//******************************************************************** //* FSD T-38 TALON AIRCRAFT CONFIGURATION * //* For Flight Simulator 2002 * //* Copyright© 2002 By FSD International * //* All Rights Reserved * //******************************************************************** [fltsim.0] title=AT-38B Talon sim=FSD_TALON model= panel= sound= texture=A kb_checklists=T38A_check kb_reference= ui_manufacturer=Northrop ui_type=AT-38B ui_variation=#243-336 Sqn atc_id_enable=1 atc_id=243 editable=0 atc_heavy=0 atc_airline=Air Force atc_flight_number= description=Northrop AT-38B out of 479th Holloman AFB, NM. [fltsim.1] title=AT-38B Talon sim=FSD_TALON model= panel= sound= texture=136 kb_checklists=T38A_check kb_reference= ui_manufacturer=Northrop ui_type=F-5B ui_variation=#136-336 Sqn atc_id_enable=1 atc_id=136 editable=0 atc_heavy=0 atc_airline=Air Force atc_flight_number= description= [General] editable=0 atc_type=NORTHROP performance=Northrop T-38a TALON by FlightSim Developers (FSD). Aircraft Design by J. Owen Hewitt. Flight Dynamics by Steve Small. Panel and Gauges by Tim Dickens & FSD. NOTE : this file and all parts thereof is Copyright © the Authors & FSD International. No re-use of any parts of this archive is permitted. This file may NOT be uploaded or posted on any file server or included on CD-ROM or any other any media without the express written permission of the Authors. All Rights Reserved by FSD International and the Authors : Release date 12 July 2002 ... atc_model=F5 [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] reference_datum_position=0.0,0.0,0.0 empty_weight_CG_position=0.0,0.0,0.0 max_number_of_stations=2 station_load.0=200.0,-8.5.0,0.0,0.0 station_load.1=200.0,-1.5.0,0.0,0.0 empty_weight=8500.0 empty_weight_roll_MOI=13500.0 empty_weight_pitch_MOI=41000.0 empty_weight_yaw_MOI=77000.0 empty_weight_coupled_MOI=0.0 max_gross_weight= 12587.000 [fuel] //----------Fwd/Aft--L-R----Vert--Capacity-Unusable--- LeftMain= 1.3, 0.0, 0.0, 305.0, 10.0 RightMain= 1.3, 0.0, 0.0, 305.0, 10.0 fuel_type=2.0 number_of_tank_selectors=1 electric_pump=0 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 2.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.5 roll_stability = 1.0 yaw_stability = 2.0 elevator_trim_effectiveness = 2.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [airplane_geometry] wing_area=170.0 wing_span=25.3 wing_root_chord=7.0 wing_dihedral=0.7 wing_incidence=-2.2 wing_twist=0.0 oswald_efficiency_factor=0.73 wing_winglets_flag=0 wing_sweep=24.0 wing_pos_apex_lon=0.0 wing_pos_apex_vert=0.0 htail_area=47.0 htail_span=14.0 htail_pos_lon=-18.0 htail_pos_vert=0.0 htail_incidence=2.0 htail_sweep=24.0 vtail_area=77.0 vtail_span=7.9 vtail_sweep=45.0 vtail_pos_lon=-17.0 vtail_pos_vert=1.2 elevator_area=24.0 aileron_area=19.0 rudder_area=13.0 elevator_up_limit=19.0 elevator_down_limit=11.0 aileron_up_limit=19.0 aileron_down_limit=17.0 rudder_limit=31.0 elevator_trim_limit=21.5 spoiler_limit=45.0 spoilerons_available=0 aileron_to_spoileron_gain=0.0 min_ailerons_for_spoilerons=0.0 min_flaps_for_spoilerons=0.0 [pitot_static] vertical_speed_time_constant = 100 [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 // Gear 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0=1.0, 17.5 , 0.0, -6.05, 1900.0, 0.0, 0.5, 22.5, 0.3, 2.5, 1.5, 5.0, 5.0, 0.0, 0.0, 0.0 // Nose Gear point.1=1.0, -1.6, -5.0, -6.35, 2000.0, 1.0, 0.5, 0.0, 0.7, 2.5, 0.7, 5.0, 5.0, 2.0, 0.0, 0.0 // Left Mains point.2=1.0, -1.6, 5.0, -6.35, 2000.0, 2.0, 0.5, 0.0, 0.7, 2.5, 0.7, 5.0, 5.0, 3.0, 0.0, 0.0 // Right mains // Scrapes 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.3=2.0, -6.08,-12.67, -1.16, 1250.