[fltsim.0] title = X-24A sim = X-24A model = panel = sound = texture = panel_alias = sound_alias = kb_checklists = kb_reference = atc_id = atc_id_color = 0xffffffff atc_parking_types = atc_parking_code = ui_manufacturer = Martin Marietta ui_type = X-24A ui_variation = USAF/NASA description = FS2004 MARTIN MARIETTA X-24A Lifting Body Research X-Plane from '60's -'70's. Built and flown to research re-entry spaceplane aerodynamics, and flight behaviour. The X-24A, along with the X-24B, HL-10, and M2-F series, provided valuable data for the Space Shuttle Program.These planes created lift from their flat fuselage bottoms an end fins, and were lifted aloft by NASA NB-52's to fly under rocket power, then gliding back to a runway. The X-24A, and it's stablemates, explored the lower end of the re-entry flight profile. The X-23 PRIME program explored the hypersonic and re-entry end of the re-entry profile. [General] atc_type = atc_model = editable = 1 performance = + Weight: 6500 lbs Max 11780 lbs + Power: 2120 lbs thrust + 8.0g Corner speed: 380 mph + Max speed @ SL: 806 mph + Max speed: 1036 mph @ 44000 ft + Climb rate: 3475 ft/min @ 806 mph Flight Dynamics By: Tim Piglet Conrad Piglet's Peculiar Planes FD Build 2 - 1/22/04 11:37 PM Flight Dynamics Workbook V2.84.50 [pitot_static] vertical_speed_time_constant = 2 [WEIGHT_AND_BALANCE] max_gross_weight = 11780 empty_weight = 6300 reference_datum_position = 0, 0, 0 empty_weight_CG_position = -0.2, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 2 station_load.0 = 200, 6, 0, 0, Pilot station_load.1 = 0, 0, 0, 0 empty_weight_pitch_MOI = 10663 empty_weight_roll_MOI = 1638 empty_weight_yaw_MOI = 11979 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 1 rudder_effectiveness = 1 pitch_stability = 1 roll_stability = 1 yaw_stability = 1 elevator_trim_effectiveness = 1 aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1 hi_alpha_on_roll = 1 hi_alpha_on_yaw = 1 p_factor_on_yaw = 1 torque_on_roll = 1 gyro_precession_on_roll = 1 gyro_precession_on_yaw = 1 [GeneralEngineData] engine_type = 1 Engine.0 = -10, 0, -0.17 Engine.1 = -10, 0, -0.85 Engine.2 = -10, -0.28, -0.54 Engine.3 = -10, 0.28, -0.54 fuel_flow_scalar = 35 min_throttle_limit = 0 max_contrail_temperature = 37 [TurbineEngineData] fuel_flow_gain = 0.1 inlet_area = 0.126662725391664 rated_N2_rpm = 20000 static_thrust = 2120 afterburner_available = 0 reverser_available = 0 [jet_engine] thrust_scalar = 1 [contact_points] max_number_of_points = 7 point.0 = 1, 7.61, 0, -5.3, 2500, 0, 0.7, 30, 0.3, 2.5, 0.95, 1.5, 5, 0, 254.64, 286.47 point.1 = 1, -1.72, -3.31, -5.3, 2500, 1, 0.9, 0, 0.4, 2.5, 0.7, 1.2, 6.5, 2, 254.64, 286.47 point.2 = 1, -1.72, 3.31, -5.3, 2500, 2, 0.9, 0, 0.4, 2.5, 0.7, 1.3, 5.5, 3, 254.64, 286.47 point.3 = 2, 2.66, 0, -2.36, 1250, 0, 0, 0, 0, 0, 0, 0, 0, 4 point.4 = 2, -11, 0, -1.7, 1250, 0, 0, 0, 0, 0, 0, 0, 0, 9 point.5 = 2, -2.7, -4.33, -2.2, 1250, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.6 = 2, -2.7, 4.33, -2.2, 1250, 0, 0, 0, 0, 0, 0, 0, 0, 6 static_pitch= 0 static_cg_height= 5.3 gear_system_type = 2 [Views] eyepoint= 6.9, 0, 2.335 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 11, 575 flaps-position.2 = 22, 550 flaps-position.3 = 33, 525 flaps-position.4 = 45, 500 damaging-speed = 575 blowout-speed = 625 system_type = 1 lift_scalar = 1 drag_scalar = 1 pitch_scalar = 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 electric_always_available = 1 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 4, 7.44, 0.00, 1.0, fx_vclight light.1 = 6, -11.10, 0.00, -.1, fx_hustler_burner light.2 = 7, -11.10, 0.00, -.827, fx_hustler_burner light.3 = 8, -11.10, -.313, -.466, fx_hustler_burner light.4 = 9, -11.10, .313, -.466, fx_hustler_burner [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 1 exit_rate.0 = 0.8 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 [autopilot] autopilot_available = 1 flight_director_available = 0 default_vertical_speed = 1000 autothrottle_available = 0 autothrottle_arming_required = 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8 max_pitch_velocity_hi_alt = 1.5 max_pitch_velocity_lo_alt_breakpoint = 20000 max_pitch_velocity_hi_alt_breakpoint = 28000 max_pitch = 10 max_pitch_acceleration = 1 max_pitch_velocity_lo_alt = 2 max_bank= 25 max_bank_acceleration = 1.8 max_bank_velocity = 3 max_throttle_rate = 0.1 nav_proportional_control = 9 nav_integrator_control = 0.25 nav_derivative_control = 0 nav_integrator_boundary = 2.5 nav_derivative_boundary = 0 gs_proportional_control = 9.52 gs_integrator_control = 0.26 gs_derivative_control = 0 gs_integrator_boundary = 0.7 gs_derivative_boundary = 0 yaw_damper_gain = 0 [fuel] LeftMain = 0, -2, 0.1, 390, 0 RightMain = 0, 2, 0.1, 390, 0 fuel_type = 2 number_of_tank_selectors = 1 electric_pump=0 [airplane_geometry] wing_area = 162 wing_span = 25.6666666666667 wing_root_chord = 6.31168831168831 wing_dihedral = 1 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.892125450108488 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 1.57792207792208 wing_pos_apex_vert = 0 htail_area = 20 htail_span = 5.2 htail_pos_lon = -15 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 25 vtail_span = 2.4 vtail_sweep = 0 vtail_pos_lon = -15 vtail_pos_vert = 0 elevator_area = 20 aileron_area = 14 rudder_area = 15 elevator_up_limit = 15 elevator_down_limit = 15 aileron_up_limit = 15 aileron_down_limit = 15 rudder_limit = 30 elevator_trim_limit = 18 spoiler_limit = 45 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 116.4 full_flaps_stall_speed = 116.4 cruise_speed = 229 max_indicated_speed = 1500 max_mach = 3.2856 [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 stick_shaker_magnitude = 5000 stick_shaker_direction = 0 stick_shaker_period = 111111 [gear_warning_system] gear_warning_available = 0 pct_throttle_limit = 0.1 flap_limit_idle = 33.75 flap_limit_power = 16.875 [brakes] toe_brakes_scale = 0.840888698995941 parking_brake = 1 [stall_warning] type = 1 [hydraulic_system] electric_pumps = 0 engine_map = 1, 1, 1, 1 normal_pressure = 3000 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
