RocketActions.DelCompAct.ttip.Delete=Delete the selected component.
RocketActions.DelSimuAct.Delete=Delete
RocketActions.DelSimuAct.ttip.Delete=Delete the selected simulation.
RocketActions.DelAct.Delete=Delete
RocketActions.DelAct.ttip.Delete=Delete the selected component or simulation.
RocketActions.CutAction.Cut=Cut
RocketActions.CutAction.ttip.Cut=Cut this component or simulation to the clipboard and remove from this design
RocketActions.CopyAct.Copy=Copy
RocketActions.CopyAct.ttip.Copy=Copy this component (and subcomponents) to the clipboard.
RocketActions.PasteAct.Paste=Paste
RocketActions.PasteAct.ttip.Paste=Paste the component or simulation on the clipboard to the design.
RocketActions.EditAct.Edit=Edit
RocketActions.EditAct.ttip.Edit=Edit the selected component.
RocketActions.NewStageAct.Newstage=New stage
RocketActions.NewStageAct.ttip.Newstage=Add a new stage to the rocket design.
RocketActions.ActBoosterstage=Booster stage
RocketActions.MoveUpAct.Moveup=Move up
RocketActions.MoveUpAct.ttip.Moveup=Move this component upwards.
RocketActions.MoveDownAct.Movedown=Move down
RocketActions.MoveDownAct.ttip.Movedown=Move this component downwards.
! RocketPanel
RocketPanel.FigTypeAct.Sideview=Side view
RocketPanel.FigTypeAct.ttip.Sideview=Side view
RocketPanel.FigTypeAct.Backview=Back view
RocketPanel.FigTypeAct.ttip.Backview=Rear view
RocketPanel.lbl.Motorcfg=Motor configuration:
RocketPanel.lbl.infoMessage=<html>Click to select Shift+click to select other Double-click to edit Click+drag to move
bugreport.dlg.successmsg2=Thank you for helping make OpenRocket better!
bugreport.dlg.successmsg3=Bug report sent
bugreport.dlg.connectedInternet=<html>If connected to the Internet, you can simply click <em>Send bug report</em>.
bugreport.dlg.otherwise=Otherwise, send the text below to the address:
bugreport.lbl.Theinformation=The information above may be included in a public bug report. Make sure it does not contain any sensitive information you do not want to be made public.
bugreport.dlg.failedmsg1=OpenRocket was unable to send the bug report:
bugreport.dlg.failedmsg2=Please send the report manually to
bugreport.dlg.failedmsg3=Error sending report
bugreport.reportDialog.txt=<html><b>You can report a bug in OpenRocket by filling in and submitting the form below.</b><br>You can also report bugs and include attachments on the project web site.
bugreport.reportDialog.txt2=<html><b>Please include a short description about what you were doing when the exception occurred.</b>
pref.dlg.checkbox.Checkupdates=Check for software updates at startup
pref.dlg.ttip.Checkupdatesnow=Check for software updates now
pref.dlg.lbl.Selectprefunits=Select your preferred units:
pref.dlg.lbl.Rocketdimensions=Rocket dimensions:
pref.dlg.lbl.Linedensity=Line density:
pref.dlg.lbl.Motordimensions=Motor dimensions:
pref.dlg.lbl.Surfacedensity=Surface density:
pref.dlg.lbl.Distance=Distance:
pref.dlg.lbl.Bulkdensity=Bulk density::
pref.dlg.lbl.Velocity=Velocity:
pref.dlg.lbl.Surfaceroughness=Surface roughness:
pref.dlg.lbl.Acceleration=Acceleration:
pref.dlg.lbl.Area=Area:
pref.dlg.lbl.Mass=Mass:
pref.dlg.lbl.Angle=Angle:
pref.dlg.lbl.Force=Force:
pref.dlg.lbl.Rollrate=Roll rate:
pref.dlg.lbl.Totalimpulse=Total impulse:
pref.dlg.lbl.Temperature=Temperature:
pref.dlg.lbl.Momentofinertia=Moment of inertia:
pref.dlg.lbl.Pressure=Pressure:
pref.dlg.lbl.Stability=Stability:
pref.dlg.lbl.effect1=The effects will take place the next time you open a window.
