[fltsim.0] title=Jaguar XK120 sim=jag120 model= panel= sound= texture=Black atc_type=ground atc_id_enable=1 atc_id=XK120 atc_model=Jag120 ui_variation=Black ui_type=Jaguar XK120 ui_manufacturer=Jaguar Ltd. description=An early Jaguar XK-120 by Sir William Lyons. The car was an immediate success and lived up to it's name by being able to achieve 120mph! [fltsim.1] title=Jaguar XK120 Paint 2 sim=jag120 model= panel= sound= texture=Red atc_type=ground atc_id_enable=1 atc_id=XK120 atc_model=Jag120 ui_variation=Red ui_type=Jaguar XK120 ui_manufacturer=Jaguar Ltd. description=An early Jaguar XK-120 by Sir William Lyons. The car was an immediate success and lived up to it's name by being able to achieve 120mph! [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [WEIGHT_AND_BALANCE] max_gross_weight=2550 // (pounds) empty_weight=2650 // (pounds) reference_datum_position=3.6, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-3.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=170, -3.0, -1.5, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, -3.0, 1.5, 0.0 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=0, -6.2, -1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=0, -6.2, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=0, -8.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=5400.0 empty_weight_roll_MOI=7137.0 empty_weight_yaw_MOI=2360.0 CG_forward_limit=0.000000 CG_aft_limit=1.000000 empty_weight_coupled_MOI=0.000000 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=6.0 induced_drag_scalar=5.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [piston_engine] power_scalar=3.0 //Piston power scalar cylinder_displacement=90.3 //Cubic inches per cylinder compression_ratio=8.5 //Compression ratio number_of_cylinders=6 //Number of cylinders max_rated_rpm=2400 //Max rated RPM max_rated_hp=230 //Max rated HP fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter 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=1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar=1.0 //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=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=6.8 //Propeller Diameter, (feet) propeller_blades=2 //Number of propeller blades propeller_moi=8.7 //Propeller moment of inertia beta_max=31.8 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=17.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=1400 //Miminum governed RPM prop_tc=0.1 //Prop time-constant gear_reduction_ratio=1.0 //Propeller gear reduction ratio fixed_pitch_beta=20 //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 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) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 //0 Class //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) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type [contact_points] point.0=1, 2.48, -9.50, -4.46, 4500, 1, 0.5, 23.0, 0.34, 5.5, 1.0, 0.0, 0.0, 0 point.1=1, 2.48, 9.50, -4.46, 4500, 2, 0.5, 23.0, 0.34, 5.5, 1.0, 0.0, 0.0, 0 point.2=1, -5.02, -9.50, -4.52, 4500, 1, 0.5, 0.0, 0.35, 5.5, 1.0, 0.0, 0.0, 2 point.3=1, -5.02, 9.50, -4.52, 4500, 2, 0.5, 0.0, 0.35, 5.5, 1.0, 0.0, 0.0, 3 point.4=4, 2.48, -4.50, -4.00, 4500, 0, 0.5, 23.0, 0.34, 5.5, 1.0, 0.0, 0.0, 0 point.5=4, 2.48, 4.50, -4.00, 4500, 0, 0.5, 23.0, 0.34, 5.5, 1.0, 0.0, 0.0, 0 point.6=4, -5.02, -9.50, -4.00, 4500, 1, 0.5, 0.0, 0.35, 5.5, 1.0, 0.0, 0.0, 2 point.7=4, -5.02, 9.50, -4.00, 4500, 2, 0.5, 0.0, 0.35, 5.5, 1.0, 0.0, 0.0, 3 //point.8=2, 2.48, -4.50, -2.46, 2500, 0, 0.0, 0.0, 0.0, 5.5, 1.0, 0.0, 0.0, 0 //point.9=2, 2.48, 4.50, -2.46, 2500, 0, 0.0, 0.0, 0.0, 5.5, 1.0, 0.0, 0.0, 0 //point.10=2, -15.02, -9.50, -2.52, 2500, 0, 0.0, 0.0, 0.0, 0, 0.0, 0.0, 0.0, 0 //point.11=1, -15.02, 9.50, -2.52, 2500, 0, 0.0, 0.0, 0.0, 0, 0.0, 0.0, 0.0, 0 static_pitch=0.000000 static_cg_height=0.000000 [Views] eyepoint=-1.5, 1.1, -0.4 //(feet) longitudinal, lateral, vertical distance from reference datum [EFFECTS] wake=fx_wakeboo water=fx_sprayboo dirt=fx_tchdrtboo concrete=fx_sparksboo touchdown=fx_tchdwn_sboo, 1boo [SMOKESYSTEM] smoke.0=0.0, -12.0, -2.40, fx_smoke_w [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=0 Com.1=1, 0 Nav.1=0, 0, 0 Adf.1=0 Transponder.1=0 Marker.1=0 [LIGHTS] panel=0.00, 0.30, 2.20, fx_vclightx nav_left=-5.52, 0.95,1.88, fx_navredx nav_right=5.52, 0.95, 1.88, fx_navgrex nav_tail=0.00, 1.85, -4.17, fx_navwhix strobe_left=-5.58, 0.98, 1.76, fx_strobelx strobe_right=5.58, 0.98, 1.76, fx_stroberx beacon=0.00, 1.95, -3.55, fx_beaconx [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=100, 180 aileron=200, 1000 rudder=200, 1000 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type=4 direction_indicator.0=1,0 //[fuel] //Center1=-2.6, 0.0, 0.0, 11.1, 0.0 //fuel_type=1.000000 //number_of_tank_selectors=1 [airplane_geometry] wing_area=39.000000 wing_span=6.083333 wing_root_chord=4.916670 wing_tip_chord=4.916670 wing_dihedral=1.735840 wing_incidence=-2.499634 wing_twist=-2.999268 oswald_efficiency_factor=0.708470 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=-2.371000 wing_pos_apex_vert=0.000000 htail_area=39.000000 htail_span=11.666667 htail_pos_lon=-18.266667 htail_pos_vert=0.000000 htail_incidence=3.246460 htail_sweep=0.000000 vtail_area=18.000000 vtail_pos_lon=-16.183333 vtail_pos_vert=1.500000 elevator_area=16.610000 aileron_area=18.300000 rudder_area=6.650000 elevator_up_limit=28.000447 elevator_down_limit=20.998903 aileron_up_limit=19.996227 aileron_down_limit=15.000035 rudder_limit=23.995472 elevator_trim_limit=19.497754 spoiler_limit=0.000000 vtail_span=4.837355 vtail_sweep=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [Flaps.0] type=1 span-outboard=0.500000 extending-time=1.500000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=12.666187,0.000000 flaps-position.2=25.332374,0.000000 flaps-position.3=37.998561,0.000000 [Reference Speeds] flaps_up_stall_speed=54.000000 full_flaps_stall_speed=43.200000 cruise_speed=118.800000 never_exceed_speed=166.320000 max_indicated_speed=180.000000 [General] performance=Maximum Speed\t120mph [GeneralEngineData] engine_type=0 Engine.0=2.400000,0.000000,0.000000 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 autoland_available=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 [fuel] LeftMain=-3.600000,0.000000,0.000000,20.000000,0.000000 RightMain=-3.600000,0.000000,0.000000,20.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [brakes] toe_brakes_scale=1.000000 parking_brake=1 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
