[fltsim.0]
title=Gulf_IV
sim=Gulf_IV
model=
panel=
sound=
texture=
kb_checklists=Gulf_IV_check
kb_reference=Gulf_IV_ref
atc_id=N01CF
ui_manufacturer=Gulfstream
ui_type=Gulf_IV
ui_variation=American Spirit Racing
description=The Gulfstream IV is still the best-selling large cabin, long-range business jet in the market. It is the aircraft chosen by nine of the top ten Fortune 500 companies and more than 30 world governments including the President of the United States. The Gulfstream IV has a range of 4,220 nautical miles and a cruising speed of 560 miles per hour. The Gulfstream IV operates efficiently at altitudes as high as 45,000 feet, enabling it to fly above commercial airline traffic and adverse weather.
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=GULFSTREAM
atc_model=
editable=1
performance=Cruise Speed Mach 0.81 464 kts 859kmh\nEngines\tRolls Royce TAY611-8 13,850 lb thrust\nMaximum Range 4,480 nm\nService Ceiling 45,000 ft
15,545 m\n\nFuel Capacity\t\n29,500lb
\n\nMaximum Gross Weight\t\n74,500 lb
\n\nUseful Load\t\n31,750 lb
[WEIGHT_AND_BALANCE]
max_gross_weight= 74500.000
empty_weight= 49000.000
reference_datum_position= 34.500, 0.000, 0.000
empty_weight_CG_position= -35.790, 0.000, 0.000
max_number_of_stations=50
station_load.0= 170.000, -17.000, -1.200, 0.000
station_load.1= 170.000, -17.000, 1.200, 0.000
station_load.2= 170.000, -22.500, -1.200, 0.000
station_load.3= 170.000, -22.500, 1.200, 0.000
station_load.4= 170.000, -26.700, -1.200, 0.000
station_load.5= 170.000, -26.700, 1.200, 0.000
station_load.6= 170.000, -30.900, -1.200, 0.000
station_load.7= 170.000, -30.900, 1.200, 0.000
station_load.8= 170.000, -35.100, -1.200, 0.000
station_load.9= 170.000, -35.100, 1.200, 0.000
station_load.10= 100.000, -42.000, 0.000, 0.000
station_load.11= 50.000, -45.000, 0.000, 0.000
;Moments of Inertia
empty_weight_pitch_MOI= 350048.000
empty_weight_roll_MOI= 177442.000
empty_weight_yaw_MOI= 543541.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[electrical]
max_battery_voltage=12.0
generator_alternator_voltage=13.8
max_generator_alternator_amps=40.0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus=0, 10, 9.5
avionics=1, 5 , 9.5
additional_system=0, 20, 9.5
marker_beacon=1, 2 , 9.0
fuel_pump=0, 5 , 9.0
[flight_tuning]
cruise_lift_scalar=1.401
parasite_drag_scalar=1.301
induced_drag_scalar=1.301
elevator_effectiveness=1.000
aileron_effectiveness=0.701
rudder_effectiveness=0.800
pitch_stability=1.201
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= -42.800, -4.800, 0.800
Engine.1= -42.800, 4.800, 0.800
fuel_flow_scalar= 0.900
[TurbineEngineData]
fuel_flow_gain= 0.003
inlet_area= 8.290
rated_N2_rpm= 29920.000
static_thrust= 13850.000
afterburner_available= 0
reverser_available= 1
[jet_engine]
thrust_scalar=1.000
[SMOKESYSTEM]
smoke.0=0.8,-48.4,-4.8, fx_smoke_rxS3
smoke.1=0.8,-48.4, 4.8, fx_smoke_rxS3
//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
[contact_points]
point.0= 1.000, -11.170, 0.000, -4.120, 3200.100, 0.000, 0.635, 45.000, 0.120, 2.500, 0.850, 10.000, 10.000, 0.000, 0.000, 0.000
point.1= 1.000, -37.250, -6.750, -5.520, 3200.800, 1.000, 0.635, 0.000, 1.000, 2.500, 0.946, 9.000, 9.000, 2.000, 0.000, 0.000
point.2= 1.000, -37.250, 6.750, -5.520, 3200.800, 2.000, 0.635, 0.000, 1.000, 2.500, 0.946, 9.000, 9.000, 3.000, 0.000, 0.000
point.3= 2.000, -37.830, -23.920, -3.000, 787.400, 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, -37.830, 23.920, -3.000, 787.400, 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, -57.170, 0.000, 0.000, 787.400, 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, -11.470, 0.000, -1.500, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= -0.750
static_cg_height= 4.410
[Views]
eyepoint=4.31, -1.31, 6.44
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=1, -18.223, 0.00, 8.595, fx_beaconbGulf ,
light.1=1, -36.572, 0.00, 0.30, fx_beaconbGulf ,
light.2=3, -41.75, -39.00, 2.80, fx_navredm ,
light.3=3, -41.75, 39.00, 2.80, fx_navgrem ,
light.4=2, -41.75, -39.00, 2.80, fx_strobe ,
light.5=2, -41.75, 39.00, 2.80, fx_strobe ,
light.6=2, -67.10, 0.00, 5.73, fx_strobe ,
light.7=3, -67.10, 0.00, 5.73, fx_navwhi ,
light.8=4, 4.90, 0.00, 5.44, fx_vclight ,
light.9=4, -0.50, 0.00, 5.44, fx_vclight ,
light.10=4, -10.00, 0.00, 5.44, fx_vclighth ,
light.11=4, -20.00, 0.00, 5.44, fx_vclighth ,
light.12=4, -33.00, 0.00, 5.44, fx_vclighth ,
light.13=6, 17.0, 0.00, -5.0, RNLE2 ,
light.14=5, -10.0, -4.00, -5.0, RNLE2 ,
light.15=5, -10.0, 4.00, -5.0, RNLE2 ,
[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
[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=150, 250
aileron=150, 250
rudder=150, 250
[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=3,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
LeftMain= -36.300, -10.000, -1.500, 2202.200, 0.000
RightMain= -36.300, 10.000, -1.500, 2202.200, 0.000
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
[exits]
number_of_exits=2
exit_rate.0=0.05
exit_rate.1=0.1
[airplane_geometry]
wing_area= 950.390
wing_span= 77.100
wing_root_chord= 12.320
wing_dihedral= 2.500
wing_incidence= 0.000
wing_twist= -4.000
oswald_efficiency_factor= 0.860
wing_winglets_flag= 1
wing_sweep= 35.000
wing_pos_apex_lon= -28.000
wing_pos_apex_vert= 0.000
htail_area= 220.000
htail_span= 32.000
htail_pos_lon= -59.100
htail_pos_vert= 0.000
htail_incidence= 2.000
htail_sweep= 30.000
vtail_area= 82.000
vtail_span= 12.400
vtail_sweep= 35.000
vtail_pos_lon= -55.000
vtail_pos_vert= 4.100
elevator_area= 57.000
aileron_area= 23.500
rudder_area= 47.300
elevator_up_limit= 17.000
elevator_down_limit= 15.500
aileron_up_limit= 18.000
aileron_down_limit= 18.000
rudder_limit= 30.000
elevator_trim_limit= 15.000
spoiler_limit= 55.000
spoilerons_available= 1
aileron_to_spoileron_gain= 2.200
min_ailerons_for_spoilerons= 5.000
min_flaps_for_spoilerons= 0.000
[Reference Speeds]
flaps_up_stall_speed= 112.000
full_flaps_stall_speed= 102.000
cruise_speed= 464.000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8.00000
use_no_default_bank=1
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
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=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 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
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 5.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.500
drag_scalar= 1.200
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 39.000, 0.000