[fltsim.0] title=Su-43 Berkut sim=Su43 model=su43 panel= sound= texture= kb_checklists= kb_reference= ui_manufacturer=General Resource ui_type=Su-43 Berkut ui_variation=UPEO atc_id=N1200 editable=0 atc_heavy=0 atc_airline=S23 atc_flight_number= description=Sukhoi UPEO visual_damage=1 [General] editable=1 atc_type= performance= Category=airplane [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 [CameraDefinition.0] Title = "Engine" Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59} Description = Exaust view Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.5 ShowWeather = Yes InitialXyz = -1.0, 1.0, -20.0 InitialPbh = 0, 0, 10 XyzAdjust = TRUE Category=Aircraft ClipMode=Minimum [WEIGHT_AND_BALANCE] reference_datum_position=0.0,0.0,0.0 empty_weight_CG_position=0.0,0.0,0.0 max_number_of_stations=2 station_load.0=200.0,4.1,0.0,0.0 station_load.1=000.0,0.0.0,0.0,0.0 empty_weight=8400.0 empty_weight_roll_MOI=13500.0 empty_weight_pitch_MOI=41000.0 empty_weight_yaw_MOI=77000.0 empty_weight_coupled_MOI=0.0 max_gross_weight= 16587.000 [fuel] //----------Fwd/Aft--L-R----Vert--Capacity-Unusable--- LeftMain=0.000000,-6.000000,0.000000,500.000000,0.000000 RightMain=0.000000,6.000000,0.000000,500.000000,0.000000 Center1=0.000000,0.000000,0.000000,450.000000,0.000000 fuel_type=2.0 number_of_tank_selectors=1 electric_pump=0 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.9 aileron_effectiveness = 1.5 rudder_effectiveness = 1.0 pitch_stability = 1.9 roll_stability = 1.9 yaw_stability = 2.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [airplane_geometry] wing_area=206.0 wing_span=50.6 wing_root_chord=11.11 wing_dihedral=0 wing_incidence=-0.2 wing_twist=0.0 oswald_efficiency_factor=0.8 wing_winglets_flag=0 wing_sweep=-24.0 wing_pos_apex_lon=-6.56 wing_pos_apex_vert=1.83 htail_area=55.33 htail_span=12.46 htail_pos_lon=-26.24 htail_pos_vert=1.83 htail_incidence=1.0 htail_sweep=45.0 vtail_area=22.6 vtail_span=4.92 vtail_sweep=34.0 vtail_pos_lon=-25.3 vtail_pos_vert=1.00 elevator_area=55.84 aileron_area=23.84 rudder_area=18.0 elevator_up_limit=25.0 elevator_down_limit=25.0 aileron_up_limit=25.0 aileron_down_limit=25.0 rudder_limit=36.0 elevator_trim_limit=21.5 spoiler_limit=45.0 spoilerons_available=0 aileron_to_spoileron_gain=0.0 min_ailerons_for_spoilerons=0.0 min_flaps_for_spoilerons=0.0 auto_spoiler_available=0 spoiler_extension_time=3.500000 positive_g_limit_flaps_up=10.886752 positive_g_limit_flaps_down=10.433761 negative_g_limit_flaps_up=-10.240385 negative_g_limit_flaps_down=-10.666667 [pitot_static] vertical_speed_time_constant = 100 pitot_heat=1.000000 [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 // Gear 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0=1.0, 16.14 , 0.0, -6.61, 1900.0, 0.0, 0.5, 80.0, 0.8, 2.5, 1.5, 2.0, 3.0, 0.0, 0.0, 0.0 // Nose Gear point.1=1.0, -9.97, -5.74, -6.3, 2000.0, 1.0, 0.5, 0.0, 0.7, 2.0, 0.7, 4.0, 4.0, 2.0, 0.0, 0.0 // Left Mains point.2=1.0, -9.97, 5.74, -6.3, 2000.0, 2.0, 0.5, 0.0, 0.7, 2.0, 0.7, 4.0, 4.0, 3.0, 0.0, 0.0 // Right mains // Scrapes 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.3=2.0, -7.28, 16.47, -1.25, 1250.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0 // Wingtip Left point.4=2.0, -7.28, -16.47, -1.25, 1250.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0 // Wingtip Right point.5=2.0, -12.4, 0.00, -1.20, 1250.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0 // Exhaust Nozzle point.6=2.0, 5.61, 0.00, -1.2, 1250.