//NBAI F-22A Raptor Flight Model Version 2.0 by Michael MacIntyre - 5/28/2007 //Requires touchdown=fx_nicks_tchdwn_s, 1 effect file by Nick Needham [fltsim.0] title=NBAI_F22A_Raptor_Clean sim=NBAI_F22A_Raptor_AI_ONLY model=clean texture= atc_airline=Raptor atc_parking_codes=F22 atc_parking_types=MIL_COMBAT ui_manufacturer=Nick Black AI ui_type=F-22 Raptor ui_variation=Clean description=NBAI F-22 Raptor [fltsim.1] title=NBAI_F22A_Raptor_armed sim=NBAI_F22A_Raptor_AI_ONLY model=armed texture= atc_airline=Raptor atc_parking_codes=F22 atc_parking_types=MIL_COMBAT ui_manufacturer=Nick Black AI ui_type=F-22 Raptor ui_variation=Armed description=NBAI F-22 Raptor [fltsim.2] title=NBAI_F22A_Raptor_2tanks sim=NBAI_F22A_Raptor_AI_ONLY model=2tanks texture= atc_airline=Raptor atc_parking_codes=F22 atc_parking_types=MIL_COMBAT ui_manufacturer=Nick Black AI ui_type=F-22 Raptor ui_variation=2 Tanks description=NBAI F-22 Raptor [fltsim.3] title=NBAI_F22A_Raptor_4tanks_unarmed sim=NBAI_F22A_Raptor_AI_ONLY model=4tanks_unarmed texture= atc_airline=Raptor atc_parking_codes=F22 atc_parking_types=MIL_COMBAT ui_manufacturer=Nick Black AI ui_type=F-22 Raptor ui_variation=4 Tanks Unarmed description=NBAI F-22 Raptor [fltsim.4] title=NBAI_F22A_Raptor_4tanks_armed sim=NBAI_F22A_Raptor_AI_ONLY model=4tanks_armed texture= atc_airline=Raptor atc_parking_codes=F22 atc_parking_types=MIL_COMBAT ui_manufacturer=Nick Black AI ui_type=F-22 Raptor ui_variation=4 Tanks Armed description=NBAI F-22 Raptor [General] atc_type=silent atc_model=F22 editable=1 performance=Model Designer : Nick Black\nFlight model : Michael MacIntyre\nAI USE ONLY [WEIGHT_AND_BALANCE] max_gross_weight = 20450.0 // (pounds) empty_weight = 11700.0 // (pounds) reference_datum_position = 0, 0, 0 empty_weight_CG_position = -3.00, 0, 1.0 max_number_of_stations = 1 ;Moments of Inertia empty_weight_pitch_MOI = 90000 empty_weight_roll_MOI = 45000 empty_weight_yaw_MOI = 90000 empty_weight_coupled_MOI = 0.0 [GeneralEngineData] engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -8.3, -2.55, -1.5 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = -8.3, 2.55, -1.5 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency min_throttle_limit = -0.05 //Minimum percent throttle. Generally negative for turbine reverser max_contrail_temperature=-127 //Temperature (deg C) below which contrails may appear [TurbineEngineData] fuel_flow_gain = 0.0025 //Gain on fuel flow inlet_area = 4.2895 //Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 //RPM, second stage compressor rated value static_thrust = 5775 //Lbs, max rated static thrust at Sea Level afterburner_available = 1 //Afterburner available? reverser_available = 0 //Thrust reverser available? [jet_engine] thrust_scalar = 1.0 [Reference Speeds] flaps_up_stall_speed=130 //KTAS full_flaps_stall_speed=110 //KTAS cruise_speed=614 //KTAS max_indicated_speed=475 //KIAS max_mach=2.0 [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 static_pitch = 0 static_cg_height = 8.7 tailwheel_lock = 0 gear_system_type = 1 max_number_of_points = 3 point.0 = 1, 15.75, 0.00, -8.700, 1181.1, 0, 0.6349, 46.8, 0.2000, 2.500, 0.9100, 5.000, 5.000, 0.000, 260.000, 260.000 point.1 = 1, -7.30, -5.65, -8.800, 1574.8, 1, 0.6349, 0.0, 0.4000, 2.500, 0.5456, 4.000, 4.000, 2.000, 260.000, 260.000 point.2 = 1, -7.30, 5.65, -8.800, 1574.8, 2, 0.6349, 0.0, 0.4000, 2.500, 0.5456, 4.000, 4.000, 3.000, 260.000, 260.000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -15.00, -21.00, -0.90, fx_f16_navredm , light.1 = 3, -15.00, 21.00, -0.90, fx_f16_navgrem , light.2 = 3, -15.00, -21.00, -1.12, fx_f16_navredm , light.3 = 3, -15.00, 21.00, -1.12, fx_f16_navgrem , light.4 = 2, -15.00, -21.00, -0.90, fx_f16_strobeh , light.5 = 2, -15.00, 21.00, -0.90, fx_f16_strobeh , light.6 = 2, -15.00, -21.00, -1.12, fx_f16_strobeh , light.7 = 2, -15.00, 21.00, -1.12, fx_f16_strobeh , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_nicks_tchdwn_s, 1 [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 5 // seconds drag_scalar= 1.0 pitch_scalar= 1.0 flaps-position.0 = 0 // degrees flaps-position.1 = 27 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 1.0 //Brake scalar [fuel] Center1 = -6.9, 0.0, -1.5, 359.