationName = Symulacja podstawowa
+ GeneralOptimizationDialog.noSimulationName = Brak symulacji
+ GeneralOptimizationDialog.table.col.parameter = Parametr
+ GeneralOptimizationDialog.table.col.current = Bie\u017C\u0105cy
+ GeneralOptimizationDialog.table.col.min = Minimalny
+ GeneralOptimizationDialog.table.col.max = Maksymalny
+ GeneralOptimizationDialog.export.header = Dodaj wiersz nag\u0142ówka
+ GeneralOptimizationDialog.export.header.ttip = Dodaj wiersz nag\u0142ówka jako pierwszy wiersz zawieraj\u0105cy opisy pól.
+ GeneralOptimizationDialog.export.stability = Stabilno\u015B\u0107
+
+
+ ! Dialog for plotting optimization results
+ OptimizationPlotDialog.title = Wyniki optymalizacji
+ OptimizationPlotDialog.lbl.zoomInstructions = Kliknij i przeci\u0105gnij w dó\u0142 + prawo aby powi\u0119kszy\u0107; góra + lewo aby pomniejszy\u0107
+ OptimizationPlotDialog.plot1d.title = Wynik optymalizacji
+ OptimizationPlotDialog.plot1d.series = Wynik optymalizacji
+ OptimizationPlotDialog.plot2d.title = \u015Acie\u017Cka optymalizacji
+ OptimizationPlotDialog.plot2d.path = \u015Acie\u017Cka optymalizacji
+ OptimizationPlotDialog.plot2d.evals = Ewaluacje
+ OptimizationPlotDialog.plot.ttip.stability = Stabilno\u015B\u0107:
+ OptimizationPlotDialog.plot.label.optimum = Optymalna
+
+ ! Optimization parameters
+ MaximumAltitudeParameter.name = Wysoko\u015B\u0107 apogeum
+ MaximumVelocityParameter.name = Pr\u0119dko\u015B\u0107 maksymalna
+ MaximumAccelerationParameter.name = Przyspieszenie maksymalne
+ StabilityParameter.name = Stabilno\u015B\u0107
+ GroundHitVelocityParameter.name = Pr\u0119dko\u015B\u0107 przyziemienia
+ LandingDistanceParameter.name = Oddalenie miejsca l\u0105dowania
+ TotalFlightTimeParameter.name = Ca\u0142kowity czas lotu
+ DeploymentVelocityParameter.name = Pr\u0119dko\u015B\u0107 w chwili wyzwolenia spadochronu
+
+
+ ! Compass directions drawn on a compass rose.
+ CompassRose.lbl.north = N
+ CompassRose.lbl.east = E
+ CompassRose.lbl.south = S
+ CompassRose.lbl.west = W
+
+ ! Compass directions with subdirections. These might not be localized even if the directions on the compass rose are.
+ CompassSelectionButton.lbl.N = N
+ CompassSelectionButton.lbl.NE = NE
+ CompassSelectionButton.lbl.E = E
+ CompassSelectionButton.lbl.SE = SE
+ CompassSelectionButton.lbl.S = S
+ CompassSelectionButton.lbl.SW = SW
+ CompassSelectionButton.lbl.W = W
+ CompassSelectionButton.lbl.NW = NW
+
+
+ SlideShowDialog.btn.next = Dalej
+ SlideShowDialog.btn.prev = Wstecz
+
+ SlideShowLinkListener.error.title = Nie znaleziono instrukcji
+ SlideShowLinkListener.error.msg = Przepraszamy, wybrana instrukcja nie zosta\u0142a jeszcze napisana.
+
+ GuidedTourSelectionDialog.title = Instrukcje krok po kroku
+ GuidedTourSelectionDialog.lbl.selectTour = Wybierz instrukcj\u0119 krok po kroku:
+ GuidedTourSelectionDialog.lbl.description = Opis instrukcji:
+ GuidedTourSelectionDialog.lbl.length = Liczba slajdów:
+ GuidedTourSelectionDialog.btn.start = Rozpocznij!