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0 // Wingtip Left point.4=2.0, -6.08, 12.67, -1.16, 1250.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0 // Wingtip Right point.5=2.0, -21.08, 0.00, -1.90, 1250.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0 // Exhaust Nozzle point.6=2.0, 22.59, 0.00, -1.63, 1250.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 // Nose point.7=2.0, -18.00, 0.00, 9.50, 1250.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0 0.0 // static_pitch=0.0 static_cg_height=5.8 gear_system_type=0 [Flaps.0] type=1 span-outboard=0.5 extending-time=5.0 system_type=1 flaps-position.0 = 0.0,0.0 flaps-position.1 = 19.5,0.0 flaps-position.2 = 39.0,0.0 damaging-speed=250 blowout-speed=280 lift_scalar=1.0 drag_scalar=1.0 pitch_scalar=1.0 system_type=1 [GeneralEngineData] engine_type = 1 Engine.0 = -22.0, -2.0, 0.0 Engine.1 = -22.0, 2.0, 0.0 fuel_flow_scalar=1.4 min_throttle_limit=0.000000 [TurbineEngineData] fuel_flow_gain = 0.003 inlet_area = 2.3 rated_N2_rpm = 29920 static_thrust = 2680 afterburner_available = 1 reverser_available = 0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [Reference Speeds] flaps_up_stall_speed=120.0 full_flaps_stall_speed=98.0 cruise_speed=550.0 max_indicated_speed=1000.000000 max_mach=2.100000 [keyboard_response] elevator=150.0,250.0 aileron=150.0,250.0 rudder=150.0,250.0 [Views] eyepoint = 10.45,0.00,1.4 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //The switch code, longitudinal, lateral, and vertical position (in feet), and the name of effect file light.0=3,-5.84,-12.36,-1.17,fx_navred_t38, light.1=3,-5.84,12.36,-1.17,fx_navgre_t38, light.2=3,6.79,0.00,-2.19,fx_navwhi_t38, light.3=3,-15.78,0.24,6.72,fx_navwhi_t38, light.4=3,-15.78,-0.24,6.72,fx_navwhi_t38, light.5=1,-14.56,0.00,6.16,fx_beacon_t38, light.6=4,7.00,0.00,0.95,fx_vclight_t38, light.7=4,12.00,0.00,0.75,fx_vclight_t38, light.8=1,9.02,0.00,-2.35,fx_beacon2_t38, [exits] number_of_exits = 1 exit_rate.0 = 0.5 [SMOKESYSTEM] smoke.0=0.00, -10.00, 12.69, fx_contrail_t38.fx smoke.1=0.00, -10.00, -12.69, fx_contrail_t38.fx [autopilot] autopilot_available= 1 use_no_default_pitch= 1 use_no_default_bank=1 flight_director_available= 1 default_vertical_speed= 3000.0 autothrottle_available = 1 autothrottle_arming_required = 0 autothrottle_takeoff_ga = 1 autothrottle_max_rpm= 150 pitch_takeoff_ga = 8; default_pitch_mode=0 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 [direction_indicators] direction_indicator.0 = 3,0 [electrical] ;BusType, MaxAmpLoad, MinVoltage ;BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) max_battery_voltage=24.0 min_battery_voltage=24.0 max_generator_alternator_amps=400.0 generator_alternator_voltage=28.0 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 [brakes] toe_brakes_scale=0.762963 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
