[fltsim.0] title=P-51A RAF sim=MkIA model=Brit panel= sound= texture=A kb_checklists= ui_manufacturer=North American description=The P51 was named Mustang by the British, and the first British version was designated Mustang I. British Mustangs were used till 1944 and the Allison engine powered models could outperform the Merlin-powered variants below 15,000 feet. [fltsim.1] title=P-51A US sim=MkIA model=US panel= sound= texture=A kb_checklists= ui_manufacturer=North American description=The P51MkIA was named Apache by the US . By comparison, Mustangs with the Allison engine could outperform the Merlin-powered variants below 15,000 feet. It was used in Africa, Italy and the far East.. [WEIGHT_AND_BALANCE] empty_weight = 4860 reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 empty_weight_roll_MOI=4650.000000 empty_weight_pitch_MOI=8185.000000 empty_weight_yaw_MOI=10026.000000 empty_weight_coupled_MOI=0.000000 max_gross_weight=7290.000000 reference_datum_position=0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=200, 0.0, 0.0, 3.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 4160 empty_weight_roll_MOI = 3924 empty_weight_yaw_MOI = 7518 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 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 [piston_engine] power_scalar=1.0 cylinder_displacement=142.500000 compression_ratio=6.650000 number_of_cylinders=12 max_rated_rpm=3000.000000 max_rated_hp=1200.000000 fuel_metering_type=0 cooling_type=1 normalized_starter_torque=0.035000 turbocharged=1 max_design_mp=53.999999 min_design_mp=1.000000 critical_altitude=21000.000000 emergency_boost_type=3 emergency_boost_mp_offset=6.100000 emergency_boost_gain_offset=0.540000 fuel_air_auto_mixture=1 auto_ignition=1 max_rpm_mechanical_efficiency_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=1.000000 idle_rpm_friction_scalar=1.000000 [propeller] thrust_scalar=1.0 propeller_type=0 propeller_diameter=11.167000 propeller_blades=3 propeller_moi=42.506502 beta_max=65.000000 beta_min=15.000000 min_gov_rpm=1200.000000 prop_tc=0.010000 gear_reduction_ratio=2.380000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0.000000 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [exits] number_of_exits=1 exit_rate.0=0.4 ;Percent per second [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=60.0 [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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) point.0=1, -20.21, 0.00, -1.2, 3200, 0, 0.30,180.0, 0.40, 2.5, 0.80, 7.5, 5.00, 0, 0, 135 point.1=1, 1.41, -5.86, -7.20, 2200, 1, 1.05, 0.0, 0.50, 2.5, 0.83, 2.5, 4.00, 2, 0, 135 point.2=1, 1.41, 5.86, -7.20, 2200, 2, 1.05, 0.0, 0.50, 2.5, 0.83, 2.5, 8.25, 3, 0, 135 point.3=2, 0.00,-20.00, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5 point.4=2, 0.00, 20.00, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6 point.5=2, -20.25, 0.00, 1.00, 2400, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9 point.6=2, 2.41, 0.00, -2.08, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4 static_cg_height = 6.12500 //(feet) altitude of CG when at rest (altitude when loaded on ground) static_pitch = 14.10 //degrees (pitch when loaded on ground) gear_system_type=1 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.12 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=14 // degrees, KIAS flaps-position.2=28 // degrees, KIAS flaps-position.3=42 // degrees, KIAS flaps-position.4=55 // degrees, KIAS damaging-speed=172 // KIAS blowout-speed=260 // KIAS [Views] eyepoint=-2.65,0.000000,2.25 [General] performance=Weight: 6433 lbs empty, 10,600 Max\nPower: 1200 hp Allison V-1710-81\nRange: 750 Miles, 2000 with Drop tanks\nCeiling: 31,350 ft\nMax speed:390 mph @ 20000 ft\nClimb rate: 20,000 feet in 9.1 minutes\n\nGMAX mdl by A.F.Scrub\nJanuary 2012\n Category=airplane [fuel] Center1=-3.000000,0.000000,0.000000,85.000000,0.000000 LeftMain=0.400000,-5.100000,0.000000,76.000000,0.000000 RightMain=0.400000,5.100000,0.000000,76.000000,0.000000 External1=-0.600000,-2.200000,-1.400000,125.000000,0.000000 External2=-0.600000,2.200000,-1.400000,125.