BasicFrame.dlg.lbl2 = ' has not been saved.
BasicFrame.dlg.lbl3 = Do you want to save it?
BasicFrame.dlg.title = Design not saved
+BasicFrame.StageName.Sustainer = Sustainer
+BasicFrame.WarningDialog.txt1 = The following problems were encountered while opening
+BasicFrame.WarningDialog.txt2 = Some design features may not have been loaded correctly.
+BasicFrame.WarningDialog.title = Warnings while opening file
! Labels used in buttons of dialog windows
button.ok = OK
bugreport.dlg.successmsg1 = Bug report successfully sent.
bugreport.dlg.successmsg2 = Thank you for helping make OpenRocket better!
bugreport.dlg.successmsg3 = Bug report sent
+bugreport.dlg.connectedInternet = <html>If connected to the Internet, you can simply click <em>Send bug report</em>.
+bugreport.dlg.otherwise = Otherwise, send the text below to the address:
+bugreport.lbl.Theinformation = The information above may be included in a public bug report. Make sure it does not contain any sensitive information you do not want to be made public.
+bugreport.dlg.failedmsg1 = OpenRocket was unable to send the bug report:
+bugreport.dlg.failedmsg2 = Please send the report manually to
+bugreport.dlg.failedmsg3 = Error sending report
+bugreport.reportDialog.txt = <html><b>You can report a bug in OpenRocket by filling in and submitting the form below.</b><br>You can also report bugs and include attachments on the project web site.
+bugreport.reportDialog.txt2 = <html><b>Please include a short description about what you were doing when the exception occurred.</b>
+
! Debug log dialog
debuglogdlg.but.clear = Clear
! Example design dialog
exdesigndlg.but.open = Open
+exdesigndlg.lbl.Selectexample = Select example designs to open:
+exdesigndlg.lbl.Openexampledesign = Open example design
+exdesigndlg.lbl.Exampledesignsnotfound = Example designs could not be found.
+exdesigndlg.lbl.Examplesnotfound = Examples not found
! Print panel dialog
printdlg.but.saveaspdf = Save as PDF
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.lbl.runsimfirst = Please run the simulation first.
simedtdlg.chart.Simflight = Simulated flight
simedtdlg.dlg.Simres = Simulation results
+simedtdlg.IntensityDesc.None = None
+simedtdlg.IntensityDesc.Verylow = Very low
+simedtdlg.IntensityDesc.Low = Low
+simedtdlg.IntensityDesc.Medium = Medium
+simedtdlg.IntensityDesc.High = High
+simedtdlg.IntensityDesc.Veryhigh = Very high
+simedtdlg.IntensityDesc.Extreme = Extreme
SimExpPan.lbl.Commentchar = Comment character:
SimExpPan.lbl.ttip.Commentchar = The character(s) that mark a comment line.
SimExpPan.but.Exporttofile = Export to file...
+SimExpPan.Fileexists.desc1 = File \"
+SimExpPan.Fileexists.desc2 = \" exists. Overwrite?
+SimExpPan.Fileexists.title = File exists
+SimExpPan.ExportingVar.desc1 = Exporting 1 variable out of
+SimExpPan.ExportingVar.desc2 = Exporting
+SimExpPan.ExportingVar.desc3 = variables out of
+SimExpPan.Col.Variable = Variable
+SimExpPan.Col.Unit = Unit
! MotorPlot
MotorPlot.title.Motorplot = Motor plot
simplotpanel.Desc = The data will be plotted in time order even if the X axis type is not time.
simplotpanel.OptionPane.lbl1 = A maximum of 15 plots is allowed.
simplotpanel.OptionPane.lbl2 = Cannot add plot
-
+simplotpanel.AUTO_NAME = Auto
+simplotpanel.LEFT_NAME = Left
+simplotpanel.RIGHT_NAME = Right
+simplotpanel.CUSTOM = Custom
! Component add buttons
compaddbuttons.Bodycompandfinsets = Body components and fin sets
ringcompcfg.radialdirectionfrom = The radial direction from the rocket centerline
ringcompcfg.but.Reset = Reset
ringcompcfg.but.Resetcomponant = Reset the component to the rocket centerline
+ringcompcfg.EngineBlock.desc = <html>An <b>engine block</b> stops the motor from moving forwards in the motor mount tube.<br><br>In order to add a motor, create a <b>body tube</b> or <b>inner tube</b> and mark it as a motor mount in the <em>Motor</em> tab.
