[fltsim.0] title=Spitfire IX BAF sim=spitLF9e model= panel= sound= texture= KB_checklists= ui_manufacturer=Supermarine ui_type=Supermarine Spitfire MK IX ui_variation=BAF KB_checklists= kb_reference= atc_airline=air force atc_id=SM41 atc_flight_number= atc_heavy=0 description=LFIXb SM41 Belgian Air Force Fighter School, Coxyde, early 1950s. [WEIGHT_AND_BALANCE] empty_weight= 6180.000 reference_datum_position= 0.150, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0= 190.000, -5.000, 0.000, 0.500 ;Moments of Inertia empty_weight_pitch_MOI= 6286.000 empty_weight_roll_MOI= 3777.000 empty_weight_yaw_MOI= 8913.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 7192.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 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=1.0 cylinder_displacement= 137.500 compression_ratio= 6.000 number_of_cylinders= 12 max_rated_rpm= 3000.000 max_rated_hp= 1525.000 fuel_metering_type= 2 cooling_type= 1 normalized_starter_torque= 0.035 turbocharged= 1 max_design_mp= 61.000 min_design_mp= 12.000 critical_altitude= 21100.000 emergency_boost_type= 3 emergency_boost_mp_offset= 4.510 emergency_boost_gain_offset= 0.350 fuel_air_auto_mixture= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=1.000000 idle_rpm_friction_scalar=1.000000 [propeller] thrust_scalar=1.0 rotation=1 propeller_type= 0 propeller_diameter= 10.750 propeller_blades= 3 propeller_moi= 32.781 beta_max= 65.000 beta_min= 15.000 min_gov_rpm= 450.000 prop_tc= 0.010 gear_reduction_ratio= 2.096 fixed_pitch_beta= 20.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 70.000 beta_feather= 88.500 power_absorbed_cf= 0.900 defeathering_accumulators_available= 0 prop_reverse_available= 0 minimum_on_ground_beta= 1.000 minimum_reverse_beta= -14.000 [exits] number_of_exits=1 exit_rate.0=0.4 ;Percent per second [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=60.0 electric_always_available=1 [contact_points] //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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) point.0= 1.000, -18.250, 0.000, -2.800, 2165.354, 0.000, 0.551, 43.140, 0.547, 2.500, 0.456, 3.000, 3.000, 0.000, 0.000, 0.000 point.1= 1.000, 1.917, -4.000, -6.633, 2165.354, 1.000, 0.551, 0.000, 0.620, 2.500, 0.858, 5.000, 5.000, 2.000, 0.000, 0.000 point.2= 1.000, 1.917, 4.000, -6.633, 2165.354, 2.000, 0.551, 0.000, 0.620, 2.500, 0.858, 9.000, 9.000, 3.000, 0.000, 0.000 point.3= 2.000, 0.000, -18.250, -3.267, 1181.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, 0.000, 18.250, -3.267, 1181.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -24.000, 0.000, 0.000, 1181.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 8.017, 0.000, -2.033, 1181.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_cg_height= 5.450 static_pitch= 11.000 [Views] eyepoint=-3.900000,0.000000,2.11 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit panel=0.00, 0.10, -0.80, fx_vclight light.0=3, 1.65, -16.24, -0.55, fx_navred light.1=3, 1.65, 16.24, -0.55, fx_navgre light.2=2, 1.65, -16.24, -0.55, fx_strobe light.3=2, 1.65, 16.24, -0.55, fx_strobe light.4=3, -22.07, 0.00, 0.80, fx_navwhi light.5=1, -8.90, 0.00, 2.65, fx_beacon //top light.6=1, -0.96, 0.00, -2.95, fx_beacon //bottom light.7=4, 0.00, 0.10, -0.80, fx_vclight [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [SMOKESYSTEM] smoke.0=1.65,-11.24,-16.2, fx_contrail_spit smoke.1=1.65,-11.24, 16.2, fx_contrail_spit [forcefeedback] gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5# ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1# crash_magnitude1=10000 crash_direction1=1000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [General] atc_type=EXPERIMENTAL atc_model= editable=1 performance=Weight: 6562 lbs\nPower: 1525 hp\n7.5g Corner speed: 235 mph\nMax speed @ SL: 342 mph\nMax speed: 415 mph @ 21100 ft\nClimb rate: 4620 ft\/min @ 137 mph\nFlight Model By: Bill Wilson \/ gregoryp\n1\/7\/03 04:34 PM\nFlight Model Workbook V2.80.55\nAircraft by Paul Rebuffat\nTexture templates by Dan Swart\nRepaint by Paul Barry [fuel] Center2= 0.250, 0.000, -1.000, 101.000, 0.000 External1= -0.150, 0.000, -3.000, 36.000, 0.000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 231.000 wing_span= 32.583 wing_root_chord= 7.083 wing_dihedral= 4.999 wing_incidence= 2.000 wing_twist= 0.000 oswald_efficiency_factor= 0.980 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= -0.150 wing_pos_apex_vert= 0.000 htail_area= 27.000 htail_span= 13.000 htail_pos_lon= -17.400 htail_pos_vert= 0.000 htail_incidence= 1.000 htail_sweep= 0.000 vtail_area= 13.000 vtail_span= 4.111 vtail_sweep= 0.000 vtail_pos_lon= -17.400 vtail_pos_vert= 4.917 elevator_area= 18.200 aileron_area= 22.000 rudder_area= 9.900 elevator_up_limit= 28.000 elevator_down_limit= 23.000 aileron_up_limit= 26.000 aileron_down_limit= 19.000 rudder_limit= 28.500 elevator_trim_limit= 15.000 spoiler_limit= 0.000 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [GeneralEngineData] engine_type= 0 Engine.0= 9.100, 0.000, 0.000 fuel_flow_scalar= 1.000 [Reference Speeds] flaps_up_stall_speed= 92.000 full_flaps_stall_speed= 73.600 cruise_speed= 285.550 [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=200.000000,1000.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 5.000 system_type= 1 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 42.500, 0.000