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = -1.8, -10.0, -1.5, 268.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -1.8, 10.0, -1.5, 268.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area = 312.0 //Square feet wing_span = 45.8 //Feet wing_root_chord = 9.9 //Feet wing_dihedral = 2.5 //Degrees wing_incidence = 0.5 //Degrees wing_twist = -1.5 //Degrees oswald_efficiency_factor= 0.8 //Measure of lift effeciency of wing wing_winglets_flag = 1 //Are winglets available? wing_sweep = 13.4 //Degrees, wing leading edge wing_pos_apex_lon = -31.5 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_area = 67.0 //Square feet htail_span = 17.2 //Feet htail_pos_lon = -59.1 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_incidence = 2.0 //Degrees htail_sweep = 25.0 //Degrees, horizontal tail leading edge vtail_area = 42.0 //Square feet vtail_span = 7.4 //Feet, tip to body vtail_sweep = 30.0 //Degrees, vertical tail leading edge vtail_pos_lon = -55.0 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 4.1 //Feet, vertical distance from reference point, positive going up elevator_area = 17.0 //Square feet aileron_area = 13.5 //Square feet rudder_area = 7.3 //Square feet elevator_up_limit = 17.0 //Degrees elevator_down_limit = 15.5 //Degrees aileron_up_limit = 18.0 //Degrees aileron_down_limit = 18.0 //Degrees rudder_limit = 30.0 //Degrees elevator_trim_limit = 15.0 //Degrees spoiler_limit = 60.0 //Degrees spoilerons_available = 1 //Spoilerons Available? aileron_to_spoileron_gain = 4.6 //Aileron to spoileron gain min_ailerons_for_spoilerons = 5 //Degrees min_flaps_for_spoilerons= 0.0 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 3.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 6.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1800.0 autothrottle_available= 1 autothrottle_arming_required= 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga= 0 pitch_takeoff_ga = 8; max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=11.00 nav_integrator_control=0.20 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 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 [stall_warning] type=2 [electrical] max_battery_voltage = 12.0 generator_alternator_voltage = 13.8 max_generator_alternator_amps = 40.0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus = 0, 5 , 9.5 avionics = 1, 5 , 9.5 additional_system = 0, 2 , 9.5 marker_beacon = 1, 2 , 9.0 fuel_pump = 0, 5 , 9.0 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 15.0 //Flap angle that activates warning at idle flap_limit_power = 30.0 //Flap angle that activates warning at above idle [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint = -16.385, -1.435, 3.012 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 0 Com.2 = 1, 0 Nav.1 = 1, 0, 1 Nav.2 = 1, 0, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [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 = 150, 250 aileron = 150, 250 rudder = 150, 250 [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=3,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 2 attitude_indicator.1 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0