+ringcompcfg.note.desc = Note: An inner tube will not affect the aerodynamics of the rocket even if it is located outside of the body tube.
+
! Body Tube Config
BodyTubecfg.lbl.Bodytubelength = Body tube length:
! ThrustCurveMotorSelectionPanel
TCMotorSelPan.lbl.Selrocketmotor = Select rocket motor:
TCMotorSelPan.checkbox.hideSimilar = Hide very similar thrust curves
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc1 = Show all motors
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc2 = Show motors with diameter less than that of the motor mount
+TCMotorSelPan.SHOW_DESCRIPTIONS.desc3 = Show motors with diameter equal to that of the motor mount
+TCMotorSelPan.lbl.Motormountdia = Motor mount diameter:
+TCMotorSelPan.lbl.Search = Search:
+TCMotorSelPan.lbl.Selectthrustcurve = Select thrust curve:
+TCMotorSelPan.lbl.Ejectionchargedelay = Ejection charge delay:
+TCMotorSelPan.equalsIgnoreCase.None = None
+TCMotorSelPan.lbl.NumberofsecondsorNone = (Number of seconds or \"None\")
+TCMotorSelPan.lbl.Totalimpulse = Total impulse:
+TCMotorSelPan.lbl.Avgthrust = Avg. thrust:
+TCMotorSelPan.lbl.Maxthrust = Max. thrust:
+TCMotorSelPan.lbl.Burntime = Burn time:
+TCMotorSelPan.lbl.Launchmass = Launch mass:
+TCMotorSelPan.lbl.Emptymass = Empty mass:
+TCMotorSelPan.lbl.Datapoints = Data points:
+TCMotorSelPan.lbl.Digest = Digest:
+TCMotorSelPan.title.Thrustcurve = Thrust curve:
+TCMotorSelPan.title.Thrust = Thrust
+TCMotorSelPan.delayBox.None = None
+
! PlotDialog
PlotDialog.title.Flightdataplot = Flight data plot
main.menu.debug = Debug
main.menu.debug.whatisthismenu = What is this menu?
main.menu.debug.createtestrocket = Create test rocket
+
+! database
+! Translate here all material database
+!
+
+! Material database
+! BULK_MATERIAL
+Databases.materials.Acrylic = Acrylic
+Databases.materials.Balsa = Balsa
+Databases.materials.Birch = Birch
+Databases.materials.Cardboard = Cardboard
+Databases.materials.Carbonfiber = Carbon fiber
+Databases.materials.Cork = Cork
+Databases.materials.DepronXPS = Depron (XPS)
+Databases.materials.Fiberglass = Fiberglass
+Databases.materials.Kraftphenolic = Kraft phenolic
+Databases.materials.Maple = Maple
+Databases.materials.Paperoffice = Paper (office)
+Databases.materials.Pine = Pine
+Databases.materials.Plywoodbirch = Plywood (birch)
+Databases.materials.PolycarbonateLexan = Polycarbonate (Lexan)
+Databases.materials.Polystyrene = Polystyrene
+Databases.materials.PVC = PVC
+Databases.materials.Spruce = Spruce
+Databases.materials.StyrofoamgenericEPS = Styrofoam (generic EPS)
+Databases.materials.StyrofoamBluefoamXPS = Styrofoam \"Blue foam\" (XPS)
+Databases.materials.Quantumtubing = Quantum tubing
+!SURFACE_MATERIAL
+Databases.materials.Ripstopnylon = Ripstop nylon
+Databases.materials.Mylar = Mylar
+Databases.materials.Polyethylenethin = Polyethylene (thin)
+Databases.materials.Polyethyleneheavy = Polyethylene (heavy)
+Databases.materials.Silk = Silk
+Databases.materials.Paperoffice = Paper (office)
+Databases.materials.Cellophane = Cellophane
+Databases.materials.Creape paper = Cr\u00eape paper
+! LINE_MATERIAL
+Databases.materials.Threadheavy-duty = Thread (heavy-duty)
