[fltsim.0] title=F-107 sim=F-107 model= panel= sound= texture= kb_checklists= ui_manufacturer=North American atc_id_color=0000000000 visual_damage=0 description=The unusual looking F-107A was a excellent performing Mach 2 fighter bomber that lost out to the F=105 "Thud".\n [General] atc_type=USAF atc_model=F-107 editable=0 performance=Span: 36' 7\nLength:61' 10 "\nWeight: 22,696 lbs empty, 39,755 lbs gross\nSpeed: 1295 mph at 36000 ft\nRange:788 miles\nCeiling: 53,200 ft\nPower: P&W J-75-P-9, 17,200 lbs thrust dry, 24,500 with a\/b\nDesigner: P. Clawson\nDate:7\/2004 [weight_and_balance] // ACM V2.3 max_gross_weight = 41537 empty_weight = 22696 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 196385 empty_weight_roll_MOI = 175000 empty_weight_yaw_MOI = 250000 empty_weight_coupled_MOI = 1300 max_number_of_stations = 1 station_load.0 = 0.000000,0.000000,0.000000,0.000000 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -13.2, -18.34, -0.286, fx_navred , light.1 = 3, -13.2, 18.34, -0.286, fx_navgre , light.2 = 3, -24.86, 0.0, 6.3, fx_navwhi , light.3 = 4, 19.0, 0.00, 1.0, fx_vclight light.4 = 10, -10.0, 0.0, 0.0, fx_RCB_machenvlop,1 light.5 = 8, 6.5, 0, 0, fx_vapor_fa18 light.6 = 9, -24.5, 0, 0, fx_burner2 [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 1.000000 engine.0 = 0.000000,0.000000,0.000000 min_throttle_limit=0.100000 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 Center1 = 0, 0, 0, 300, 0 Center2 = 0, 0, 0, 300, 0 LeftMain = 0, 0, 0, 300, 0 RightMain = 0, 0, 0, 300, 0 electric_pump=0 [contact_points] static_pitch = 0.6 static_cg_height = 5 max_number_of_points = 8 point.0 = 1, 13.044, 0, -5.9776, 1181.102, 0, 0.79, 22, 0.946, 1.22, 0.441, 2, 3, 0, 0, 0 point.1 = 1, -3.6122, -4.1637, -6.4964, 1574.803, 1, 0.632, 0, 1.867, 1.7, 0.744, 2, 3, 2, 0, 0 point.2 = 1, -3.4558, 4.1623, -6.515, 1574.803, 2, 0.632, 0, 1.867, 1.7, 0.744, 2, 3, 3, 0, 0 point.3 = 2, -7.591, -18.1709, -1.2697, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -7.591, 18.0417, -1.2697, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -23.8931, 0, -2.2113, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 31.0695, 0, -0.6495, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.7 = 5.000, 13.192, 0.000, -6.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 3.0, 3.0, 0, 0.0, 0.0 gear_system_type=0 [keyboard_response] elevator = 150.000000, 250.000000 aileron = 150.000000, 250.000000 rudder = 150.000000, 250.000000 [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 = 00500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5.0 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1.0 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 [airplane_geometry] wing_area = 376.000000 wing_span = 36.66 wing_root_chord = 10.833333 wing_dihedral = 1.0 wing_incidence = -0.494385 wing_twist = 0.351563 oswald_efficiency_factor = 3.195582 wing_winglets_flag = 0 wing_sweep = 0.000000 wing_pos_apex_lon = 0.000000 wing_pos_apex_vert = 0.000000 htail_area = 230.000000 htail_span = 22.50000 htail_pos_lon = -17.10000 htail_pos_vert = 0.000000 htail_incidence = 0.000000 htail_sweep = 0.000000 vtail_area = 88.000000 vtail_span = 11.000 vtail_sweep = 0.000000 vtail_pos_lon = -17.33333 vtail_pos_vert = 6.333333 elevator_area = 50.000000 aileron_area = 16.080000 rudder_area = 88.000000 elevator_up_limit = 11.0 elevator_down_limit = 11.0 aileron_up_limit = 22.0 aileron_down_limit = 22.0 rudder_limit = 8.0 elevator_trim_limit = 19.480565 spoiler_limit = 59.988681 aileron_to_spoileron_gain = 0.000000 min_ailerons_for_spoilerons = 0.000000 min_flaps_for_spoilerons = 0.000000 spoilerons_available = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 electric_always_available = 0 [flight_tuning] elevator_effectiveness=1.3 aileron_effectiveness=0.8 rudder_effectiveness=1.0 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=39.992454,0.000000 [TurbineEngineData] fuel_flow_gain=0.002500 inlet_area=16.289500 rated_N2_rpm=29920.000000 static_thrust=17200.000000 afterburner_available=1 reverser_available=0 [jet_engine] thrust_scalar=1.30 [Reference Speeds] flaps_up_stall_speed=145.000000 full_flaps_stall_speed=116.000000 cruise_speed=380.786348 max_indicated_speed=810.000000 max_mach=2.500000 [Views] eyepoint=18.5, 0, 3.14 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=4800.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=110.000000 pitch_takeoff_ga=8.000000 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 [brakes] toe_brakes_scale=1.000031 parking_brake=1 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.12,0.11 ;Percent per second [TailHook] tailhook_length=4 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1.0 [exits] number_of_exits = 2 exit_rate.1 = 0.4 ;Percent per second exit_rate.0 = 0.4 ;Percent per second [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 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000