[fltsim.0]
title=Gulfstream V
sim=ldgv
model=
panel=
sound=
texture=
kb_checklists=GV_check
kb_reference=GV_ref
atc_id_enable=1
atc_id=PH-FVL
ui_manufacturer=Gulfstream
ui_type=Ultra long range large corporate transport
ui_variation=Gulfstream G550
description=The Gulfstream G550 is the largest and latest development of the Gulfstream line of corporate transports, designed to fly intercontinental distances. It competes with Bombardier's Global Express, the Boeing Business Jet and Airbus A319CJ.\n\nModel, Sounds & Textures By:\nPeter Brun (peter@liderdesigns.com)\nFlight Dynamics and Data By:\nDouglas E. Trapp (KC6ZOF@Yahoo.com)\nFS Flight Dynamics Engineer\nArlington, Texas\nAugust 2009\n
atc_airline=
atc_flight_number=
atc_heavy=0
visual_damage=1
atc_parking_types=GATE
atc_parking_codes=INT
atc_id_color=0xff000000
[General]
atc_type=GULFSTREAM
editable=1
performance=Note: Data below reflects this aircraft model with real-world specifications.\n\nPowerplants: Two Rolls-Royce BR710-48 @ 15,385 lbf ea\nLength: 96ft 5in\nHeight @ tail: 25ft 10in\nCabin length: 50ft 1in\nCabin height: 6ft 2in\nCabin width: 7ft 4in n\nWingspan: 93ft 5in\nWing area: 1,137 ft/sq\nEmpty weight: 48,300 lb\nMTOW: 91,000 lb\nRamp weight: 91,400 lb\nMLW: 75,300 lb\nFuel capacity: 6,164 US gal\nClimb rate: 2,000 ft/min to FL370\nMmo: .885\nLong distance cruise speeds:\nmach .80-.84 @ FL370 to FL450\nmach .83-.87 @ FL450 to FL510\nCertified service ceiling: FL510\nMax Range: 8,700 nm @ FL510E, mach .80\nCrew: 2\nPassengers: 6\nLuggage: 442 lb\n
atc_model=G550
Category=airplane
[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
point.0=1, 38.83, 0.00, -6.70, 981.1, 0, 0.8500, 70.0, 0.25, 2.5, 0.8878, 9.0, 10.0, 0, 180.0, 200.0
point.1=1, -2.19, -5.39, -8.10, 1174.8, 1, 1.5000, 0.0, 1.0, 2.5, 0.8456, 13.0, 15.0, 2, 180.0, 200.0
point.2=1, -2.19, 5.39, -8.10, 1174.8, 2, 1.5000, 0.0, 1.0, 2.5, 0.8456, 13.0, 15.0, 3, 180.0, 200.0
point.3=2, -5.83, -33.32, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -5.83, 33.32, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -36.29, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 46.47, 0.00, -1.50, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
static_pitch = -0.750
static_cg_height = 6.410
gear_system_type=0
[Views]
eyepoint = 36.48, -1.15, 4.15
[electrical]
// ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot = 0, 5 , 17.0
flap_motor = 1, 0 , 1.0
gear_motor = 0, 5 , 17.0
avionics_bus = 0, 0 , 1.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 0 , 1.0
additional_system = 0, 0 , 1.0
marker_beacon = 1, 2 , 17.0
gear_warning = 7, 0 , 99.0
gear_motor = 4, 0 , 1.0
fuel_pump = 0, 0 , 1.0
fuel_transfer_pump = 0, 0 , 1.0
starter1 = 0, 20, 17.0
starter2 = 0, 0 , 1.0
light_nav = 0, 0 , 1.0
light_beacon = 0, 0 , 1.0
light_landing = 0, 0 , 1.0
light_taxi = 0, 0 , 1.0
light_strobe = 0, 0 , 1.0
light_panel = 0, 7 , 99.0
light_recognition = 0, 0 , 1.0
light_wing = 0, 0 , 1.0
marker_beacon = 0, 0 , 1.0
standby_vacuum = 0, 0 , 1.0
auto_brakes = 0, 0 , 1.0
hydraulic_pump = 0, 0 , 1.0
propeller_device = 0, 0 , 1.0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 0.8
induced_drag_scalar = 0.8
elevator_effectiveness = 1.0
aileron_effectiveness = 1.5
rudder_effectiveness = 1.0
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[airplane_geometry]
wing_area=1137.000
wing_span=93.5
wing_root_chord=18.480
wing_dihedral=2.330
wing_incidence=0.000
wing_twist=1.000
oswald_efficiency_factor=2.500
wing_winglets_flag=1
wing_sweep=28.000
wing_aspect_ratio=7.7
wing_pos_apex_lon=0.000
wing_pos_apex_vert=0.000
htail_area=244.870
htail_span=35.160
htail_pos_lon=-49.167
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=30.000
vtail_area=140.160
vtail_span=11.720
vtail_sweep=37.000
vtail_pos_lon=-47.917
vtail_pos_vert=5.833
elevator_area=57.500
aileron_area=25.000
rudder_area=32.300
elevator_up_limit=27.502
elevator_down_limit=20.626
aileron_up_limit=25.000
aileron_down_limit=25.000
rudder_limit=23.491
elevator_trim_limit=19.481
spoiler_limit=50.000