+Databases.materials.Elasticcordround2mm = Elastic cord (round 2mm, 1/16 in)
+Databases.materials.Elasticcordflat6mm = Elastic cord (flat 6mm, 1/4 in)
+Databases.materials.Elasticcordflat12mm = Elastic cord (flat 12mm, 1/2 in)
+Databases.materials.Elasticcordflat19mm = Elastic cord (flat 19mm, 3/4 in)
+Databases.materials.Elasticcordflat25mm = Elastic cord (flat 25mm, 1 in)
+Databases.materials.Braidednylon2mm = Braided nylon (2 mm, 1/16 in)
+Databases.materials.Braidednylon3mm = Braided nylon (3 mm, 1/8 in)
+Databases.materials.Tubularnylon11mm = Tubular nylon (11 mm, 7/16 in)
+Databases.materials.Tubularnylon14mm = Tubular nylon (14 mm, 9/16 in)
+Databases.materials.Tubularnylon25mm = Tubular nylon (25 mm, 1 in)
+
+! ExternalComponent
+ExternalComponent.Rough = Rough
+ExternalComponent.Unfinished = Unfinished
+ExternalComponent.Regularpaint = Regular paint
+ExternalComponent.Smoothpaint = Smooth paint
+ExternalComponent.Polished = Polished
+
+! LineStyle
+LineStyle.Solid = Solid
+LineStyle.Dashed = Dashed
+LineStyle.Dotted = Dotted
+LineStyle.Dash-dotted = Dash-dotted
+LineStyle.Defaultstyle = Default style
+
+! Shape
+Shape.Conical = Conical
+Shape.Conical.desc1 = A conical nose cone has a profile of a triangle.
+Shape.Conical.desc2 = A conical transition has straight sides.
+Shape.Ogive = Ogive
+Shape.Ogive.desc1 = An ogive nose cone has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube, values less than 1 produce <b>secant ogives</b>.
+Shape.Ogive.desc2 = An ogive transition has a profile that is a segment of a circle. The shape parameter value 1 produces a <b>tangent ogive</b>, which has a smooth transition to the body tube at the aft end, values less than 1 produce <b>secant ogives</b>.
+Shape.Ellipsoid = Ellipsoid
+Shape.Ellipsoid.desc1 = An ellipsoidal nose cone has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>.
+Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×<i>Length</i> and <i>Diameter</i>. If the transition is not clipped, then the profile is extended at the center by the corresponding radius.
+Shape.Powerseries = Power series
+Shape.Powerseries.descA1 = 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>
+Shape.Powerseries.descA2 = -power</b> or <b>parabolic</b> nose cone, for <i>k</i>=0.75 a <b>
+Shape.Powerseries.descA3 = -power</b>, and for <i>k</i>=1 a <b>conical</b> nose cone.
+Shape.Powerseries.descB1 = 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>
+Shape.Powerseries.descB2 = -power</b> or <b>parabolic</b>, for <i>k</i>=0.75 a <b>
+Shape.Powerseries.descB3 = -power</b>, and for <i>k</i>=1 <b>conical</b>.
+Shape.Parabolicseries = Parabolic series
+Shape.Parabolicseries.desc1 = A parabolic series nose cone has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> nose cone.
+Shape.Parabolicseries.desc2 = A parabolic series transition has a profile of a parabola. The shape parameter defines the segment of the parabola to utilize. The shape parameter 1.0 produces a <b>full parabola</b> which is tangent to the body tube at the aft end, 0.75 produces a <b>3/4 parabola</b>, 0.5 procudes a <b>1/2 parabola</b> and 0 produces a <b>conical</b> transition.