pref.dlg.lbl.Checkingupdates=Checking for updates...
pref.dlg.lbl.msg1=An error occurred while communicating with the server.
pref.dlg.lbl.msg2=Unable to retrieve update information
pref.dlg.lbl.msg3=You are running the latest version of OpenRocket.
pref.dlg.lbl.msg4=No updates available
pref.dlg.PrefChoiseSelector1=Always ask
pref.dlg.PrefChoiseSelector2=Insert in middle
pref.dlg.PrefChoiseSelector3=Add to end
pref.dlg.PrefBooleanSelector1=Delete
pref.dlg.PrefBooleanSelector2=Confirm
pref.dlg.Add=Add
pref.dlg.DescriptionArea.Adddirectories=Add directories, RASP motor files (*.eng), RockSim engine files (*.rse) or ZIP archives separated by a semicolon (;) to load external thrust curves. Changes will take effect the next time you start OpenRocket.
! Simulation edit dialog
simedtdlg.but.runsimulation=Run simulation
simedtdlg.but.resettodefault=Reset to default
simedtdlg.but.add=Add
simedtdlg.but.remove=Remove
simedtdlg.title.Editsim=Edit simulation
simedtdlg.lbl.Simname=Simulation name:
simedtdlg.tab.Launchcond=Launch conditions
simedtdlg.tab.Simopt=Simulation options
simedtdlg.tab.Plotdata=Plot data
simedtdlg.tab.Exportdata=Export data
simedtdlg.lbl.Motorcfg=Motor configuration:
simedtdlg.lbl.ttip.Motorcfg=Select the motor configuration to use.
simedtdlg.combo.ttip.motorconf=Select the motor configuration to use.
simedtdlg.lbl.Wind=Wind
simedtdlg.lbl.Averwindspeed=Average windspeed:
simedtdlg.lbl.ttip.Averwindspeed=The average windspeed relative to the ground.
simedtdlg.lbl.Stddeviation=Standard deviation:
simedtdlg.lbl.ttip.Stddeviation=<html>The standard deviation of the windspeed.<br>The windspeed is within twice the standard deviation from the average for 95% of the time.
simedtdlg.lbl.ttip.Temperature=The temperature at the launch site.
simedtdlg.lbl.Pressure=Pressure:
simedtdlg.lbl.ttip.Pressure=The atmospheric pressure at the launch site.
simedtdlg.lbl.Launchsite=Launch site
simedtdlg.lbl.Latitude=Latitude:
simedtdlg.lbl.ttip.Latitude=<html>The launch site latitude affects the gravitational pull of Earth.<br>Positive values are on the Northern hemisphere, negative values on the Southern hemisphere.
simedtdlg.lbl.Altitude=Altitude:
simedtdlg.lbl.ttip.Altitude=<html>The launch altitude above mean sea level.<br>This affects the position of the rocket in the atmospheric model.
simedtdlg.border.Launchrod=Launch rod
simedtdlg.lbl.Length=Length:
simedtdlg.lbl.ttip.Length=The length of the launch rod.
simedtdlg.lbl.Angle=Angle:
simedtdlg.lbl.ttip.Angle=The angle of the launch rod from vertical.
simedtdlg.lbl.Direction=Direction:
simedtdlg.lbl.ttip.Direction1=<html>Direction of the launch rod relative to the wind.<br>
simedtdlg.lbl.ttip.Direction2== towards the wind,
simedtdlg.lbl.ttip.Direction3== downwind.