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=235.000000 wing_span=37.000000 wing_root_chord=6.333333 wing_dihedral=4.998779 wing_incidence=0.000000 wing_twist=0.000000 oswald_efficiency_factor=0.890997 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=0.000000 htail_span=0.000000 htail_pos_lon=0.000000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=0.000000 vtail_span=0.000000 vtail_sweep=0.000000 vtail_pos_lon=0.000000 vtail_pos_vert=0.000000 elevator_area=13.050000 aileron_area=12.730000 rudder_area=10.410000 elevator_up_limit=30.000000 elevator_down_limit=20.000000 aileron_up_limit=15.000000 aileron_down_limit=15.000000 rudder_limit=30.000000 elevator_trim_limit=18.000000 spoiler_limit=60.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 auto_spoiler_available=0 spoiler_extension_time=0.000000 positive_g_limit_flaps_up=7.500000 positive_g_limit_flaps_down=5.000000 negative_g_limit_flaps_up=-6.000000 negative_g_limit_flaps_down=-5.000000 [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 [GeneralEngineData] engine_type=0 Engine.0=9.250000,0.000000,0.000000 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=80.000000 full_flaps_stall_speed=64.000000 cruise_speed=250.000000 max_indicated_speed=444.398438 [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=200.000000,1000.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 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 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=6.930556 [stall_warning] type=1 stick_shaker=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn startup=fx_engstrt [smokesystem] smoke.0= 0.00, -12.6, -20.70, fx_WingtipVortex smoke.1= 0.00, -12.6, 20.70, fx_WingtipVortex //smoke.0= 0.00, -1.6, -1.70, Fx_contrail_l //smoke.1= 0.00, -1.6, 1.70, Fx_contrail_l [LIGHTS] panel=0,-0.15,1.3, //#1=beacon #2=strobe #3=nav #10=reheat //#4=cockpit #5=landing #6=taxi //#7=recog #8=wing #9=logo //---------------originals---------------------------- light.0=4, 1.00, -18.2, -0.60, fx_navred light.1=4, 1.00, 18.2, -0.60, fx_navgre light.2=4, -6.66, 0.00, -3.20, fx_beacon light.3=4, -20.50, 0.00, 0.50, fx_strobeh light.4=5, 2.30, -5.30, -3.40, fx_landing //------------ ExhaustFlames--------uses wing/taxi/logo //index,type, long, lat, vert, fx_filename light.5=8, 5.25, -1.70, 0.60, fx_engstrt_jenny light.6=8, 5.25, 1.70, 0.60, fx_engstrt_jenny light.7=6, 5.15, -1.76, 0.60, fx_V12_MAX_port light.8=6, 5.15, 1.76, 0.60, fx_V12_MAX_starb light.9=9, 5.05, -1.72, 0.60, fx_V12_Exhaust light.10=9, 5.05, 1.72, 0.60, fx_V12_Exhaust //------------ Guns ----------------------uses strobe light.11=2, 1.55, 7.50, -1.50, fx_Wing_Guns light.12=2, 1.55, -7.50, -1.50, fx_Wing_Guns light.13=2, 1.55, 6.50, -1.50, fx_Wing_Guns light.14=2, 1.55, -6.50, -1.50, fx_Wing_Guns light.15=2, 9.55, 0.50, -1.20, fx_Wing_Guns light.16=2, 9.55, -0.50, -1.20, fx_Wing_Guns [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.000000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,1,1,1 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.000000 [deice_system] structural_deice_type=0
