[fltsim.0] title=Hs P75 Combat sim=hsp75 model= panel= sound= texture= kb_checklists=hsp75_check kb_reference=hsp75_ref atc_id=E400HE atc_airline= atc_flight_number= ui_manufacturer=Henschel ui_type=Hs P75 Heavy Fighter ui_variation=Combat visual_damage=1 description=Hs P 75 in Standard Combat colours atc_heavy=0 atc_id=M000EX atc_airline= atc_flight_number= [fltsim.1] title=Hs P75 Desert Combat sim=hsp75 model= panel= sound= texture=1 kb_checklists=hsp75_check kb_reference=hsp75_ref atc_id=E400HE atc_airline= atc_flight_number= ui_manufacturer=Henschel ui_type=Hs P75 Heavy Fighter ui_variation=Desert Combat visual_damage=1 description=Hs P 75 in Desert Combat colours. atc_heavy=0 atc_id=M000EX atc_airline= atc_flight_number= [fltsim.2] title=Hs P75 Aero Racer sim=hsp75 model= panel= sound= texture=2 kb_checklists=hsp75_check kb_reference=hsp75_ref atc_id=E400HE atc_airline= atc_flight_number= ui_manufacturer=Henschel ui_type=Hs P75 Heavy Fighter ui_variation=Aero Racer visual_damage=1 description=Fictional Aero racer. atc_heavy=0 atc_id=M000EX atc_airline= atc_flight_number= [WEIGHT_AND_BALANCE] empty_weight= 12264.000 reference_datum_position= -3.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0= 170.000, -3.000, 0.000, 3.000 ;Moments of Inertia empty_weight_pitch_MOI= 19696.000 empty_weight_roll_MOI= 16104.000 empty_weight_yaw_MOI= 29242.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 17919.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.500 aileron_effectiveness=1.500 rudder_effectiveness=1.500 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [piston_engine] power_scalar=2.002 cylinder_displacement= 226.000 compression_ratio= 7.000 number_of_cylinders= 12 max_rated_rpm= 3000.000 max_rated_hp= 2700.000 fuel_metering_type= 0 cooling_type= 1 normalized_starter_torque= 0.035 turbocharged= 1 max_design_mp= 54.000 min_design_mp= 1.000 critical_altitude= 21000.000 emergency_boost_type= 0 emergency_boost_mp_offset= 0.000 emergency_boost_gain_offset= 0.000 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 [propeller] thrust_scalar=1.907 rotation=-1 //Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW propeller_type= 0 propeller_diameter= 14.000 propeller_blades= 3 propeller_moi= 122.000 beta_max= 65.000 beta_min= 23.000 min_gov_rpm= 1800.000 prop_tc= 0.010 gear_reduction_ratio= 2.237 fixed_pitch_beta= 0.000 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 [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= 1.000, 23.800, 0.000, -9.400, 1600.000, 0.000, 1.250, 30.000, 0.400, 2.500, 1.800, 2.500, 3.000, 0.000, 0.000, 0.000 point.1= 1.000, -1.140, -8.230, -9.400, 2200.000, 1.000, 1.670, 0.000, 0.400, 2.500, 0.750, 5.500, 5.000, 2.000, 0.000, 0.000 point.2= 1.000, -1.140, 8.230, -9.400, 2200.000, 2.000, 1.670, 0.000, 0.400, 2.500, 0.750, 6.500, 5.000, 3.000, 0.000, 0.000 point.3= 2.000, -6.880, -22.540, 1.930, 1200.000, 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, -6.880, 22.540, 1.930, 1200.000, 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, -15.120, 0.000, -6.410, 1200.000, 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, 5.850, 0.000, -2.530, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_cg_height= 9.000 static_pitch= 0.000 [Views] eyepoint=9.00,0.000000,3.000000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -6.88, -22.55, 1.93, fx_navred light.1=3, -6.88, 22.55, 1.93, fx_navgre light.2=2, 5.85, 0.00,-2.54, fx_strobe light.3=1, -8.06, 0.00, -6.94, fx_beacon light.4=4, 9.61, 0.00, 1.39, fx_vclight [General] performance=Maximum Speed\n380 kts 700 km\/hr\n\nCruise Speed\n280 kts 515 km\/hr\n\nEngine\nDaimler Benz DB610 3000 bhp\n\nPropeller\nCounter rotating variable pitch\n\nMaximum Range\n1600 nm 1700 mi 2720 km\n\nService Ceiling\n40,000 ft\t 12190 m\n\nLength\n40 ft, 2 in 12.1 m\n\nWingspan\n42 ft, 1 in\t 12.8 m\n atc_type=EXPERIMENTAL atc_model=EXPL [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] Center1= 0.000, 0.000, 0.000, 180.000, 0.000 LeftMain= 0.000, 0.000, 0.000, 135.000, 0.000 RightMain= 0.000, 0.000, 0.000, 135.000, 0.000 External1= 0.000, 0.000, 0.000, 225.000, 0.000 External2= 0.000, 0.000, 0.000, 225.000, 0.000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 358.000 wing_span= 52.000 wing_root_chord= 6.917 wing_dihedral= 5.098 wing_incidence= 1.000 wing_twist= 0.000 oswald_efficiency_factor= 0.749 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 2.000 wing_pos_apex_vert= 0.000 htail_area= 34.000 htail_span= 10.500 htail_pos_lon= -17.667 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 15.000 vtail_span= 4.416 vtail_sweep= 0.000 vtail_pos_lon= -19.583 vtail_pos_vert= 3.250 elevator_area= 13.260 aileron_area= 18.900 rudder_area= 8.230 elevator_up_limit= 28.000 elevator_down_limit= 22.999 aileron_up_limit= 26.001 aileron_down_limit= 18.999 rudder_limit= 28.000 elevator_trim_limit= 19.996 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 [GeneralEngineData] engine_type= 0 Engine.0= 0.000, 0.000, 0.000 fuel_flow_scalar= 1.000 [Reference Speeds] flaps_up_stall_speed= 64.000 full_flaps_stall_speed= 51.200 cruise_speed= 400.000 [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 [direction_indicators] direction_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 [Flaps.0] type= 1 span-outboard= 0.125 extending-time= 5.000 system_type= 0 damaging-speed= 191.000 blowout-speed= 290.000 lift_scalar= 0.500 drag_scalar= 1.500 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 8.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 40.000, 0.000
