//5:53 PM 3/9/2005 Version 2.1 for FS9
[fltsim.0]
title=ALPHA RA-5C Vigilante
sim=RA-5C
model=
panel=
sound=
texture=
KB_checklists=vigilante_check
kb_reference=
ui_manufacturer=North American
ui_type=RA-5C Vigilante
ui_variation=USS Ranger
atc_id_color=0x00000000
visual_damage=1
atc_parking_types=MIL_COMBAT
description=© ALPHA Simulations 2005\n\nNorth American RA-5C Vigilante\n\nPlanned in late 1950's as a successor to the AJ-1 Savage, the Vigilante prototype first flew in 1958 and was decades ahead of its time, with many 'firsts' such as a digital computer, INS, slab tail and variable inlets and much more. Although conceived as a bomber, the USAF soon adopted the nuclear strike role which meant the A-5 was used solely for the recon role. The RA-5C was used in Vietnam (18 were lost) and continued in service until 1980.
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
atc_id_font=Verdana,-11,1,600,0

[General]
performance=Model: M Davies\nPanel: P Perrott\nTextures: M Davies\nFlight Model: J McDaniel\n\nLength: 76 ft 0 in\nSpan: 53 ft 0.4 in\nWing area: 754 sq ft\nWeight: Empty: 43,608 lbs\s loaded, 68,088 lbs.\nPower: (2) GE J79-GE-10 Turbojet, 17,860 lbs thrust with afterburners\nRange: 3,000 miles\nMax Speed: Mach 2.1 @ 36,000 ft\nService Ceiling: 48,400 ft.\nArmament: None 
editable=1 
atc_type= 
atc_model= 
Category=airplane

[weight_and_balance]
max_gross_weight = 68088.00
empty_weight = 43608.00
reference_datum_position = 0.00, 0.00, 0.00
empty_weight_CG_position = 0.00, 0.00, 0.00
empty_weight_pitch_MOI = 172817.00
empty_weight_roll_MOI = 77250.00
empty_weight_yaw_MOI = 145928.00
empty_weight_coupled_MOI = 0.00
CG_forward_limit = 0.00
CG_aft_limit = 1.00
max_number_of_stations = 2

station_load.0 =200.00, 28.70, 0.00, 0.81, Station 1
station_load.1 =200.00, 22.08, 0.00, 1.52, Station 2

[smokesystem]
smoke.0 = -30.00,-3.00, -0.70, fx_smoke_f6
smoke.1 = -30.00, 3.00, -0.70, fx_smoke_f6

[lights]

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

light.0 = 4, 29.60, 0, 1.28, fx_vclight
light.1= 4, 23.42, 0, 2.09, fx_vclight
light.2= 1, -9.5, 0, 2.20, fx_beacon
light.3= 1, -7.70, 0, -3.80, fx_beacon


//afterburner effects
light.13= 6, -24.7, -3.1, -0.90, fx_Bob_Burn_blue ,    // Eng1 Afterburner
light.14= 6, -28.3, -3.0, -1.30, fx_F14_Burnerflame ,    // Eng1 Afterburner Flame
light.15= 6, -24.7,  3.1, -0.90, fx_Bob_Burn_blue ,      // Eng2 Afterburner
light.16= 6, -28.3,  3.0, -1.30, fx_F14_Burnerflame ,    // Eng2 Afterburner Flame
light.17= 6, -26.0, -3.1, -0.70, fx_Bob_small_Blueflame ,      // Eng1 Blueflame,
light.18= 6, -26.0,  3.0, -0.70, fx_Bob_small_Blueflame ,      // Eng2 Blueflame,


[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 0.60
min_throttle_limit = 0.00
engine.0 = -24.70, -3.10, -0.70
engine.1 = -24.70, 3.10, -0.70

[TurbineEngineData]
fuel_flow_gain= 0.002 
inlet_area= 13.40 
rated_N2_rpm= 29920.00 
static_thrust= 17860.00 
afterburner_available= 1 
reverser_available= 0.00 

[Reference Speeds]
flaps_up_stall_speed= 123.00 
full_flaps_stall_speed= 93.00 
cruise_speed= mach 0.94		//320 indicated at 37,000 
max_indicated_speed=1600.00
max_mach=2.50
max_level_speed=1205		//Knots over the ground at 36,000 ft.

