[fltsim.0] title=Ta-183 Huckebein sim=ta183 model= panel= sound= texture= KB_checklists=CheckList_Ta 183 visual_damage=1 description=In 1944 Kurt Tank proposed the Ta 183 (to replace the Flitzer) for a contender for the German Air Ministry's emergency fighter specification, which called for a fighter, powered by the HeS 011A turbojet be able to operate with the Me 262, but using less premium resources to make. The Ta 183 was accepted in February 1945, an order for a prototype was given at the beginning of March 1945. The Ta 183 V1 was to use the Junkers Jumo 004 turbojet, as the He S 011 was still not ready for use. The first flight was scheduled for May\/ June 1945. On the 8\/4\/1945 Allies captured Focke-Wulf's design department, none the less work on the prototype did go on, but the Ta 183 V1 was never finished by the war's end. When the war did end, Soviets took the aircraft and scientists back to the USSR, and the aircraft eventually became the Mig-15. ui_manufacturer=Focke-Wulf ui_type=Ta-183 ui_variation=Default atc_heavy=0 atc_id=183 atc_airline=AIR FORCE atc_flight_number= [WEIGHT_AND_BALANCE] empty_weight= 7384.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= -0.065, 0.000, 0.000 max_number_of_stations=50 station_load.0= 200.000, 3.000, 0.000, 3.000 ;Moments of Inertia empty_weight_pitch_MOI= 6995.000 empty_weight_roll_MOI= 6256.000 empty_weight_yaw_MOI= 11624.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 9895.500 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=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 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 [jet_engine] thrust_scalar=1.000 [exits] number_of_exits=1 exit_rate.0=0.4 ;Percent per second [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=160.0 ; ;TESTING FOR ELECTRICAL STUFF ;setting=BusType, MaxAmpLoad, MinVoltage ;where BusTypes: 0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 0.0 gear_motor=0, 5 , 0.0 autopilot=0, 5 , 0.0 avionics_bus=0, 10, 0.0 avionics=1, 5 , 0.0 pitot_heat=0, 2 , 0.0 additional_system=0, 20, 0.0 marker_beacon=1, 2 , 0.0 gear_warning=0, 2 , 0.0 fuel_pump=0, 5 , 0.0 starter1=0, 20, 0.0 light_nav=0, 5 , 0.0 light_beacon=0, 5 , 0.0 light_landing=0, 5 , 0.0 light_taxi=0, 5 , 0.0 light_strobe=0, 5 , 0.0 light_panel=0, 5 , 0.0 [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, 6.700, 0.000, -7.300, 2200.00, 0.000, 1.000, 12.000, 0.290, 2.500, 0.950, 5.000, 5.000, 0.000, 0.000, 0.000 point.1= 1.000, -2.110, -3.000, -6.700, 2200.00, 1.000, 1.300, 0.000, 0.450, 2.500, 0.750, 5.000, 5.000, 2.000, 0.000, 0.000 point.2= 1.000, -2.110, 3.000, -6.700, 2200.00, 2.000, 1.300, 0.000, 0.450, 2.500, 0.750, 5.000, 5.000, 3.000, 0.000, 0.000 point.3= 2.000, -7.560, -16.300, -3.070, 1574.80, 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, -7.560, 16.300, -0.730, 1574.80, 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, -9.830, 0.000, -1.230, 1574.80, 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, 1.580, 0.000, -2.650, 1574.80, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 1.300 static_cg_height= 6.100 [Views] eyepoint= 2.3, 0.0, 2.6 [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 [General] performance=Weight: 6584 lbs\nPower: 2865 lbs thrust\n7.5g Corner speed: 242 mph\nMax speed @ SL: 530 mph\nMax speed: 597 mph @ 20000 ft\nClimb rate: 4100 ft\/min @ 333 mph\nFlight Model By: David Adams\n4\/15\/03 04:31 PM\nFlight Model Workbook V2.80.55 atc_type=FOKKER atc_model=183 [fuel] LeftMain= 0.200, -3.000, 0.000, 172.500, 0.000 RightMain= 0.200, 3.000, 0.000, 172.500, 0.000 fuel_type=2.000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 260.000 wing_span= 38.750 wing_root_chord= 6.750 wing_dihedral= 2.499 wing_incidence= 1.000 wing_twist= 0.000 oswald_efficiency_factor= 0.891 wing_winglets_flag= 1 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 39.000 htail_span= 15.500 htail_pos_lon= -17.333 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 44.000 vtail_span= 7.563 vtail_sweep= 0.000 vtail_pos_lon= -17.333 vtail_pos_vert= 6.667 elevator_area= 19.300 aileron_area= 23.400 rudder_area= 10.500 elevator_up_limit= 35.000 elevator_down_limit= 35.000 aileron_up_limit= 20.000 aileron_down_limit= 20.000 rudder_limit= 22.000 elevator_trim_limit= 35.000 spoiler_limit= 0.000 spoilerons_available= 1 aileron_to_spoileron_gain= 4.600 min_ailerons_for_spoilerons= 4.985 min_flaps_for_spoilerons= 0.000 [GeneralEngineData] engine_type= 1 Engine.0= -2.750, 0.000, 0.000 fuel_flow_scalar= 1.000 [TurbineEngineData] fuel_flow_gain= 0.002 inlet_area= 0.847 rated_N2_rpm= 9000.000 static_thrust= 2865.000 afterburner_available= 0 reverser_available= 1 [Reference Speeds] flaps_up_stall_speed= 105.000 full_flaps_stall_speed= 84.000 cruise_speed= 239.392 [keyboard_response] elevator=150.000, 250.000 aileron=150.000, 250.000 rudder=150.000, 250.000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=800.000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000 pitch_takeoff_ga=8.000 [direction_indicators] direction_indicator.0=3,0 [Flaps.0] type= 1 span-outboard= 0.120 extending-time= 5.000 system_type= 0 damaging-speed= 340.000 blowout-speed= 380.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 14.000, 0.000 flaps-position.2= 28.000, 0.000 flaps-position.3= 42.000, 0.000 flaps-position.4= 55.000, 0.000