+
+
+ ! Custom Fin BMP Importer
+ CustomFinImport.button.label = Importuj z obrazka
+ CustomFinImport.badFinImage = Niew\u0142a\u015Bciwy obraz Statecznika. Upewnij si\u0119, \u017Ce kolor statecznika jest czarny lub ciemny, a kszta\u0142t statecznika przylega do dolnej kraw\u0119dzi obrazu.
+ CustomFinImport.errorLoadingFile = B\u0142\u0105d przy \u0142adowaniu pliku:
+ CustomFinImport.errorParsingFile = B\u0142\u0105d podczas przetwarzania obrazu statecznika:
+ CustomFinImport.undo = Importuj zestaw stateczników o niestandardowym kszta\u0142cie
+ CustomFinImport.error.title = B\u0142\u0105d podczas wgrywania profilu statecznika
+ CustomFinImport.error.badimage = Okre\u015Blenie kszta\u0142tu statecznika z obrazu nie by\u0142o mo\u017Cliwe
+ CustomFinImport.description = Obraz zostanie automatycznie zamieniony na czarno-bia\u0142y (statecznik w kolorze czarnym), wi\u0119c upewnij si\u0119, \u017Ce kszta\u0142t statecznika jest wype\u0142niony ciemnym kolorem, a t\u0142o jest bia\u0142e lub jasne. Podstawa statecznika musi przylega\u0107 do dolnej kraw\u0119dzi obrazu.
+
+
+ PresetModel.lbl.select = Wybierz ustawienia:
+ PresetModel.lbl.database = Z bazy danych...
+
+
+ ! Component Preset Chooser Dialog
+ ComponentPresetChooserDialog.title = Wybierz ustawienia cz\u0119\u015Bci
+ ComponentPresetChooserDialog.filter.label = Filtr:
+ ComponentPresetChooserDialog.checkbox.filterAftDiameter = Dopasuj tyln\u0105 \u015Brednic\u0119
+ ComponentPresetChooserDialog.checkbox.filterForeDiameter = Dopasuj przedni\u0105 \u015Brednic\u0119
+ ComponentPresetChooserDialog.menu.sortAsc = Szereguj rosn\u0105co
+ ComponentPresetChooserDialog.menu.sortDesc = Szereguj malej\u0105co
+ ComponentPresetChooserDialog.menu.units = Jednostki
+ ComponentPresetChooserDialog.checkbox.showAllCompatible = Poka\u017C wszystkie kompatybilne
+ table.column.Favorite = Ulubione
+ table.column.Manufacturer = Producent
+ table.column.PartNo = Numer cz\u0119\u015Bci
+ table.column.Description = Opis
+ table.column.Type = Typ
+ table.column.Length = D\u0142ugo\u015B\u0107
+ table.column.Width = Szeroko\u015B\u0107
+ table.column.InnerDiameter = \u015Arednica wewn\u0119trzna
+ table.column.OuterDiameter = \u015Arednica zewn\u0119trzna
+ table.column.AftOuterDiameter = Tylna \u015Brednica zewn\u0119trzna
+ table.column.AftShoulderLength = Tylna d\u0142ugo\u015B\u0107 wpustu
+ table.column.AftShoulderDiameter = Tylna \u015Brednica wpustu
+ table.column.ForeShoulderLength = Przednia d\u0142ugo\u015B\u0107 wpustu
+ table.column.ForeShoulderDiameter = Przednia \u015Brednica wpustu
+ table.column.ForeOuterDiameter = Przednia \u015Brednica zewn\u0119trzna
+ table.column.Shape = Kszta\u0142t
+ table.column.Material = Materia\u0142
+ table.column.Finish = Wyko\u0144czenie
+ table.column.Thickness = Grubo\u015B\u0107
+ table.column.Filled = Wype\u0142nione
+ table.column.Mass = Masa
+ table.column.Diameter = \u015Arednica
+ table.column.Sides = Boki
+ table.column.LineCount = Liczba linek
+ table.column.LineLength = D\u0142ugo\u015B\u0107 linki
+ table.column.LineMaterial = Materia\u0142 linek
+
projects / debian / openrocket / commitdiff