[fltsim.0]
title=ALPHA Swift FR5
sim=alpha_fr5
model=
panel=
sound=
texture=
KB_checklists=fr5_check
kb_reference=
ui_manufacturer=ALPHA
ui_type=Supermarine Swift FR.5
ui_variation=FR.5
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_id=
atc_airline=
atc_flight_number=
atc_parking_types=MIL_COMBAT
description=© AlphaSim 2006\n\nThe Supermarine Swift was the first British production aircraft to have swept wings and tailplanes.  Essentially a revision of the Supermarine Attacker, the type evolved through several marques, eventually arriving at the FR.5, which was the most numerous.  Incorporating tricycle gear and an afterburning engine, this aircraft held the world speed record for a scant 24 hours, when it was again broken by the Douglas F4D Skyray.  The FR.5 utilised a "sawtooth" leading edge on the main wing (adding stability at high angles of attack) and remained operational until the summer of 1961.  A later development, the FR.7, was adapted to the reconnaissance role, with a dozen of these being produced.

[fltsim.1]
title=ALPHA Swift FR5 longrange
sim=alpha_fr5
model=1
panel=
sound=
texture=
KB_checklists=fr5_check
kb_reference=
ui_manufacturer=ALPHA
ui_type=Supermarine Swift FR.5
ui_variation=FR.5, long range
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
atc_id=
atc_airline=
atc_flight_number=
atc_parking_types=MIL_COMBAT
description=© AlphaSim 2006\n\nThe Supermarine Swift was the first British production aircraft to have swept wings and tailplanes.  Essentially a revision of the Supermarine Attacker, the type evolved through several marques, eventually arriving at the FR.5, which was the most numerous.  Incorporating tricycle gear and an afterburning engine, this aircraft held the world speed record for a scant 24 hours, when it was again broken by the Douglas F4D Skyray.  The FR.5 utilised a "sawtooth" leading edge on the main wing (adding stability at high angles of attack) and remained operational until the summer of 1961.  A later development, the FR.7, was adapted to the reconnaissance role, with a dozen of these being produced.

[General]
performance=Model: AlphaSim\nPanel: P Perrott\nGauges: H Pralle\nTextures: G Flores\nFlight Model: J. McDaniel\n\nFirst flight: 25 August 1952 \nWingspan: 32 feet 4 inches  \nLength: 42 feet 3 inches  \nHeight: 13 feet 6 inches\nEmpty weight: 13,435 pounds \nMaximum weight: 21,400 pounds  \nMax speed: 717 mph  \nCeiling: 45,800 feet  \nPower plant: Rolls-Royce Avon 114, 9450-lbf\nRange: 630 miles\nAccommodation: One pilot\nArmament: Two 30 mm cannon 
editable=1 
atc_type= 
atc_model= 

[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3,  -5.61, -15.65, -0.96, fx_navred
light.1 = 3,  -5.61,  15.65, -0.96, fx_navgre
light.2 = 3,  -19.72, 0.0, 1.51, fx_navwhi
light.3 = 4,  10.77,  0.0, 2.36, fx_vclight

//afterburner
light.17=9, -19.00, 0.00, 0.00, fx_Bob_both_smaller_blue
light.18=9, -21.50, 0.00, -0.50, fx_Bshort_Burnerflame

[smokesystem]
smoke.0 = 0.0, -30.00, 0.00, fx_smoke_f6

[weight_and_balance]
max_gross_weight = 21400
empty_weight = 13435
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 28494
empty_weight_roll_MOI = 11585
empty_weight_yaw_MOI = 23848
empty_weight_coupled_MOI = 0
CG_forward_limit = 0.00
CG_aft_limit = 1.00
max_number_of_stations = 0


[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.0
min_throttle_limit = 0.00
engine.0 = -20.00, 0.00, 0.00

[TurbineEngineData]
fuel_flow_gain=0.90 
inlet_area=5.80 
rated_N2_rpm=12000.00 
static_thrust=9450.00 
afterburner_available=1 
reverser_available=0.00 

[Reference Speeds]
flaps_up_stall_speed=114.00 
full_flaps_stall_speed=96.00 
cruise_speed=450.00			//knots over the ground at 36,000 ft. (264 indicated)
max_indicated_speed=820
max_mach=1.20
max_level_speed=737 mph (649 knots)	//indicated at 5,000 feet.