+Shape.Haackseries = Haack series
+Shape.Haackseries.desc1 = The Haack series nose cones are designed to minimize drag. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> nose cone, which minimizes drag for fixed length and diameter, while a value of 0.333 produces an <b>LV-Haack</b> nose cone, which minimizes drag for fixed length and volume.
+Shape.Haackseries.desc2 = The Haack series <i>nose cones</i> are designed to minimize drag. These transition shapes are their equivalents, but do not necessarily produce optimal drag for transitions. The shape parameter 0 produces an <b>LD-Haack</b> or <b>Von Karman</b> shape, while a value of 0.333 produces an <b>LV-Haack</b> shape.
+
+
+! RocketComponent
+RocketComponent.Position.TOP = Top of the parent component
+RocketComponent.Position.MIDDLE = Middle of the parent component
+RocketComponent.Position.BOTTOM = Bottom of the parent component
+RocketComponent.Position.AFTER = After the parent component
+RocketComponent.Position.ABSOLUTE = Tip of the nose cone
+
+! LaunchLug
+LaunchLug.Launchlug = Launch lug
+! NoseCone
+NoseCone.NoseCone = Nose cone
+! Transition
+Transition.Transition = Transition
+!Stage
+Stage.Stage = Stage
+! BodyTube
+BodyTube.BodyTube = Body tube
+! TubeCoupler
+TubeCoupler.TubeCoupler = Tube coupler
+!InnerTube
+InnerTube.InnerTube = Inner Tube
+! TrapezoidFinSet
+TrapezoidFinSet.TrapezoidFinSet = Trapezoidal fin set
+! FreeformFinSet
+FreeformFinSet.FreeformFinSet = Freeform fin set
+!MassComponent
+MassComponent.MassComponent = Mass component
+! Parachute
+Parachute.Parachute = Parachute
+! ShockCord
+ShockCord.ShockCord = Shock cord
+! Bulkhead
+Bulkhead.Bulkhead = Bulkhead
+
+!Rocket
+Rocket.motorCount.Nomotor = [No motors]
+Rocket.compname.Rocket = Rocket
+
+!MotorMount
+MotorMount.IgnitionEvent.AUTOMATIC = Automatic (launch or ejection charge)
+MotorMount.IgnitionEvent.LAUNCH = Launch
+MotorMount.IgnitionEvent.EJECTION_CHARGE = First ejection charge of previous stage
+MotorMount.IgnitionEvent.BURNOUT = First burnout of previous stage
+MotorMount.IgnitionEvent.NEVER = Never
+
+!ComponentIcons
+ComponentIcons.Nosecone = Nose cone
+ComponentIcons.Bodytube = Body tube
+ComponentIcons.Transition = Transition
+ComponentIcons.Trapezoidalfinset = Trapezoidal fin set
+ComponentIcons.Ellipticalfinset = Elliptical fin set
+ComponentIcons.Freeformfinset = Freeform fin set
+ComponentIcons.Launchlug = Launch lug
+ComponentIcons.Innertube = Inner tube
+ComponentIcons.Tubecoupler = Tube coupler
+ComponentIcons.Centeringring = Centering ring
+ComponentIcons.Bulkhead = Bulk head
+ComponentIcons.Engineblock = Engine block
+ComponentIcons.Parachute = Parachute
+ComponentIcons.Streamer = Streamer
+ComponentIcons.Shockcord = Shock cord
+ComponentIcons.Masscomponent = Mass component
+ComponentIcons.disabled = (disabled)
+
+! StageAction
+StageAction.Stage = Stage
+
+! RecoveryDevice
+RecoveryDevice.DeployEvent.LAUNCH = Launch (plus NN seconds)