simedtdlg.border.Simopt=Simulator options
simedtdlg.lbl.Calcmethod=Calculation method:
simedtdlg.lbl.ttip.Calcmethod=<html>The Extended Barrowman method calculates aerodynamic forces according <br>to the Barrowman equations extended to accommodate more components.
simedtdlg.lbl.ExtBarrowman=Extended Barrowman
simedtdlg.lbl.Simmethod=Simulation method:
simedtdlg.lbl.ttip.Simmethod1=<html>The six degree-of-freedom simulator allows the rocket total freedom during flight.<br>
simedtdlg.lbl.ttip.Simmethod2=Integration is performed using a 4<sup>th</sup> order Runge-Kutta 4 numerical integration.
simedtdlg.lbl.Timestep=Time step:
simedtdlg.lbl.ttip.Timestep1=<html>The time between simulation steps.<br>A smaller time step results in a more accurate but slower simulation.<br>
simedtdlg.lbl.ttip.Timestep2=The 4<sup>th</sup> order simulation method is quite accurate with a time step of
simedtdlg.but.ttip.resettodefault=Reset the time step to its default value (
simedtdlg.border.Simlist=Simulator listeners
simedtdlg.txt.longA1=<html><i>Simulation listeners</i> is an advanced feature that allows user-written code to listen to and interact with the simulation.
simedtdlg.txt.longA2=For details on writing simulation listeners, see the OpenRocket technical documentation.
simedtdlg.lbl.Curlist=Current listeners:
simedtdlg.lbl.Addsimlist=Add simulation listener
simedtdlg.lbl.Noflightdata=No flight data available.
simedtdlg.lbl.runsimfirst=Please run the simulation first.
simedtdlg.chart.Simflight=Simulated flight
simedtdlg.dlg.Simres=Simulation results
simedtdlg.IntensityDesc.None=None
simedtdlg.IntensityDesc.Verylow=Very low
simedtdlg.IntensityDesc.Low=Low
simedtdlg.IntensityDesc.Medium=Medium
simedtdlg.IntensityDesc.High=High
simedtdlg.IntensityDesc.Veryhigh=Very high
simedtdlg.IntensityDesc.Extreme=Extreme
! Simulation Panel
simpanel.but.newsimulation=New simulation
simpanel.but.editsimulation=Edit simulation
simpanel.but.runsimulations=Run simulations
simpanel.but.deletesimulations=Delete simulations
simpanel.but.plotexport=Plot / export
simpanel.but.ttip.newsimulation=Add a new simulation
simpanel.but.ttip.editsim=Edit the selected simulation
simpanel.but.ttip.runsimu=Re-run the selected simulations
simpanel.but.ttip.deletesim=Delete the selected simulations
simpanel.checkbox.donotask=Do not ask me again
simpanel.lbl.defpref=You can change the default operation in the preferences.
simpanel.dlg.lbl.DeleteSim1=Delete the selected simulations?
simpanel.dlg.lbl.DeleteSim2=<html><i>This operation cannot be undone.</i>
simpanel.dlg.lbl.DeleteSim3=Delete simulations
simpanel.col.Name=Name
simpanel.col.Motors=Motors
simpanel.col.Apogee=Apogee
simpanel.col.Maxvelocity=Max. velocity
simpanel.col.Maxacceleration=Max. acceleration
simpanel.col.Timetoapogee=Time to apogee
simpanel.col.Flighttime=Flight time
simpanel.col.Groundhitvelocity=Ground hit velocity
! SimulationRunDialog
SimuRunDlg.title.RunSim=Running simulations...
SimuRunDlg.lbl.Running=Running ...
SimuRunDlg.lbl.Simutime=Simulation time:
SimuRunDlg.lbl.Altitude=Altitude:
SimuRunDlg.lbl.Velocity=Velocity:
SimuRunDlg.msg.Unabletosim=Unable to simulate:
SimuRunDlg.msg.errorOccurred=An error occurred during the simulation:
SimuRunDlg.msg.AnException1=An exception occurred during the simulation:
SimuRunDlg.msg.AnException2=Please report this as a bug along with the details below.
