[fltsim.0] title=1US P-55A Ascender sim=Curtiss_XP-55 model= panel= sound= texture= KB_checklists = CheckList_P-55 Ascender atc_id=N700MS atc_airline=Army atc_flight_number=1123 atc_heavy=0 ui_manufacturer=Curtiss ui_type=XP55 description=1% Solution AssemblyLine Version 2.78Z4\n714VFTS & William Tell© Competition Certified\nP-55 Ascender [WEIGHT_AND_BALANCE] empty_weight = 7633 reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -0.060, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = 200, 1.959, 0.0, 2.5 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 6372 empty_weight_roll_MOI = 8346 empty_weight_yaw_MOI = 13186 empty_weight_coupled_MOI=0.000000 [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=80.000000 compression_ratio=6.650000 number_of_cylinders=28 max_rated_rpm=3000.000000 max_rated_hp=1800.000000 fuel_metering_type=0 cooling_type=1 normalized_starter_torque=0.035000 turbocharged=1 max_design_mp=44.499999 min_design_mp=12.000000 critical_altitude=19300.000000 emergency_boost_type=1 emergency_boost_mp_offset=2.000000 emergency_boost_gain_offset=0.540000 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 propeller_type=0 propeller_diameter=11.000000 propeller_blades=2 propeller_moi=28.450689 beta_max=65.000000 beta_min=15.000000 min_gov_rpm=1200.000000 prop_tc=0.010000 gear_reduction_ratio=2.227000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=700.000000 beta_feather=82.500000 power_absorbed_cf=0.900000 defeathering_accumulators_available=0 prop_reverse_available=0 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=1.000000,15.166667,0.000000,-6.916667,2574.803200,0,0.549823,2.0,0.261993,2.500000,1.038912,5.000000,5.000000,0.000000,0.000000,0.000000 point.1=1.000000,-1.083333,-7.000000,-7.333333,2968.504000,1.000000,0.549823,0.000000,0.491786,2.500000,0.831437,5.100000,5.100000,2.000000,0.000000,0.000000 point.2=1.000000,-1.083333,7.000000,-7.333333,2968.504000,2.000000,0.549823,0.000000,0.491786,2.500000,0.831437,5.000000,5.000000,3.000000,0.000000,0.000000 point.3=2, -.849,-19.158, -.681, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5 // left wing point.4=2, -.849, 19.158, -.681, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6 //right wing point.5=2, -20.049, 0.00, .290, 2400, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9 //tail point.6=2, 0, 0.00, -2.40, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4 //belly static_pitch=-1.466675 static_cg_height=5.747077 [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=16 // degrees, KIAS flaps-position.2=32 // degrees, KIAS flaps-position.3=45 // degrees, KIAS damaging-speed=191 // KIAS blowout-speed=290 // KIAS [Views] eyepoint=5.613312,0.000000,2.524709 [LIGHTS] panel= 2.100, 0.0, 1.90, fx_vclight [General] performance=Weight: 7833 lbs\nPower: 1800 hp\n8.0g Corner speed: 270 mph\nMax speed @ SL: 393 mph\nMax speed: 443 mph @ 19300 ft\nClimb rate: 4667 ft\/min @ 153 mph\ngregoryp\n1\/28\/02 05:23 PM [fuel] Center2=0.000000,0.000000,0.000000,120.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=235.000000 wing_span=44.083333 wing_root_chord=5.333333 wing_dihedral=4.476929 wing_incidence=0.999756 wing_twist=0.000000 oswald_efficiency_factor=0.883884 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=356.000000 htail_span=43.416667 htail_pos_lon=-60.083333 htail_pos_vert=0.000000 htail_incidence=-0.999756 htail_sweep=0.000000 vtail_area=333.000000 vtail_span=20.806249 vtail_sweep=0.000000 vtail_pos_lon=-52.750000 vtail_pos_vert=1.500000 elevator_area=183.080000 aileron_area=198.400000 rudder_area=116.550000 elevator_up_limit=35.000000 elevator_down_limit=30.000000 aileron_up_limit=15.000000 aileron_down_limit=15.000000 rudder_limit=30.000000 elevator_trim_limit=21.000000 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 [GeneralEngineData] engine_type=0 Engine.0=-7.500000,0.000000,-0.166667 fuel_flow_scalar=1.000000 [Reference Speeds] flaps_up_stall_speed=101.000000 full_flaps_stall_speed=80.800000 cruise_speed=326.271570 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0
