[fltsim.0] title=A-ST P-51D Whitehead Eagle sim=A-ST P-51D Whitehead Eagle model= panel= sound= texture= checklists= ui_manufacturer=A-ST P-51D Whitehead Eagle ui_type=North American P-51D Mustang ui_variation=Whitehead Eagle, FT-L, s/n 463607 description=The graceful North American P-51D Mustang considered as the epitome of fighters in WWII era. The famous "Whitehead Eagle" with code FT-L, s\/n 463607, 353FS, 354FG, 8AF. Superbly accurate model by Shigeru Tanaka. atc_heavy=0 atc_id=STP51D atc_airline=mustang atc_flight_number=FTL [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=7598.000 empty_weight_roll_MOI=9736.000 empty_weight_pitch_MOI=8185.000 empty_weight_yaw_MOI=10026.000 empty_weight_coupled_MOI=0.000 max_gross_weight=9212.000 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=0.7007007007007 rudder_effectiveness=0.0350709317 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 [fuel] Center1=-3.000, 0.000, 0.000, 85.000, 0.000 LeftMain=0.000, -5.100, 0.000, 92.000, 0.000 RightMain=0.000, 5.100, 0.000, 92.000, 0.000 fuel_type=1.000 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=228.000 wing_span=37.000 wing_root_chord=4.000 wing_dihedral=4.999 wing_incidence=1.000 wing_twist=-2.999 oswald_efficiency_factor=0.802 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=1.460 wing_pos_apex_vert=0.000 htail_area=28.000 htail_span=13.167 htail_pos_lon=-15.917 htail_pos_vert=0.000 htail_incidence=-0.247 htail_sweep=0.000 vtail_area=10.000 vtail_span=3.606 vtail_sweep=0.000 vtail_pos_lon=-17.500 vtail_pos_vert=3.167 elevator_area=13.050 aileron_area=12.730 rudder_area=7.0410 elevator_up_limit=30.000 elevator_down_limit=19.996 aileron_up_limit=30.000 aileron_down_limit=30.000 rudder_limit=30.000 elevator_trim_limit=17.997 spoiler_limit=57.296 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 [contact_points] point.0=1.000, -13.47, 0.000, -4.17510, 2165.354, 0.000, 0.564, 36.600, 0.537, 2.500, 0.341, 3.000, 3.000, 0.000, 0.000, 0.000 point.1=1.000, 2.250, -6.5400, -7.323, 2165.354, 1.000, 1.564, 0.000, 0.542, 2.500, 0.868, 3.000, 3.000, 2.000, 0.000, 0.000 point.2=1.000, 2.250, 6.5400, -7.323, 2165.354, 2.000, 1.564, 0.000, 0.542, 2.500, 0.868, 3.000, 3.000, 3.000, 0.000, 0.000 point.3=2.000, 0.000, -18.500, 0.000, 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, 18.500, 0.000, 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, -19.9167, 0.000, -0.600, 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, 9.250, 0.000, -1.917, 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_pitch=11.7233 static_cg_height=5.907 gear_system_type=1 [GeneralEngineData] engine_type=0 Engine.0=9.250, 0.000, 0.000 fuel_flow_scalar=1.000 min_throttle_limit=0.000000 [piston_engine] cylinder_displacement=137.500 compression_ratio=6.000 number_of_cylinders=12 max_rated_rpm=3000.000 max_rated_hp=1590.000 fuel_metering_type=2 cooling_type=1 normalized_starter_torque=0.025 turbocharged=1 max_design_mp=61.000 min_design_mp=1.000 critical_altitude=25000.000 emergency_boost_type=3 emergency_boost_mp_offset=6.000 emergency_boost_gain_offset=0.528 fuel_air_auto_mixture=1 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [propeller] propeller_type=0 propeller_diameter=11.167 propeller_blades=4 propeller_moi=58.000 beta_max=65.000 beta_min=23.000 min_gov_rpm=1800.000 prop_tc=0.010 gear_reduction_ratio=2.088 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=0.000 beta_feather=0.000 power_absorbed_cf=0.000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000 minimum_reverse_beta=0.000 [Reference Speeds] flaps_up_stall_speed=69.000 full_flaps_stall_speed=55.200 cruise_speed=293.002 max_indicated_speed=439.132813 [keyboard_response] elevator=350.000, 500.000 aileron=450.000, 1000.000 rudder=200.000, 1000.000 [Views] eyepoint=-2.576, 0.000, 1.820 [General] performance=Designer: Shigeru Tanaka\nModel file: stp51d.zip\nCopyright: Shigeru Tanaka\nProject: June 7, 2003\nEmail: wing.shigeru@nifty.ne.jp\nCopyright held lawfully by the author under the copyright laws applicable and concerned :\nDigital watermarking is the technology wherein copyright owner's identification information, copyright control information and the similar are embedded into digitally created data in such manner as not to be easily perceived, thereafter watermarking information is detected from the data at necessity, thereby copyright protection is duly conducted and effectively promoted.\nCopyright 2003 Shigeru Tanaka\n atc_type= atc_model= atc_model= [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000 autothrottle_available=0 pitch_takeoff_ga=8.000 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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.5, -19.3, -0.8, fx_navred light.1=3, 0.5, 19.3, -0.8, fx_navgre light.2=4, -2.24, 0.00, 2.20, fx_vclight [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=11.748, 0.000 flaps-position.2=23.497, 0.000 flaps-position.3=35.245, 0.000 flaps-position.4=46.994, 0.000 [brakes] toe_brakes_scale=1.000000 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=1,0,0,0 normal_pressure=6.930556 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [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
