[fltsim.0] title=Republic P 47D-25 Thunderbolt Panther sim=P47D3_25 model=P47D3_25 [General] editable=0 [WEIGHT_AND_BALANCE] max_gross_weight= 19400.000 empty_weight= 10291.1 reference_datum_position= 8.980, 0.000, 0.000 empty_weight_CG_position= -8.980, 0.000, 0.000 max_number_of_stations= 50 station_load.0= 180.000, -13.400, 0.000, 0.000 empty_weight_roll_MOI= 8253.000 empty_weight_pitch_MOI= 13454.000 empty_weight_yaw_MOI= 17273.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] Center1= -8.350, 0.000, 0.000, 270.000, 0.000 Center2= -13.200, 0.000, 0.000, 100.000, 0.000 fuel_type= 1.000 number_of_tank_selectors= 1 [airplane_geometry] wing_area= 300.000 wing_span= 40.780 wing_root_chord= 9.170 wing_dihedral= 6.000 wing_incidence= 1.000 wing_twist= 0.000 oswald_efficiency_factor= 0.65 wing_winglets_flag= 0 wing_sweep= 3.000 wing_pos_apex_lon= -6.690 wing_pos_apex_vert= -1.890 htail_area= 33.000 htail_span= 16.000 htail_pos_lon= -27.720 htail_pos_vert= 0.945 htail_incidence= 2.000 htail_sweep= 19.000 vtail_area= 26.000 vtail_span= 6.000 vtail_sweep= 30.000 vtail_pos_lon= -27.240 vtail_pos_vert= 1.890 elevator_area= 22.000 aileron_area= 26.300 rudder_area= 11.920 elevator_up_limit= 30.000 elevator_down_limit= 20.000 aileron_up_limit= 16.000 aileron_down_limit= 12.000 rudder_limit= 28.000 elevator_trim_limit= 7.000 spoiler_limit= 0.000 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 3.00 system_type= 1 damaging-speed= 170.000 blowout-speed= 200.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000 flaps-position.1= 10.000 flaps-position.2= 20.000 flaps-position.3= 30.000 flaps-position.4= 40.000 [Reference Speeds] flaps_up_stall_speed= 100.0 full_flaps_stall_speed= 87.000 cruise_speed= 202.000 [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [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= 1.000, -28.100, 0.000, -3.9, 2165.354, 0.000, 0.551, 180.000, 0.327, 2.500, 0.390, 3.000, 3.000, 0.000, 175.000, 180.000 point.1= 1.000, -7.480, -7.670, -8.0, 2165.354, 1.000, 1.400, 0.000, 0.547, 2.500, 0.891, 6.500, 7.500, 2.000, 175.000, 180.000 point.2= 1.000, -7.480, 7.670, -8.0, 2165.354, 2.000, 1.400, 0.000, 0.547, 2.500, 0.891, 9.500, 9.500, 3.000, 175.000, 180.000 point.3= 2.000, 0.0, 0.000, 0.00, 2100.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.4= 2.000, -6.480, 0.000, -4.0, 3000.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.5= 2.000, -8.980, -20.333, 0.000, 800.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.6= 2.000, -8.980, 20.333, 0.000, 800.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.7= 2.000, -30.913, 0.000, 6.95, 700.102, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.8= 2.000, 0.37, 0.000, -4.5, 750.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.9= 2.000, -31.0, 0.000, -0.5, 1200.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.10= 2.000, -8.980, -10.333, 0.000, 1000.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.11= 2.000, -8.980, 10.333, 0.000, 1000.0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 static_pitch= 11.66 static_cg_height= 6.93 tailwheel_lock = 1 [GeneralEngineData] engine_type= 0 Engine.0= 0.37, 0.000, 0.000 [piston_engine] cylinder_displacement= 155.780 compression_ratio= 6.650 number_of_cylinders= 18 max_rated_rpm= 2700.000 max_rated_hp= 2000.000 fuel_metering_type= 2 cooling_type= 0 normalized_starter_torque= 0.025 turbocharged= 1 max_design_mp= 52.000 min_design_mp= 1.000 critical_altitude= 30000.000 emergency_boost_type= 1 emergency_boost_mp_offset= 4.000 emergency_boost_gain_offset= 0.528 fuel_air_auto_mixture= 0 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 power_scalar=1.000 fuel_flow_scalar= 1.000 [propeller] propeller_type= 0 propeller_diameter= 13.0 propeller_blades= 4 propeller_moi= 77.000 beta_max= 65.000 beta_min= 18.500 min_gov_rpm= 1400.000 prop_tc= 0.010 gear_reduction_ratio= 2.000 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= 700.000 beta_feather= 80.000 power_absorbed_cf= 0.000 defeathering_accumulators_available= 0 prop_reverse_available= 0 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 thrust_scalar=1.000 [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=200.000000,1000.000000 [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