[effects]
windshield_rain_effect_available = 1

[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 1
electric_pump = 1
Center1 = 2, 0, 0, 300, 3
Center2 = -2, 0, 0, 250, 3


[contact_points]
static_pitch = -1.59
static_cg_height = 5.29
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 7

point.0 =1, 13.10, 0.00, -5.15, 3000.00, 0.00, 0.80, 25.00, 0.13, 3.50, 0.85, 5.00, 5.00, 0.00, 250.00, 230.00
point.1 =1, -1.00, -7.60, -5.80, 3000.00, 1.00, 1.15, 0.00, 0.45, 2.50, 0.80, 5.00, 5.00, 2.00, 250.00, 230.00
point.2 =1, -1.00, 7.60, -5.80, 3000.00, 2.00, 1.15, 0.00, 0.45, 2.50, 0.80, 5.00, 5.00, 3.00, 250.00, 230.00

point.3 =2, -10.00, -16.03, -1.06, 1500.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00
point.4 =2, -10.00, 16.03, -1.06, 1500.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00
point.5 =2, -20.00, 0.00, -1.10, 1500.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 5.00, 9.00, 0.00, 0.00
point.6 =2, 20.60, 0.00, 0.60, 1500.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00


[keyboard_response]
elevator = 150.00, 250.00
aileron = 150.00, 150.00
rudder = 150.00, 250.00


[forcefeedback]
gear_bump_nose_magnitude = 1000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 450
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 2000
crash_direction1 = 1000
crash_magnitude2 = 2000
crash_direction2 = 9000
crash_period2 = 7500
crash_duration2 = 2500000
stick_shaker_magnitude = 2000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
wing_area = 327.70
wing_span = 32.33
wing_root_chord = 13.50
wing_dihedral = 1.00
wing_incidence = 0.00
wing_twist = 0.00
oswald_efficiency_factor = 0.85
wing_winglets_flag = 0
wing_sweep = 50.00
wing_pos_apex_lon = 8.00
wing_pos_apex_vert = -0.80
htail_area = 40.00
htail_span = 13.00
htail_pos_lon = -13.30
htail_pos_vert = 1.50
htail_incidence = -1.00
htail_sweep = 50.00
vtail_area = 19.14
vtail_span = 5.46
vtail_sweep = 45.00
vtail_pos_lon = -11.00
vtail_pos_vert = 2.50
elevator_area = 12.00
aileron_area = 33.00
rudder_area = 9.50
elevator_up_limit = 14.00
elevator_down_limit = 11.00
aileron_up_limit = 20.00
aileron_down_limit = 15.00
rudder_limit = 30.00
elevator_trim_limit = 18.00
spoiler_limit = 0.00
aileron_to_spoileron_gain = 0.00
spoiler_handle_available = 0
min_ailerons_for_spoilerons = 0.00
min_flaps_for_spoilerons = 0.00
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 400
engine_generator_map = 1
electric_always_available = 1

[exits]
number_of_exits=1
exit_rate.0=0.5

[TailHook]
tailhook_length = 3
tailhook_position = -15, 0, -2.00
cable_force_adjust = 1

[Views]
eyepoint=9.5, 0.00, 2.80

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800.0 
autothrottle_available=1 
autothrottle_arming_required= 0
autothrottle_max_rpm = 100
autothrottle_takeoff_ga= 0
pitch_takeoff_ga=8 ;
max_pitch=10.0
max_pitch_acceleration=0.8
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.2
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.5
max_bank_velocity=2.00
max_throttle_rate=0.10
nav_proportional_control=11.00
nav_integrator_control=0.20
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 0.0

[direction_indicators]
direction_indicator.0=3,0 

[brakes]
toe_brakes_scale=1.09
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=1
flap_limit_power=25
flap_limit_idle=5

[hydraulic_system]
electric_pumps=1
engine_map=1
normal_pressure=3000.00

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[folding_wings]
wing_fold_system_type = 4			;0=None
fold_rates = 0.12,0.11				;Percent per second
[jet_engine]
thrust_scalar=1.000 

[flight_tuning]
cruise_lift_scalar=1.00 
pitch_stability=1.00 
roll_stability=1.00 
yaw_stability=1.00 
parasite_drag_scalar=1.00 
induced_drag_scalar=1.00 
elevator_effectiveness=1.00 
aileron_effectiveness=1.00 
rudder_effectiveness=1.00 
elevator_trim_effectiveness=1.00 
aileron_trim_effectiveness=1.00 
rudder_trim_effectiveness=1.00 

[Radios]
Audio.1=1 
Com.1=1,0 
Com.2=0,0 
Nav.1=1,0,1 
Nav.2=0,0,0 
Adf.1=1,0 
Transponder.1=1 
Marker.1=1 

[Flaps.0]
type= 1
span-outboard= 0.50
extending-time= 5.00
system_type= 1
damaging-speed= 255.00
blowout-speed= 300.00

flaps-position.0= 0.00, 0.00
flaps-position.1= 15.00, 0.00
flaps-position.2= 30.00, 0.00
flaps-position.3= 45.00, 0.00
flaps-position.4= 100.00, 0.00