SimuRunDlg.msg.AssertionError1=A computation error occurred during the simulation.
SimuRunDlg.msg.AssertionError2=Please report this as a bug along with the details below.
SimuRunDlg.msg.unknownerror1=An unknown error was encountered during the simulation.
SimuRunDlg.msg.unknownerror2=The program may be unstable, you should save all your designs and restart OpenRocket now!
! SimulationExportPanel
SimExpPan.desc=Comma Separated Files (*.csv)
SimExpPan.border.Vartoexport=Variables to export
SimExpPan.but.Selectall=Select all
SimExpPan.but.Selectnone=Select none
SimExpPan.border.Fieldsep=Field separator
SimExpPan.lbl.Fieldsepstr=Field separator string:
SimExpPan.lbl.longA1=<html>The string used to separate the fields in the exported file.<br>
SimExpPan.lbl.longA2=Use ',' for a Comma Separated Values (CSV) file.
ringcompcfg.radialdirectionfrom=The radial direction from the rocket centerline
ringcompcfg.but.Reset=Reset
ringcompcfg.but.Resetcomponant=Reset the component to the rocket centerline
ringcompcfg.EngineBlock.desc=<html>An <b>engine block</b> stops the motor from moving forwards in the motor mount tube.<br><br>In order to add a motor, create a <b>body tube</b> or <b>inner tube</b> and mark it as a motor mount in the <em>Motor</em> tab.
ringcompcfg.note.desc=Note: An inner tube will not affect the aerodynamics of the rocket even if it is located outside of the body tube.
Databases.materials.Braidednylon2mm=Braided nylon (2 mm, 1/16 in)
Databases.materials.Braidednylon3mm=Braided nylon (3 mm, 1/8 in)
Databases.materials.Tubularnylon11mm=Tubular nylon (11 mm, 7/16 in)
Databases.materials.Tubularnylon14mm=Tubular nylon (14 mm, 9/16 in)
Databases.materials.Tubularnylon25mm=Tubular nylon (25 mm, 1 in)
! ExternalComponent
ExternalComponent.Rough=Rough
ExternalComponent.Unfinished=Unfinished
ExternalComponent.Regularpaint=Regular paint
ExternalComponent.Smoothpaint=Smooth paint
ExternalComponent.Polished=Polished
! LineStyle
LineStyle.Solid=Solid
LineStyle.Dashed=Dashed
LineStyle.Dotted=Dotted
LineStyle.Dash-dotted=Dash-dotted
LineStyle.Defaultstyle=Default style
! Shape
Shape.Conical=Conical
Shape.Conical.desc1=A conical nose cone has a profile of a triangle.
Shape.Conical.desc2=A conical transition has straight sides.
Shape.Ogive=Ogive
Shape.Ogive.desc1=An ogive nose cone has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube, values less than 1 produce <b>secant ogives</b>.
Shape.Ogive.desc2=An ogive transition has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube at the aft end, values less than 1 produce <b>secant ogives</b>.
Shape.Ellipsoid=Ellipsoid
Shape.Ellipsoid.desc1=An ellipsoidal nose cone has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>.
Shape.Ellipsoid.desc2=An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>. If the transition is not clipped, then the profile is extended at the center by the corresponding radius.
Shape.Powerseries=Power series
Shape.Powerseries.desc1=A power series nose cone has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 this is a <b>\u00BD-power</b> or <b>parabolic</b> nose cone, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 a <b>conical</b> nose cone.
Shape.Powerseries.desc2=A power series transition has a profile of <i>Radius</i> × (<i>x</i> / <i>Length</i>)<sup><i>k</i></sup> where <i>k</i> is the shape parameter. For <i>k</i>=0.5 the transition is <b>\u00BD-power</b> or <b>parabolic</b>, for <i>k</i>=0.75 a <b>\u00BE-power</b>, and for <i>k</i>=1 <b>conical</b>.
