[fltsim.0]
title=Supermarine Attacker
sim=Attacker
model=
panel=
sound=
texture=
kb_checklists=Attacker_check
kb_reference=
atc_id=WK327
ui_manufacturer=Supermarine
ui_type=Attacker FB.2
ui_variation=800 Squadron, Fleet Air Arm, HMS Eagle 1954
description=British Naval Jet Fighter\n\nFirst flew July 1946\nEntered service August 1951\nType 398 used basic wing structure, armament and undercarriage parts from the Spiteful\/Seafang\n
atc_heavy=0
atc_airline=NAVY
atc_flight_number=WK327

[General]
editable=1
atc_type=NAVY
atc_model=GC1
performance=Maximum Speed    \t 590 mph @ sea level\n\t\t 538 mph @ 30,000ft\nClimb                       \t 6,350 ft\/min @ sea level\n\t\t 6.6 mins to 30,000ft\nService Ceiling        \t45,000 ft\nRange                     \t 590 miles\n\nCopyright Ralph Pegram 2002\nrwp.forward@talk21.com\n\n\n

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000

max_gross_weight= 12211.000
empty_weight= 8426.000

max_number_of_stations=50
station_load.0= 170.000, 7.000, 0.000, 0.000

;Moments of Inertia
empty_weight_pitch_MOI= 19500.000
empty_weight_roll_MOI= 5000.000
empty_weight_yaw_MOI= 11000.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.1= 1.000, 12.000, 0.000, 0.000

[pitot_static]
vertical_speed_time_constant=1.5              //Increasing this value will cause a more instantaneous reaction in the VSI


[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

[GeneralEngineData]
engine_type= 1
Engine.0= -22.000, 0.000, 0.000
fuel_flow_scalar= 1.100

[TurbineEngineData]
fuel_flow_gain= 0.003
inlet_area= 8.000
rated_N2_rpm= 12500.000
static_thrust= 5100.000
afterburner_available= 0
reverser_available= 0

[jet_engine]
thrust_scalar=1.000

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)

max_battery_voltage=24.0
generator_alternator_voltage=28
max_generator_alternator_amps=40.0

autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
starter1=0, 20, 17.0


[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3,   1.25, -18.68,  0.35, fx_navredh ,
light.1=3,   1.25,  18.68,  0.35, fx_navgreh ,
light.3=3, -21.77,   0.00,  1.40, fx_navwhi ,
light.4=4,   9.26,   0.00,  2.00, fx_vclight ,


[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)

//         0     1        2       3       4          5     6        7      8      9     10    11      12    13 14  15
point.0= 1.000, -15.940, 0.000, -3.070, 3500.000, 0.000, 0.440, 90.000, 0.250, 0.700, 0.850, 3.000, 4.000, 0.000, 0.000, 0.000
point.1= 1.000, 2.360, -5.880, -5.700, 3500.000, 1.000, 1.000, 0.000, 0.540, 0.700, 0.850, 8.000, 6.000, 2.000, 250, 300
point.2= 1.000, 2.360, 5.880, -5.700, 3500.000, 2.000, 1.000, 0.000, 0.540, 0.700, 0.850, 9.000, 7.000, 3.000, 250, 300
point.3= 2.000, 0.000, -20.000, -1.250, 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, 0.000, 20.000, -1.250, 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, -20.250, 0.000, -1.660, 2400.000, 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, 5.410, 0.000, -3.500, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7= 2.000, 0.000, -5.430, -3.750, 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.8= 2.000, 0.000, 5.430, -3.750, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000

static_cg_height= 4.800
static_pitch= 7.500

max_number_of_points=21

[exits]
number_of_exits=1
exit_rate.0=0.4	 			;Percent per second

[Views]
eyepoint=8.26, 0.0, 2.8

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

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
elevator=100,  180
aileron=200, 1000
rudder=200, 1000

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type=4
direction_indicator.0=1,0

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

[fuel]
LeftMain= 0.000, -5.000, 0.000, 20.500, 0.000
RightMain= 0.000, 5.000, 0.000, 20.500, 0.000
fuel_type=2   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
                  
Center1= 0.000, 0.000, 2.000, 228.000, 2.000
Center2= -7.000, 0.000, 0.000, 24.000, 0.000

[airplane_geometry]
wing_area= 227.000
wing_span= 37.000
wing_root_chord= 8.500
wing_dihedral= 5.000
wing_incidence= 0.200
wing_twist= 0.000
oswald_efficiency_factor= 0.900
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 50.000
htail_span= 11.800
htail_pos_lon= -18.000
htail_pos_vert= 1.200
htail_incidence= 0.500
htail_sweep= 0.000
vtail_area= 30.000
vtail_span= 4.500
vtail_sweep= 0.000
vtail_pos_lon= -18.000
vtail_pos_vert= 4.300
elevator_area= 24.000
aileron_area= 22.000
rudder_area= 8.000
elevator_up_limit= 28.000
elevator_down_limit= 21.000
aileron_up_limit= 20.000
aileron_down_limit= 15.000
rudder_limit= 24.000
elevator_trim_limit= 19.500
spoiler_limit= 90.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[Reference Speeds]
flaps_up_stall_speed= 96.000
full_flaps_stall_speed= 88.000
cruise_speed= 380.000

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.0
autothrottle_available=1
pitch_takeoff_ga=8.000000
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
use_no_default_bank=1
use_no_default_pitch=1

[forcefeedback]
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
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

[SMOKESYSTEM]
smoke.0=0.00, -20.00, 0.00, fx_exhaust_g

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 280.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 40.000, 0.000
flaps-position.2= 80.000, 0.000