[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 = 0
//Simple flight model
Center1 =   0.00, 0.00, 0.00, 460.00, 0.00
Center2 =   0.00, 0.00, 0.00, 500.00, 0.00
Center3 =   0.00, 0.00, 0.00, 130.00, 0.00
LeftMain =  0.00,-9.00, 0.00, 830.00, 0.00
RightMain = 0.00, 9.00, 0.00, 830.00, 0.00
External1 = 0.00,-9.00,-3.00, 295.00, 0.00
External2 = 0.00, 9.00,-3.00, 295.00, 0.00


[contact_points]
static_pitch = 1.220
static_cg_height = 7.620
tailwheel_lock = 0
gear_system_type = 1

point.0 = 1, 17.20, 0.00, -8.20, 2000.00, 0.00, 1.10, 25.00, 0.20, 2.00, 0.80, 5.00, 5.00, 0.00, 300.00, 325.00
point.1 = 1, -5.00, -5.70, -7.80, 3000.00, 1.00, 1.50, 0.00, 0.40, 2.50, 0.80, 5.00, 5.00, 2.00, 300.00, 325.00
point.2 = 1, -5.00, 5.70, -7.80, 3000.00, 2.00, 1.50, 0.00, 0.40, 2.50, 0.80, 5.00, 5.00, 3.00, 300.00, 325.00
//scrape
point.3 = 2, -12.30, -27.00, 1.20, 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, -12.30, 27.00, 1.20, 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, -27.20, 0.00, -2.50, 1500.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00
point.6 = 2, 42.40, 0.00, -1.80, 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, 250.00
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 = 754.00
wing_span = 54.210
wing_root_chord = 22.40
wing_dihedral = 2.00
wing_incidence = 0.00
wing_twist = 0.00
oswald_efficiency_factor = 0.880
wing_winglets_flag = 0
wing_sweep = 43.00
wing_pos_apex_lon = 9.50
wing_pos_apex_vert = 1.50
htail_area = 116.00
htail_span = 32.20
htail_pos_lon = -12.70
htail_pos_vert = -0.30
htail_incidence = -0.50
htail_sweep = 50.00
vtail_area = 50.00
vtail_span = 13.20
vtail_sweep = 50.00
vtail_pos_lon = -13.40
vtail_pos_vert = 1.50
elevator_area = 77.00
aileron_area = 25.00
rudder_area = 40.00
elevator_up_limit = 21.00
elevator_down_limit = 13.00
aileron_up_limit = 15.00
aileron_down_limit = 15.00
rudder_limit = 8.00
elevator_trim_limit = 18.00
spoiler_limit = 70.00
aileron_to_spoileron_gain = 0.00
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.00
min_flaps_for_spoilerons = 0.00
spoilerons_available = 0
auto_spoiler_available=0
spoiler_extension_time=1.000000
positive_g_limit_flaps_up=9.017094
positive_g_limit_flaps_down=6.205128
negative_g_limit_flaps_up=-6.205128
negative_g_limit_flaps_down=-4.136752

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 300
engine_generator_map = 1,1
electric_always_available = 1

[TailHook]
tailhook_length=6.5
tailhook_position=-18.35, 0.0, -1.0		
cable_force_adjust=1.0

[folding_wings]
wing_fold_system_type=4
fold_rates=0.12,0.11

[exits]
number_of_exits=1
exit_rate.0=0.7

[Views]
eyepoint=29.5,0.0,2.2 

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1800.00 
autothrottle_available=1 
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=125.00
pitch_takeoff_ga=8.00 
max_pitch=10.00
max_pitch_acceleration=2.00
max_pitch_velocity_lo_alt=1.00
max_pitch_velocity_hi_alt=1.50
max_pitch_velocity_lo_alt_breakpoint=20000.00
max_pitch_velocity_hi_alt_breakpoint=28000.00
max_bank=25.00
max_bank_acceleration=1.80
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.250
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.520
gs_integrator_control=0.260
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.00

[direction_indicators]
direction_indicator.0=3,0 

[brakes]
toe_brakes_scale=1.0031
parking_brake=1

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

[hydraulic_system]
electric_pumps=1
engine_map=1,1,0,0
normal_pressure=3000.00

[stall_warning]
type=1
stick_shaker=0

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[General]
atc_type= 
atc_model= 
performance= 
editable=1 

[jet_engine]
thrust_scalar=1.00 

[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 


[Flaps.0]
type= 1
span-outboard= 0.65
extending-time= 5.00
system_type= 1
damaging-speed= 230.00
blowout-speed= 250.00
lift_scalar= 1.00
drag_scalar= 0.00
pitch_scalar= 1.00
flaps-position.0= 0.00, 0.00
flaps-position.1= 20.00, 0.00
flaps-position.2= 40.00, 0.00
flaps-position.3= 60.00, 0.00
flaps-position.4= 70.00, 0.00
flaps-position.5= 80.00, 0.00

[Flaps.1]
type= 2
span-outboard= 0.65
extending-time= 5.00
system_type= 1
damaging-speed= 230.00
blowout-speed= 250.00
lift_scalar= 0.00
drag_scalar= 1.00
pitch_scalar= 0.00
flaps-position.0= 0.00, 0.00
flaps-position.1= 1.00, 0.00
flaps-position.2= 15.00, 0.00
flaps-position.3= 30.00, 0.00
flaps-position.4= 50.00, 0.00
flaps-position.5= 80.00, 0.00

[pitot_static]
pitot_heat=1.00

[vacuum_system]
max_pressure=5.15
vacuum_type=2
electric_backup_pressure=0.00
engine_map=0,0,0,0

[pneumatic_system]
max_pressure=18.00
bleed_air_scalar=1.00

[deice_system]
structural_deice_type=0