[fltsim.0]
title=Focke Wulf Ta283
sim=fw283
model=
panel=
sound=
texture=
kb_checklists=fw283_check
kb_reference=fw283_ref
atc_id=E400HE
atc_airline=
atc_flight_number=
ui_manufacturer=Focke Wulf
ui_type=Interceptor
ui_variation=Prototype
visual_damage=1
description=Modern version of the Focke Wulf Ta283 designed by German engineers at the end of the war. Originally powered by two ram-jets it achieved takeoff  through a rocket motor housed in the rear of the fuselage, once airborne the ram-jets would take over. The aircraft would probably have achieved speeds in excess of 700 mph!. This particular aircraft is a prototype recon aircraft. For more info please visit www.luft46.com, there are many other unusual aircrafts on this site besides this one.


[fltsim.1]
title=Focke Wulf Ta283 Paint1
sim=fw283
model=
panel=
sound=
texture=1
kb_checklists=fw283_check
kb_reference=fw283_ref
atc_id=E400HE
atc_airline=
atc_flight_number=
ui_manufacturer=Focke Wulf
ui_type=Interceptor
ui_variation=Luft46 Combat
visual_damage=1
description=Modern version of the Focke Wulf Ta283 designed by German engineers at the end of the war. Originally powered by two ram-jets it achieved takeoff  through a rocket motor housed in the rear of the fuselage, once airborne the ram-jets would take over. The aircraft would probably have achieved speeds in excess of 700 mph!. This particular aircraft is a high speed interceptor. For more info please visit www.luft46.com, there are many other unusual aircrafts on this site besides this one.


[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=Span: 26ft\nLength: 38.6ft\nHeight: 9.6ft\nDry weight: 15000 lb\nFuel capacity: 2200 gal\nTakeoff weight: 29735 lb\nMax speed: 950 knots\nMax height: 52000 ft\nMax range: 3200 miles\nat 10000ft and 52% N1\nThrust 2 x 5000 lb\nChect notes for more info.


[WEIGHT_AND_BALANCE]
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=15000.000000
empty_weight_roll_MOI=135000.000000
empty_weight_pitch_MOI=262662.000000
empty_weight_yaw_MOI=373480.000000
empty_weight_coupled_MOI=1300.000000
max_gross_weight=46388.000

[fuel]
LeftMain=0.000, 0.000, 0.000, 700.000, 0.000
RightMain=0.000, 0.000, 0.000, 700.000, 0.000
Center1=0.000, 0.000, 0.000, 800.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=1


[airplane_geometry]
wing_area=400.000000
wing_span=40.666667
wing_root_chord=11.000000
wing_dihedral=-0.049438
wing_incidence=-0.494385
wing_twist=-0.999756
oswald_efficiency_factor=126.608319
wing_winglets_flag=0
wing_sweep=45.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=60.000000
htail_span=15.000000
htail_pos_lon=-14.166667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=45.000000
vtail_area=100.000000
vtail_span=11.490738
vtail_sweep=45.000000
vtail_pos_lon=-14.333333
vtail_pos_vert=5.833333
elevator_area=10.250000
aileron_area=3.920000
rudder_area=12.750000
elevator_up_limit=15.000000
elevator_down_limit=15.000000
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=30.000000
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000


[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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
point.0=1.000, 19.352, 0.000, -3.950, 1574.803, 0.000, 0.694, 30.000, 0.300, 2.500, 0.453, 5.000, 5.000, 0.000, 0.000, 0.000
point.1=1.000, -3.140, -2.720, -3.950, 1574.803, 1.000, 1.010, 0.000, 0.300, 2.500, 0.627, 5.000, 5.000, 2.000, 0.000, 0.000
point.2=1.000, -3.140, 2.720, -3.950, 1574.803, 2.000, 1.010, 0.000, 0.300, 2.500, 0.627, 5.000, 5.000, 3.000, 0.000, 0.000
point.3=2.000, -15.580, -23.060, -1.250, 1574.803, 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, -15.580, 23.060, -1.250, 1574.803, 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, -15.590, 0.000, -0.330, 1574.803, 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, 5.110, 0.000, -2.990, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=0.000
static_cg_height=3.65


// need this to enable wing folding
[folding_wings]
wing_fold_system_type=4
fold_rates=0.5,0.5                          ;Percent per second

// need this to enable tailhook
[TailHook]
tailhook_length=1                             ;(feet)
tailhook_position=0.0, 0.0, 0.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0


[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=10.000000,0.000000
flaps-position.2=25.000000,0.000000
flaps-position.3=50.000000,0.000000

[GeneralEngineData]
engine_type=1
Engine.0=-16.698000,-5.833000,1.205000
Engine.1=-16.698000,5.833000,1.205000
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_gain=0.002170
inlet_area=7.247200
rated_N2_rpm=29920.000000
static_thrust=8100.000000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=70.000000
full_flaps_stall_speed=56.000000
cruise_speed=1486.846856

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=0.505000,0.000000,2.674000

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
use_no_default_pitch=1		
use_no_default_bank=1

[direction_indicators]
direction_indicator.0=3,0

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit            
light.0=3,  -6.86, -13.17, -0.25, fx_navred
light.1=3,  -6.86,  13.17, -0.25, fx_navgre
light.2=2,  1.89,   0.00, -2.44, fx_strobe
light.3=1,  -14.27,   0.00, 5.79, fx_beacon
light.4=4,  1.80,   0.00, 1.70, fx_vcta283


[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1

[jet_engine]
thrust_scalar=1.000

[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=0.300
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[SMOKESYSTEM]
smoke.0=1.20,-15.69,-5.83, fx_smoketa283
smoke.1=1.20,-15.69,5.83, fx_smoketa283
smoke.2=1.20,-14.69,5.83, fx_smoketa283
smoke.3=1.20,-14.69,5.83, fx_smoketa283