[fltsim.0] title=VJPL Jeep ATV sim=banshee model= panel= sound= texture= atc_id=67CVJPL ui_manufacturer=VJPL ui_type=off road ui_variation=jeep visual_damage=0 atc_airline=VJPL atc_flight_number=001 description="This model should be used with respect for your fellow simmers keep off the runways when in use, head for the hills instead" visual_damage=0 [General] atc_type=Prototype atc_model=Off Road editable=1 performance=Maximum Speed 170 Category=airplane [CameraDefinition.0] Title = "Tail" Guid = {67bf6c33-9e4b-4d7c-ae70-1b9e43ab2b4f} Description = Looking forward from behind the aircraft Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = .75 ShowWeather = Yes InitialXyz = 0, 1.5, -15.0 InitialPbh = 5, 0, 0 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.1] Title = "Right Wing" Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59} Description = View from the right wing tip looking at the cockpit Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.5 ShowWeather = Yes InitialXyz = 7.8, 0.5, -1.2 InitialPbh = 0, 0, 280 XyzAdjust = TRUE Category=Aircraft MomentumEffect = TRUE ClipMode=Minimum [CameraDefinition.2] Title = "Left Wing" Guid = {99899ca9-8b9a-45bf-9f1a-42745a56ef00} Description = View from the left wing tip looking at the cockpit Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.5 ShowWeather = Yes InitialXyz = -7.8, 0.5, -1.2 InitialPbh = 0, 0, 80 XyzAdjust = TRUE Category=Aircraft MomentumEffect = TRUE ClipMode=Minimum [CameraDefinition.001] Title = "Rear Seat" Guid = {195EAB58-9E4A-4E2A-A34C-A8D9D948F078} Origin = Virtual Cockpit MomentumEffect = Yes SnapPbhAdjust = Swivel SnapPbhReturn = False PanPbhAdjust = Swivel PanPbhReturn = False Track = None ShowAxis = YES AllowZoom = TRUE InitialZoom = .75 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.60, 0.05, -0.30//lr/ud/bf InitialPbh=0, 0, 0 [flight_tuning] cruise_lift_scalar=0.000 parasite_drag_scalar=0.201 induced_drag_scalar=0.307 elevator_effectiveness=1.000 aileron_effectiveness=0.800 rudder_effectiveness=3.301 pitch_stability=2.002 roll_stability=1.500 yaw_stability=1.000 elevator_trim_effectiveness=2.002 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [airplane_geometry] wing_area=297.000 wing_span=41.500 wing_root_chord=7.917 wing_dihedral=0.999 wing_incidence=2.500 wing_twist=0.000 oswald_efficiency_factor=0.904 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=12.000 htail_span=12.250 htail_pos_lon=-16.417 htail_pos_vert=0.000 htail_incidence=-0.698 htail_sweep=0.000 vtail_area=129.000 vtail_span=6.140 vtail_sweep=0.000 vtail_pos_lon=0.917 vtail_pos_vert=1.500 elevator_area=12.820 aileron_area=0.070 rudder_area=8.230 elevator_up_limit=28.000 elevator_down_limit=20.999 aileron_up_limit=90.000 aileron_down_limit=90.000 rudder_limit=75.0 elevator_trim_limit=260.996 spoiler_limit=0.99.000 spoilerons_available=1 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 auto_spoiler_available=0 spoiler_extension_time=0.000000 positive_g_limit_flaps_up=10.000000 positive_g_limit_flaps_down=10.000000 negative_g_limit_flaps_up=-10.000000 negative_g_limit_flaps_down=-10.000000 [attitude_indicators] attitude_indicator.0=1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=000.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=100.000000 use_no_default_bank=1use_no_default_pitch=1 use_no_default_bank=1 default_bank_mode=0 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [brakes] toe_brakes_scale=1.5 parking_brake=1 [direction_indicators] direction_indicator.0=1,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=2, 0.95, 2.6, 1.85, smkst , [smokesystem] smoke.0 = -2.76, -2.17, -7.69, fx_noize [Flaps.0] type=0 span-outboard=45.500000 extending-time=2.000000 system_type=0 [fuel] LeftMain=0.000000,0.000000,0.000000,50.000000,0.000000 RightMain=0.000000,0.000000,0.000000,50.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=20.000000 flap_limit_idle=20.000000 [GeneralEngineData] engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -3.8, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 1.0 //Fuel flow scalar min_throttle_limit = -10.0 //Minimum percent throttle. Generally negative for turbine reverser [piston_engine] power_scalar = 1.5 //Piston power scalar cylinder_displacement= 182.75 //Cubic inches per cylinder compression_ratio= 7.5 //Compression ratio number_of_cylinders=6 //Number of cylinders max_rated_rpm= 3300 //Max rated RPM max_rated_hp= 165 //Max rated HP fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque= 0.3 //Starter torque factor turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp= 0 //Max design manifold pressure, (inHg) min_design_mp= 0 //Min design manifold pressure, (inHg) critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar= 0.60 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar= 1.8 //Scalar on maximum RPM friction idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type= 1 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 6.0 //Propeller Diameter, (feet) propeller_blades= 2 //Number of propeller blades propeller_moi= 3.78 //Propeller moment of inertia beta_max= 0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 0 //Miminum governed RPM prop_tc= 0.1 //Prop time-constant gear_reduction_ratio= 1.0 //Propeller gear reduction ratio fixed_pitch_beta= 13.75 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit= 80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available= 0 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available= 0 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available= 0 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather= 0 //Minimum RPM for prop feathering beta_feather= 0 //Feathering pitch angle (degrees) power_absorbed_cf= 0 //Coefficient of friction for power absorbed by propeller in feather defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta= 0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta= 0 //Minimum pitch angle in reverse, (degrees) [hydraulic_system] normal_pressure=100.000000 engine_map=1,0,0,0 [keyboard_response] elevator=0.000000,0.000000 aileron=0.000000,0.000000 rudder=0.000000,0.000000 [propeller] propeller_type=0 propeller_diameter=2.0 propeller_blades=2 propeller_moi=41.400 beta_max=31.800 beta_min=17.000 min_gov_rpm=1400.000 prop_tc=0.10 gear_reduction_ratio=2.850 fixed_pitch_beta=20.000 low_speed_theory_limit=80.000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=1 prop_auto_feathering_available=1 min_rpm_for_feather=0.000 beta_feather=0.000 power_absorbed_cf=0.000 defeathering_accumulators_available=0 prop_reverse_available=1 minimum_on_ground_beta=1.000 minimum_reverse_beta=-14.000 thrust_scalar=1.215 [Reference Speeds] flaps_up_stall_speed=0.000 full_flaps_stall_speed=00.000 cruise_speed=55.302 max_indicated_speed=76.500000 [SMOKESYSTEM] [stall_warning] type=0 stick_shaker=0 [turn_indicators] turn_indicator.0=1,0 [Views] eyepoint = 0.00, -1.10, .12 [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, -3.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=5355.000 empty_weight_roll_MOI=347252.000 empty_weight_pitch_MOI=16941.000 empty_weight_yaw_MOI=8764.000 empty_weight_coupled_MOI=0.000 max_gross_weight=855.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [contact_points] =wheel, 2=scrape, 3=float> //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) max_indicated_speed=597.656250 max_mach=0.839990 //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) point.0=1.00, 4.270, -2.550, -4.790, 1068.000, 1.00, 1.400, 30.000, 0.400, 2.500, 0.800, 10.000, 0.000, 0.000, 0.000, 0.000 point.1=1.00, 4.270, 2.550, -4.790, 1068.000, 0.00, 1.400, 30.000, 0.400, 2.500, 0.800, 10.000, 0.000, 1.000, 0.000, 0.000 point.2=1.00, -3.260, -2.550, -4.790, 1068.000, 2.00, 1.400, 30.000, 0.400, 2.500, 0.800, 10.000, 0.000, 2.000, 0.000, 0.000 point.3=1.00, -3.260, 2.550, -4.790, 1068.000, 0.00, 1.400, 30.000, 0.400, 2.500, 0.800, 10.000, 0.000, 3.000, 0.000, 0.000 point.4=4.000, -3.000, -2.250, -4.000, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000 point.5=4.000, -3.000, 2.250, -4.000, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 1.000, 0.000, 0.000 point.6=4.000, 2.350, -2.250, -4.000, 1068.000, 1.000, 0.512, 0.000, 0.800, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000 point.7=4.000, 2.350, 2.250, -4.000, 1068.000, 2.000, 0.512, 0.000, 0.800, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000 point.8=5, 0.0, 0.0, 0.0, 0, 0, 0.0, 0.0, 0.0, 0.0, 0.00, 3.00, 0.05, 0, 0.0, 0.0 static_pitch=0.000 static_cg_height=4.600 gear_system_type=0 // need this to enable wing folding // [folding_wings] // wing_fold_system_type=4 // fold_rates=0.5,0.5 ;Percent per second gear_system_type=0 // need this to enable tailhook [TailHook] tailhook_length=4 ;(feet) tailhook_position=-8.0, 0.0, -6.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1.0 [EFFECTS] [exits] number_of_exits=1 exit_rate.0=0.4 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot = 0, 5 , 12.0 avionics_bus = 0, 5 , 12.0 avionics = 1, 5 , 12.0 pitot_heat = 0, 2 , 12.0 additional_system = 0, 2 , 12.0 marker_beacon = 1, 2 , 12.0 fuel_pump = 0, 5 , 12.0 starter1 = 0, 20, 12.0 light_nav = 0, 5 , 12.0 light_beacon = 0, 5 , 12.0 light_landing = 0, 5 , 12.0 light_taxi = 0, 5 , 12.0 light_strobe = 0, 5 , 12.0 light_panel = 0, 5 , 12.0 max_battery_voltage = 12.0 generator_alternator_voltage = 16.0 max_generator_alternator_amps = 30.0 [Radios] Audio.1=1 Com.1=1,1 Com.2=0,1 Nav.1=1,1,0 Nav.2=1,1,0 Adf.1=1,1 Transponder.1=1 Marker.1=1 [pitot_static] pitot_heat=0.000000 [vacuum_system] max_pressure=5.000000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,1,1,1 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.000000 [deice_system] structural_deice_type=0