+RecoveryDevice.DeployEvent.EJECTION = First ejection charge of this stage
+RecoveryDevice.DeployEvent.APOGEE = Apogee
+RecoveryDevice.DeployEvent.ALTITUDE = Specific altitude during descent
+RecoveryDevice.DeployEvent.NEVER = Never
+
+! FlightEvent
+FlightEvent.Type.LAUNCH = Launch
+FlightEvent.Type.IGNITION = Motor ignition
+FlightEvent.Type.LIFTOFF = Lift-off
+FlightEvent.Type.LAUNCHROD = Launch rod clearance
+FlightEvent.Type.BURNOUT = Motor burnout
+FlightEvent.Type.EJECTION_CHARGE = Ejection charge
+FlightEvent.Type.STAGE_SEPARATION = Stage separation
+FlightEvent.Type.APOGEE = Apogee
+FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT = Recovery device deployment
+FlightEvent.Type.GROUND_HIT = Ground hit
+FlightEvent.Type.SIMULATION_END = Simulation end
+FlightEvent.Type.ALTITUDE = Altitude change
+
+! ThrustCurveMotorColumns
+TCurveMotorCol.MANUFACTURER = Manufacturer
+TCurveMotorCol.DESIGNATION = Designation
+TCurveMotorCol.TYPE = Type
+TCurveMotorCol.DIAMETER = Diameter
+TCurveMotorCol.LENGTH = Length
+
+! RocketInfo
+RocketInfo.lengthLine.Length = Length
+RocketInfo.lengthLine.maxdiameter = , max. diameter
+RocketInfo.massText1 = Mass with motors
+RocketInfo.massText2 = Mass with no motors
+RocketInfo.at = at M=
+RocketInfo.cgText = CG:
+RocketInfo.cpText = CP:
+RocketInfo.stabText = Stability:
+RocketInfo.Warning = Warning:
+RocketInfo.Calculating = Calculating...
+RocketInfo.Apogee = Apogee:
+RocketInfo.Maxvelocity = Max. velocity:
+RocketInfo.Maxacceleration = Max. acceleration:
+RocketInfo.apogeeValue = N/A
+RocketInfo.Mach = (Mach
+RocketInfo.velocityValue = N/A
+RocketInfo.accelerationValue = N/A
+
+! FinSet
+FinSet.CrossSection.SQUARE = Square
+FinSet.CrossSection.ROUNDED = Rounded
+FinSet.CrossSection.AIRFOIL = Airfoil
+FinSet.TabRelativePosition.FRONT = Root chord leading edge
+FinSet.TabRelativePosition.CENTER = Root chord midpoint
+FinSet.TabRelativePosition.END = Root chord trailing edge
+
+! FlightDataType
+FlightDataType.TYPE_TIME = Time
+FlightDataType.TYPE_ALTITUDE = Altitude
+FlightDataType.TYPE_VELOCITY_Z = Vertical velocity
+FlightDataType.TYPE_ACCELERATION_Z = Vertical acceleration
+FlightDataType.TYPE_VELOCITY_TOTAL = Total velocity
+FlightDataType.TYPE_ACCELERATION_TOTAL = Total acceleration
+FlightDataType.TYPE_POSITION_X = Position upwind
+FlightDataType.TYPE_POSITION_Y = Position parallel to wind
+FlightDataType.TYPE_POSITION_XY = Lateral distance
+FlightDataType.TYPE_POSITION_DIRECTION = Lateral direction
+FlightDataType.TYPE_VELOCITY_XY = Lateral velocity
+FlightDataType.TYPE_ACCELERATION_XY = Lateral acceleration
+FlightDataType.TYPE_AOA = Angle of attack
+FlightDataType.TYPE_ROLL_RATE = Roll rate
+FlightDataType.TYPE_PITCH_RATE = Pitch rate
+FlightDataType.TYPE_YAW_RATE = Yaw rate
+FlightDataType.TYPE_MASS = Mass
+FlightDataType.TYPE_LONGITUDINAL_INERTIA = Longitudinal moment of inertia
+FlightDataType.TYPE_ROTATIONAL_INERTIA = Rotational moment of inertia
