From: bdureau Date: Mon, 14 Feb 2011 14:00:16 +0000 (+0000) Subject: I18 changes X-Git-Tag: upstream/1.1.6^2~13^2~6 X-Git-Url: https://git.gag.com/?a=commitdiff_plain;h=23b96c50e7906f26dd5f6108ac5de673b950563a;p=debian%2Fopenrocket I18 changes git-svn-id: https://openrocket.svn.sourceforge.net/svnroot/openrocket/branches/l10n@107 180e2498-e6e9-4542-8430-84ac67f01cd8 --- diff --git a/l10n/messages.properties b/l10n/messages.properties index 58428c25..65b4003e 100644 --- a/l10n/messages.properties +++ b/l10n/messages.properties @@ -68,6 +68,10 @@ BasicFrame.dlg.lbl1 = Design ' 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 @@ -91,6 +95,15 @@ bugreport.dlg.but.Sendbugreport.Ttip = Automatically send the bug report to the 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 = If connected to the Internet, you can simply click Send bug report. +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 = You can report a bug in OpenRocket by filling in and submitting the form below.
You can also report bugs and include attachments on the project web site. +bugreport.reportDialog.txt2 = Please include a short description about what you were doing when the exception occurred. + ! Debug log dialog debuglogdlg.but.clear = Clear @@ -120,6 +133,10 @@ edtmotorconfdlg.lbl.Leavenamedefault = Leave name empty for default. ! 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 @@ -198,6 +215,14 @@ 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 @@ -265,6 +290,13 @@ 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 @@ -328,6 +360,14 @@ SimExpPan.checkbox.ttip.Incflightevents = Include a comment line for every fligh 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 @@ -358,7 +398,10 @@ simplotpanel.but.ttip.Removethisplot = Remove this 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 @@ -443,6 +486,9 @@ ringcompcfg.Radialdirection = Radial direction 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 = An engine block stops the motor from moving forwards in the motor mount tube.

In order to add a motor, create a body tube or inner tube and mark it as a motor mount in the Motor 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: @@ -791,6 +837,27 @@ StorageOptChooser.lbl.Saveopt = Save options ! 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 @@ -832,3 +899,284 @@ main.menu.help.about = About 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 tangent ogive, which has a smooth transition to the body tube, values less than 1 produce secant ogives. +Shape.Ogive.desc2 = An ogive transition has a profile that is a segment of a circle. The shape parameter value 1 produces a tangent ogive, which has a smooth transition to the body tube at the aft end, values less than 1 produce secant ogives. +Shape.Ellipsoid = Ellipsoid +Shape.Ellipsoid.desc1 = An ellipsoidal nose cone has a profile of a half-ellipse with major axes of lengths 2×Length and Diameter. +Shape.Ellipsoid.desc2 = An ellipsoidal transition has a profile of a half-ellipse with major axes of lengths 2×Length and Diameter. 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 Radius × (x / Length)k where k is the shape parameter. For k=0.5 this is a +Shape.Powerseries.descA2 = -power or parabolic nose cone, for k=0.75 a +Shape.Powerseries.descA3 = -power, and for k=1 a conical nose cone. +Shape.Powerseries.descB1 = A power series transition has a profile of Radius × (x / Length)k where k is the shape parameter. For k=0.5 the transition is +Shape.Powerseries.descB2 = -power or parabolic, for k=0.75 a +Shape.Powerseries.descB3 = -power, and for k=1 conical. +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 full parabola which is tangent to the body tube, 0.75 produces a 3/4 parabola, 0.5 procudes a 1/2 parabola and 0 produces a conical 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 full parabola which is tangent to the body tube at the aft end, 0.75 produces a 3/4 parabola, 0.5 procudes a 1/2 parabola and 0 produces a conical transition. +Shape.Haackseries = Haack series +Shape.Haackseries.desc1 = The Haack series nose cones are designed to minimize drag. The shape parameter 0 produces an LD-Haack or Von Karman nose cone, which minimizes drag for fixed length and diameter, while a value of 0.333 produces an LV-Haack nose cone, which minimizes drag for fixed length and volume. +Shape.Haackseries.desc2 = The Haack series nose cones 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 LD-Haack or Von Karman shape, while a value of 0.333 produces an LV-Haack 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.