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 // Nose point.7=2.0, -0.00, 0.00, 0.00, 1250.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0 0.0 // static_pitch=0.0 static_cg_height=5.8 gear_system_type=0 [Flaps.0] type=1 span-outboard=0.55 extending-time=3.0 system_type=1 flaps-position.0 = 0.0,0.0 flaps-position.1 = 10.0,0.0 flaps-position.2 = 20.0,0.0 flaps-position.3 = 35.0,0.0 flaps-position.4 = 50.0,0.0 damaging-speed=290 blowout-speed=300 lift_scalar=1.1 drag_scalar=1.4 pitch_scalar=1.0 system_type=1 [GeneralEngineData] engine_type = 1 Engine.0 = -19.9, 2.47, 1.11 Engine.1 = -19.9, -2.47, 1.11 fuel_flow_scalar=1.4 min_throttle_limit=0.000000 [TurbineEngineData] fuel_flow_gain = 0.003 inlet_area = 2.3 rated_N2_rpm = 29920 static_thrust = 7000 afterburner_available = 1 reverser_available = 0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [Reference Speeds] flaps_up_stall_speed=80.00 full_flaps_stall_speed=50.00 cruise_speed=550.0 max_indicated_speed=1000.000000 max_mach=2.000000 [keyboard_response] elevator=100.0,250.0 aileron=100.0,250.0 rudder=100.0,250.0 [Views] eyepoint = -1.00, 0.00, 0.00 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //The switch code, longitudinal, lateral, and vertical position (in feet), and the name of effect file light.0=4, 0.0, 0.00, 0.0, fx_vclight light.1=3, 1.7, 24.77, 1.8, fx_navgre light.2=3, 1.7, -24.77, 1.8, fx_navred light.3=1, 1.7, -24.77, 1.8, fx_strobe light.4=1, 1.7, 24.77, 1.8, fx_strobe light.5=1, 5.47, 0.00, 3.70, fx_strobeh light.6=1, 5.47, 0.00, 3.70, fx_beacon light.7=3, -29.0, -8.58, 10.66, fx_navwhi light.8=3, -29.0, 8.58, 10.66, fx_beacon light.9=2, -0.62, -5.25, 1.31, fx_wing_vapor_long light.10=2, -0.62, 5.25, 1.31, fx_wing_vapor_long light.11=2, -3.37, -15.25, 1.31, fx_wing_vapor light.12=2, -3.37, 15.25, 1.31, fx_wing_vapor light.13=2, -0.5, -25.9, 1.77, fx_vortices light.14=2, -0.5, 25.9, 1.77, fx_vortices light.15=2, -29.0, -8.58, 10.66, fx_vortices light.16=2, -29.0, 8.58, 10.66, fx_vortices [SMOKESYSTEM] smoke.0= -25.9, 2.47, 1.11, fx_electrosphere_burner smoke.1= -25.9, -2.47, 1.11, fx_electrosphere_burner smoke.2= -24.9, -2.47, 1.11, fx_flame2 smoke.3= -24.9, 2.47, 1.11, fx_flame2 [exits] number_of_exits = 1 exit_rate.0 = 0.5 [autopilot] autopilot_available= 1 use_no_default_pitch= 1 use_no_default_bank=1 flight_director_available= 1 default_vertical_speed= 3000.0 autothrottle_available = 1 autothrottle_arming_required = 0 autothrottle_takeoff_ga = 1 autothrottle_max_rpm= 150 pitch_takeoff_ga = 8; default_pitch_mode=0 default_bank_mode=0 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 [direction_indicators] direction_indicator.0 = 3,0 [electrical] ;BusType, MaxAmpLoad, MinVoltage ;BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) max_battery_voltage=24.0 min_battery_voltage=24.0 max_generator_alternator_amps=400.0 generator_alternator_voltage=28.0 flap_motor = 0, 5 , 17.0 gear_motor = 0, 5 , 17.0 autopilot = 0, 5 , 17.0 avionics_bus = 0, 10, 17.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 2 , 17.0 additional_system = 0, 20, 17.0 marker_beacon = 1, 2 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 17.0 starter1 = 0, 20, 17.0 light_nav = 0, 5 , 17.0 light_beacon = 0, 5 , 17.0 light_landing = 0, 5 , 17.0 light_taxi = 0, 5 , 17.0 light_strobe = 0, 5 , 17.0 light_panel = 0, 5 , 17.0 [brakes] toe_brakes_scale=5.2 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 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=0 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=0