+FlightDataType.TYPE_CP_LOCATION = CP location
+FlightDataType.TYPE_CG_LOCATION = CG location
+FlightDataType.TYPE_STABILITY = Stability margin calibers
+FlightDataType.TYPE_MACH_NUMBER = Mach number
+FlightDataType.TYPE_REYNOLDS_NUMBER = Reynolds number
+FlightDataType.TYPE_THRUST_FORCE = Thrust
+FlightDataType.TYPE_DRAG_FORCE = Drag force
+FlightDataType.TYPE_DRAG_COEFF = Drag coefficient
+FlightDataType.TYPE_AXIAL_DRAG_COEFF = Axial drag coefficient
+FlightDataType.TYPE_FRICTION_DRAG_COEFF = Friction drag coefficient
+FlightDataType.TYPE_PRESSURE_DRAG_COEFF = Pressure drag coefficient
+FlightDataType.TYPE_BASE_DRAG_COEFF = Base drag coefficient
+FlightDataType.TYPE_NORMAL_FORCE_COEFF = Normal force coefficient
+FlightDataType.TYPE_PITCH_MOMENT_COEFF = Pitch moment coefficient
+FlightDataType.TYPE_YAW_MOMENT_COEFF = Yaw moment coefficient
+FlightDataType.TYPE_SIDE_FORCE_COEFF = Side force coefficient
+FlightDataType.TYPE_ROLL_MOMENT_COEFF = Roll moment coefficient
+FlightDataType.TYPE_ROLL_FORCING_COEFF = Roll forcing coefficient
+FlightDataType.TYPE_ROLL_DAMPING_COEFF = Roll damping coefficient
+FlightDataType.TYPE_PITCH_DAMPING_MOMENT_COEFF = Pitch damping coefficient
+FlightDataType.TYPE_YAW_DAMPING_MOMENT_COEFF = Yaw damping coefficient
+FlightDataType.TYPE_REFERENCE_LENGTH = Reference lenght
+FlightDataType.TYPE_REFERENCE_AREA = Reference area
+FlightDataType.TYPE_ORIENTATION_THETA = Vertical orientation (zenith)
+FlightDataType.TYPE_ORIENTATION_PHI = Lateral orientation (azimuth)
+FlightDataType.TYPE_WIND_VELOCITY = Wind velocity
+FlightDataType.TYPE_AIR_TEMPERATURE = Air temperature
+FlightDataType.TYPE_AIR_PRESSURE = Air pressure
+FlightDataType.TYPE_SPEED_OF_SOUND = Speed of sound
+FlightDataType.TYPE_TIME_STEP = Simulation time step
+FlightDataType.TYPE_COMPUTATION_TIME = Computation time
+
+! PlotConfiguration
+PlotConfiguration.Verticalmotion = Vertical motion vs. time
+PlotConfiguration.Totalmotion = Total motion vs. time
+PlotConfiguration.Flightside = Flight side profile
+PlotConfiguration.Stability = Stability vs. time
+PlotConfiguration.Dragcoef = Drag coefficients vs. Mach number
+PlotConfiguration.Rollcharacteristics = Roll characteristics
+PlotConfiguration.Angleofattack = Angle of attack and orientation vs. time
+PlotConfiguration.Simulationtime = Simulation time step and computation time
+
+! Warning
+Warning.LargeAOA.str1 = Large angle of attack encountered.
+Warning.LargeAOA.str2 = Large angle of attack encountered (
+Warning.DISCONTINUITY = Discontinuity in rocket body diameter.
+Warning.THICK_FIN = Thick fins may not be modeled accurately.
+Warning.JAGGED_EDGED_FIN = Jagged-edged fin predictions may be inaccurate.
+Warning.LISTENERS_AFFECTED = Listeners modified the flight simulation
+Warning.RECOVERY_DEPLOYMENT_WHILE_BURNING = Recovery device opened while motor still burning.
+Warning.FILE_INVALID_PARAMETER = Invalid parameter encountered, ignoring.
projects / debian / openrocket / commitdiff