[fltsim.0] title=MiG-3 A sim=MiG-3 model= panel= sound= texture= KB_checklists=MiG-3_check atc_id_enable=1 atc_id=NXMG3A ui_manufacturer=Mikoyan-Gurevich ui_type=MiG-3 ui_variation=A description=The Mikoyan-Gurevich MiG-3 was designed as an excellent high altitude fighter. Unfortunately, most of the combat took place at lower altitudes where the Mig-3 did not perform well. It was a very hard handling plane but because of the large numbers made served well.\n\nDimensions: \nWing span: 33 ft 5.5 in (10.2 m) \nLength: 27 ft 0.8 in (8.25 m) \nHeight: 8 ft 8.33 in (2.65 m) \nWeights: \nEmpty: 5,952 lb (2700 kg) \nFull: 7,385 lb (3350 kg)\n [fltsim.1] title=MiG-3 B sim=MiG-3 model=B panel= sound= texture=B KB_checklists=MiG-3_check atc_id_enable=1 atc_id=NXMG3B ui_manufacturer=Mikoyan-Gurevich ui_type=MiG-3 ui_variation=B description=The Mikoyan-Gurevich MiG-3 was designed as an excellent high altitude fighter. Unfortunately, most of the combat took place at lower altitudes where the Mig-3 did not perform well. It was a very hard handling plane but because of the large numbers made served well.\n\nDimensions: \nWing span: 33 ft 5.5 in (10.2 m) \nLength: 27 ft 0.8 in (8.25 m) \nHeight: 8 ft 8.33 in (2.65 m) \nWeights: \nEmpty: 5,952 lb (2700 kg) \nFull: 7,385 lb (3350 kg)\n [WEIGHT_AND_BALANCE] empty_weight = 5900 // (pounds) reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -0.1, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 1 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 = 5000.0 empty_weight_roll_MOI = 3000.0 empty_weight_yaw_MOI = 7500.0 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 = 1.1 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=1425.000000 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 propeller_type=0 propeller_diameter=12.00000 propeller_blades=3 propeller_moi=20.800000 beta_max=65.000000 beta_min=23.000000 min_gov_rpm=1800.000000 prop_tc=0.010000 gear_reduction_ratio=2.230000 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 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, -18.21, 0.00, -1.35, 3200, 0, 0.30, 0.0, 0.40, 2.5, 0.80, 7.5, 5.00, 0, 0, 165 point.1=1, 1.41, -5.76, -6.80, 2200, 1, 1.05, 0.0, 0.50, 2.5, 0.83, 2.5, 4.00, 2, 0, 165 point.2=1, 1.41, 5.76, -6.80, 2200, 2, 1.05, 0.0, 0.50, 2.5, 0.83, 2.5, 8.25, 3, 0, 165 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, 2200, 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, 2800, 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, 2200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4 static_cg_height = 5.60 //(feet) altitude of CG when at rest (altitude when loaded on ground) static_pitch = 13.50 //degrees (pitch when loaded on ground) //[TailHook] //tailhook_length=4 ;(feet) //tailhook_position = -17.5, 0.0, -0.5 ;(feet) longitudinal, lateral, vertical positions from datum //cable_force_adjust = 1.0 [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=14 // degrees, KIAS flaps-position.2=28 // degrees, KIAS flaps-position.3=42 // degrees, KIAS flaps-position.4=55 // degrees, KIAS damaging-speed=275 // KIAS blowout-speed=365 // KIAS [Views] eyepoint=-3.75,0.000000,1.65 [LIGHTS] panel=0.00, 0.30, -0.80, fx_vclight [General] performance=Max Gross: 7,385 lb (3350 kg) \nPerformance: \nMaximum Speed: 398 mph (641 km\/h) @ 25,590 ft (7800 m) \nService Ceiling: 39,370 ft (12000 m) \nRange: 742 miles (1194 km) \nPowerplant: \nMikulin AM-25A, 1,350 hp 12-cylinder Inline Vee, Liquid cooled. \nArmament: \nOne 20 mm cannon (on some models). Two .30 inch (7,62mm) ShKAS machine guns synchronized. \nBomb load 441 lb (200 kg). \n atc_type=EXPERIMENTAL atc_model=Mig-3 [fuel] LeftMain=-2.000000,-9.000000,-1.700000,60.000000,0.000000 RightMain=-2.000000,9.000000,-1.700000,60.000000,0.000000 External1=-0.500000,0.000000,-4.500000,75.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area=203.000000 wing_span=34.000000 wing_root_chord=6.083333 wing_dihedral=5.998535 wing_incidence=0.999756 wing_twist=0.000000 oswald_efficiency_factor=0.699497 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=24.000000 htail_span=11.000000 htail_pos_lon=-18.833333 htail_pos_vert=0.000000 htail_incidence=-0.999756 htail_sweep=0.000000 vtail_area=15.000000 vtail_span=4.415880 vtail_sweep=0.000000 vtail_pos_lon=-18.833333 vtail_pos_vert=0.583333 elevator_area=13.000000 aileron_area=20.400000 rudder_area=13.060000 elevator_up_limit=26.000825 elevator_down_limit=26.000825 aileron_up_limit=21.497376 aileron_down_limit=20.345731 rudder_limit=28.997394 elevator_trim_limit=19.996227 spoiler_limit=0.572958 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=-0.333333,0.000000,0.000000 fuel_flow_scalar=1.000000 [Reference Speeds] flaps_up_stall_speed=86.000000 full_flaps_stall_speed=68.800000 cruise_speed=279.543877 [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=1800.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 [direction_indicators] direction_indicator.0=1,0
