[fltsim.0] title=P-38F Lightning sim=P38F_Lightning model= panel= sound= texture= KB_checklists=p38f_lightning_check description=The striking appearance and high performance of the U.S. Army's Lockheed P-38 Lightning made a powerful first impression. It used liquid-cooled engines, but its twin Allison V-12s made you feel a lot better about flying long distances over water. Twin-engine reliability and long range were big assets, particularly in the Pacific theater, where the top- scoring American aces, including Richard Bong and Thomas McGuire, were flying it to record numbers of victories. ui_manufacturer=Lockheed [WEIGHT_AND_BALANCE] empty_weight=12264 // (pounds) 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=170, -3.0, 0.0, 3.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=19696 empty_weight_roll_MOI=16104 empty_weight_yaw_MOI=29242 empty_weight_coupled_MOI=0.000000 max_gross_weight=18651.000000 [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=1325.000000 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=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 fuel_air_auto_mixture=0 auto_ignition=0 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 rotation= -1,1 //Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW propeller_type=0 propeller_diameter=11.500000 propeller_blades=3 propeller_moi=39.920000 beta_max=65.000000 beta_min=23.000000 min_gov_rpm=1800.000000 prop_tc=0.010000 gear_reduction_ratio=2.237000 fixed_pitch_beta=0.000000 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, 6.96, 0.00, -7.45, 1600, 0, 0.93, 37.7, 0.40, 2.5, 0.95, 2.5, 3.0, 0, 0, 152 point.1=1, -3.20, -8.12, -6.55, 2200, 1, 1.40, 0.0, 0.55, 2.5, 0.75, 5.5, 5.0, 2, 0, 152 point.2=1, -3.20, 8.12, -6.55, 2200, 2, 1.40, 0.0, 0.55, 2.5, 0.75, 6.5, 5.0, 3, 0, 152 point.3=2, 0.00,-26.25, 0.00, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5, 0, 0 point.4=2, 0.00, 26.25, 0.00, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6, 0, 0 point.5=2, -23.00, 0.00, -2.50, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9, 0, 0 point.6=2, 5.10, 0.00, -4.00, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4, 0, 0 static_cg_height=6.27 //(feet) altitude of CG when at rest (altitude when loaded on ground) static_pitch=6.39 //degrees (pitch when loaded on ground) gear_system_type=1 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.125 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=25 // degrees, KIAS flaps-position.2=50 // degrees, KIAS damaging-speed=191 // KIAS blowout-speed=290 // KIAS [Views] eyepoint=1.3,0.000000,2.58 [LIGHTS] panel=0.00, 0.10, 0.35, fx_vclight [General] performance=Weight: 12,264 \/ 15,900 lbs\nEngine: Two Allison V-1710-49\/53\nliquid-cooled V-12,\n1,325 hp each\nMax speed: 395 mph @ 25,000 ft\nCeiling: 39,000 ft\nInitial climb rate: 2,500 ft\/min\nRange: 900 miles or with drop\ntanks, 1,750 miles\n [fuel] Center1=1.000000,0.000000,0.300000,120.000000,0.000000 LeftMain=0.000000,-4.200000,0.300000,90.000000,0.000000 RightMain=0.000000,4.200000,0.300000,90.000000,0.000000 External1=-0.600000,-1.200000,-2.400000,150.000000,0.000000 External2=-0.600000,1.200000,-2.400000,150.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=358.000000 wing_span=52.000000 wing_root_chord=6.916667 wing_dihedral=5.097656 wing_incidence=0.999756 wing_twist=0.000000 oswald_efficiency_factor=0.749292 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=34.000000 htail_span=10.500000 htail_pos_lon=-17.666667 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=15.000000 vtail_span=4.415880 vtail_sweep=0.000000 vtail_pos_lon=-19.583333 vtail_pos_vert=3.250000 elevator_area=13.260000 aileron_area=18.900000 rudder_area=8.230000 elevator_up_limit=28.000447 elevator_down_limit=22.998526 aileron_up_limit=26.000825 aileron_down_limit=18.999280 rudder_limit=28.000447 elevator_trim_limit=19.996227 spoiler_limit=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [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=7.500000,-8.083333,0.000000 Engine.1=7.500000,8.083333,0.000000 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=64.000000 full_flaps_stall_speed=51.200000 cruise_speed=250.000000 max_indicated_speed=760.500000 [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=0 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=1,1,0,0 normal_pressure=6.930556 [stall_warning] type=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0