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.465812
negative_g_limit_flaps_up=-2.600427
negative_g_limit_flaps_down=-1.698718
[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
//Payload = 1,800 lb
//Pax weight = 1,360 lb
//Luggage weight = 442 lb @ 55 lb/pax
station_load.0=170.000000,25.000000,2.5000000,1.800000//Pilot
station_load.1=170.000000,25.000000,-2.5000000,1.800000//Co-Pilot
station_load.2=170.000000,10.000000,3.500000,2.000000//Pax
station_load.3=170.000000,10.000000,-3.500000,2.000000//Pax
station_load.4=170.000000,5.000000,3.500000,2.000000//Pax
station_load.5=170.000000,5.000000,-3.500000,2.000000//Pax
station_load.6=170.000000,0.000000,3.500000,2.000000//Pax
station_load.7=170.000000,0.000000,-3.500000,2.000000//Pax
station_load.8=442.000000,-18.000000,0.000000,-2.000000//Luggage
empty_weight= 48300.000
empty_weight_roll_MOI= 150774.000
empty_weight_pitch_MOI= 242040.000
empty_weight_yaw_MOI= 416940.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 91000.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[fuel]
//6,164 US gal = 41,300 lb
Center1= 1.800, 0.000, -3.000, 1380.000, 0.000
LeftMain= -1.800, -9.360, -1.500, 2392.000, 0.000
RightMain= -1.800, 9.360, -1.500, 2392.000, 0.000
fuel_type= 2.000
number_of_tank_selectors= 1
electric_pump=0
[GeneralEngineData]
engine_type= 1
Engine.0= -18.667, -7.500, 5.750
Engine.1= -18.667, 7.500, 5.750
fuel_flow_scalar= 1.000000
min_throttle_limit=-0.250000
[smokesystem]
smoke.0 = -28.667, -7.500, 5.750, fx_smoke_f6
smoke.1 = -28.667, 7.500, 5.750, fx_smoke_f6
[TurbineEngineData]
//Rolls Royce BR710-48
bypass_ratio=3.3
fuel_flow_gain= 0.002
inlet_area= 5.91
rated_N1_rpm= 3854.000
rated_N2_rpm= 11055.000
static_thrust= 15385.000
afterburner_available= 0
reverser_available= 1
[jet_engine]
thrust_scalar =1.000
[flaps.0]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 8 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 8 // degrees
flaps-position.2 = 20 // degrees
flaps-position.3 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
[flaps.1]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 0 // degrees
flaps-position.2 = 8 // degrees
flaps-position.3 = 20 // degrees
flaps-position.4 = 30 // degrees
flaps-position.5 = 45 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
[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, 200
aileron = 100, 200
rudder = 100, 200
[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
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
//exit_rate.1 = 0.4 ;Percent per second
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[Reference Speeds]
flaps_up_stall_speed = 112.0 //Knots True (KTAS)
full_flaps_stall_speed = 102.0 //Knots True (KTAS)
cruise_speed = 488.0 //Knots True (KTAS)
max_indicated_speed=410.0
max_mach=0.885
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 2000.000
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_takeoff_ga= 0
autothrottle_max_rpm= 110.000
pitch_takeoff_ga = 8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=30,15
max_bank_acceleration=1.8
max_bank_velocity=3.00
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 = 1.0
[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=35999 ; 0 - 35999 degrees
crash_magnitude2=10000 ; 0 - 10000
crash_direction2=35999 ; 0 - 35999 degrees
crash_period2=75000000 ; in microseconds
crash_duration2=25000000 ; in microseconds
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3, -13.25, -45.50, 0.55, fx_navredm ,
light.1=3, -13.25, 45.50, 0.55, fx_navgrem ,
light.2=3, -38.95, 0.00, 4.35, fx_navwhi ,100
light.3=2, -13.35, -45.75, 0.55, fx_strobe ,
light.4=2, -13.35, 45.75, 0.55, fx_strobe ,
light.5=1, 13.55, 0.00, 7.08, fx_beaconh ,
light.6=1, -2.55, 0.00,-2.50, fx_beaconb ,
light.7=4, 34.30, -1.50, 3.30, fx_vclight,
light.8=4, 34.30, 1.50, 3.30, fx_vclight,
light.9=1, 34.10, -1.00, 3.4, fx_vclighth ,
light.10=1, 34.10, 1.00, 3.4, fx_vclighth ,
[brakes]
toe_brakes_scale=1.2
parking_brake=1
auto_brakes=0
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0