Shape.Parabolicseries=Parabolic series
Shape.Parabolicseries.desc1=A parabolic series nose cone has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> nose cone.
Shape.Parabolicseries.desc2=A parabolic series transition has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube at the aft end, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> transition.
Shape.Haackseries=Haack series
Shape.Haackseries.desc1=The Haack series nose cones are designed to minimize drag. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> nose cone, which minimizes drag for fixed length and diameter, while a value of 0.333 produces an <b>LV-Haack</b> nose cone, which minimizes drag for fixed length and volume.
Shape.Haackseries.desc2=The Haack series <i>nose cones</i> are designed to minimize drag. These transition shapes are their equivalents, but do not necessarily produce optimal drag for transitions. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> shape, while a value of 0.333 produces an <b>LV-Haack</b> shape.
! RocketComponent
RocketComponent.Position.TOP=Top of the parent component
RocketComponent.Position.MIDDLE=Middle of the parent component
RocketComponent.Position.BOTTOM=Bottom of the parent component
RocketComponent.Position.AFTER=After the parent component
RocketComponent.Position.ABSOLUTE=Tip of the nose cone
! LaunchLug
LaunchLug.Launchlug=Launch lug
! NoseCone
NoseCone.NoseCone=Nose cone
! Transition
Transition.Transition=Transition
!Stage
Stage.Stage=Stage
! BodyTube
BodyTube.BodyTube=Body tube
! TubeCoupler
TubeCoupler.TubeCoupler=Tube coupler
!InnerTube
InnerTube.InnerTube=Inner Tube
! TrapezoidFinSet
TrapezoidFinSet.TrapezoidFinSet=Trapezoidal fin set
! FreeformFinSet
FreeformFinSet.FreeformFinSet=Freeform fin set
!MassComponent
MassComponent.MassComponent=Mass component
! Parachute
Parachute.Parachute=Parachute
! ShockCord
ShockCord.ShockCord=Shock cord
! Bulkhead
Bulkhead.Bulkhead=Bulkhead
!Rocket
Rocket.motorCount.Nomotor=[No motors]
Rocket.compname.Rocket=Rocket
!MotorMount
MotorMount.IgnitionEvent.AUTOMATIC=Automatic (launch or ejection charge)
MotorMount.IgnitionEvent.LAUNCH=Launch
MotorMount.IgnitionEvent.EJECTION_CHARGE=First ejection charge of previous stage
MotorMount.IgnitionEvent.BURNOUT=First burnout of previous stage
MotorMount.IgnitionEvent.NEVER=Never
!ComponentIcons
ComponentIcons.Nosecone=Nose cone
ComponentIcons.Bodytube=Body tube
ComponentIcons.Transition=Transition
ComponentIcons.Trapezoidalfinset=Trapezoidal fin set
ComponentIcons.Ellipticalfinset=Elliptical fin set
ComponentIcons.Freeformfinset=Freeform fin set
ComponentIcons.Launchlug=Launch lug
ComponentIcons.Innertube=Inner tube
ComponentIcons.Tubecoupler=Tube coupler
ComponentIcons.Centeringring=Centering ring
ComponentIcons.Bulkhead=Bulk head
ComponentIcons.Engineblock=Engine block
ComponentIcons.Parachute=Parachute
ComponentIcons.Streamer=Streamer
ComponentIcons.Shockcord=Shock cord
ComponentIcons.Masscomponent=Mass component
ComponentIcons.disabled=(disabled)
! StageAction
StageAction.Stage=Stage
! RecoveryDevice
RecoveryDevice.DeployEvent.LAUNCH=Launch (plus NN seconds)
RecoveryDevice.DeployEvent.EJECTION=First ejection charge of this stage
RecoveryDevice.DeployEvent.APOGEE=Apogee
RecoveryDevice.DeployEvent.ALTITUDE=Specific altitude during descent
