[fltsim.0]
title=FSX Boeing 747 SCA
sim=SCA
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=N905NA
atc_airline=NASA
atc_flight_number=905
atc_parking_types=CARGO, RAMP
atc_heavy=1
ui_manufacturer=Boeing
ui_type=747-123 SCA
ui_variation=Shuttle Carrier Aircraft
description=Boeing 747-123 SCA\nShuttle Carrier Aircraft\nTypical flights are eastbound to Florida\nafter a Shuttle landing in the west\nModel by: Sandro Bernardini\nModified for FSX By: Eric Buchmann\nSounds by: Emil Serafino Jr.\nFlight Dynamics and Data Corrections by:\Douglas E. Trapp\nFS Flight Dynamics Engineer\nKC6ZOF@Yahoo.com\n04 June 2009\n
[General]
atc_type=BOEING
atc_model=B741
performance=Engines: 4 X P&W JT9D-7J @ 47,900 lbf ea\nLength: 231 feet, 10 inches\nHeight at Tail: 63 feet, 5 inches\nWingspan: 195 feet, 8 inches\nFuel Capacity: 33,768 US gal\nMaximum Range mated: 2,300 nm @ FL150E, 270 KIAS\nMax Speed: 280 KIAS (mach .56)\nTypical Cruise Speed: 260 KIAS (FL130E), 270 KIAS (FL150E)\nService Ceiling Mated: 15,748 feet\nEmpty Weight: 318,053 lb (N905NA)\nMTOW: 709,881 lb\nRamp Weight: 710,000 lb\nCrew: 4\nCargo: 165,000 lb (Space Shuttle)\n\nSTS-126 route:\nCruise Altitude: FL130\nCruise Speed: 260 KIAS\n(1)KEDW-KBIF\n(2)KBIF-KNFW\n(3)KNFW-KBAD\n(4)KBAD-X68\n\nSTS-125 route:\nKEDW-KSKF\nKSKF-KCBM\nKCBM-X68\n
Category=airplane
editable=1
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[WEIGHT_AND_BALANCE]
empty_weight= 318053.000
max_gross_weight= 709881.000
reference_datum_position = 83.500, 0.000, 0.000
empty_weight_CG_position = -90.500, 0.000, 0.000
max_number_of_stations = 50
//Crew Weight = 700 lb @ 175 lb X 4
//Shuttle Weight = 165,000 lb
station_load.0 =165700.0,-100.0,0.0,35.0,//Space Shuttle and Flight Crew
;Moments of Inertia
empty_weight_roll_MOI= 37018662.500
empty_weight_pitch_MOI= 46713121.500
empty_weight_yaw_MOI= 70309608.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[fuel]
//33,768 Gal = 226,246 lb
Center1 = -97.000, 0.0, -4.0, 9403.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -102.000, -35.0, -4.0, 8121.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux = -108.500, -52.0, -3.0, 4061.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -102.000, 35.0, -4.0, 8121.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = -108.500, 52.0, -3.0, 4061.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
[airplane_geometry]
wing_area = 7607.821 //747 wing + shuttle wing (sq ft)
wing_span = 195.670
wing_root_chord = 48.800
wing_dihedral = 7.000
wing_incidence = 2.000
wing_twist = -1.000
oswald_efficiency_factor= 0.680
wing_winglets_flag = 0
wing_sweep = 37.500
wing_pos_apex_lon = -68.200
wing_pos_apex_vert = 0.000
htail_area = 1310.000
htail_span = 72.800
htail_pos_lon = -210.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 37.500
vtail_area = 1257.317 //twin tail + shuttle tail
vtail_span = 37.100
vtail_sweep = 45.000
vtail_pos_lon = -198.500
vtail_pos_vert = 26.100
elevator_area = 327.000
aileron_area = 225.000
rudder_area = 229.900
elevator_up_limit = 25.000
elevator_down_limit = 15.000
aileron_up_limit = 25.000
aileron_down_limit = 15.000
rudder_limit = 31.500
elevator_trim_limit = 20.000
spoiler_limit = 45.000
spoilerons_available = 1
aileron_to_spoileron_gain = 3.000
min_ailerons_for_spoilerons = 10.000
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=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000
[Reference Speeds]
flaps_up_stall_speed = 140.0 //Knots True (KTAS)
full_flaps_stall_speed = 126.0 //Knots True (KTAS)
cruise_speed = 400.0 //Knots True (KTAS)
max_indicated_speed=280.000000
max_mach=0.560000
[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 = -107.500, -69.500, -1.900
Engine.1 = -76.000, -38.900, -5.400
Engine.2 = -76.000, 38.900, -5.400
Engine.3 = -107.500, 69.500, -1.900
fuel_flow_scalar = 1.000
min_throttle_limit=-0.250000
[SMOKESYSTEM]
smoke.0=-127.500, -69.500, -1.900, fx_smoke_f6
smoke.1=-96.000, -38.900, -5.400, fx_smoke_f6
smoke.2=-96.000, 38.900, -5.400, fx_smoke_f6
smoke.3=-127.500, 69.500, -1.900, fx_smoke_f6
[TurbineEngineData]
//P&W JT9D-7J
bypass_ratio=4.97000
fuel_flow_gain= 0.002
inlet_area= 47.500
rated_N1_rpm= 3854.000
rated_N2_rpm= 11055.000
static_thrust= 47900.000
afterburner_available= 0
reverser_available= 1
[jet_engine]
thrust_scalar =1.000
[autopilot]
autopilot_available = 1
flight_director_available = 1
default_vertical_speed = 1000.0
autothrottle_available = 1
autothrottle_arming_required = 1
autothrottle_max_rpm = 90.0
autothrottle_takeoff_ga = 1
pitch_takeoff_ga = 8;
use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank = 1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=0.300000
max_pitch_velocity_lo_alt_breakpoint= 7000.000000
max_pitch_velocity_hi_alt_breakpoint=24000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.03000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=1.000000
[contact_points]
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//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)
point.0 = 1.000, -25.000, 0.000, -15.000, 1000.000, 0.000, 2.042, 70.000, 0.890, 1.500, 0.850, 9.000, 8.000, 0.000, 0.000, 0.000
point.1 = 1.000, -114.000, -18.000, -15.000, 2000.000, 1.000, 2.000, 13.000, 1.400, 1.000, 0.850, 11.000, 9.000, 2.000, 0.000, 0.000
point.2 = 1.000, -114.000, 18.000, -15.000, 2000.000, 2.000, 2.000, 13.000, 1.400, 1.000, 0.850, 11.000, 9.000, 3.000, 0.000, 0.000
point.3 = 2.000, -152.600, -103.500, 3.000, 700.000, 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, -152.600, 103.500, 3.000, 700.000, 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, 3.000, 0.000, 0.000, 700.000, 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, -222.700, 0.000, 4.000, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = -0.300
static_cg_height = 13.850
gear_system_type=0
[Views]
eyepoint = -19.05, -1.97, 9.4 ; Longitude, Latitude and Vertical position from Reference Point, (FEET)
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot = 0, 5 , 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -129.47, -98.96, 11.03, fx_navredh ,
light.1 = 3, -129.47, 98.96, 11.03, fx_navgreh ,
light.2 = 3, -205.10, 0.00, 16.90, fx_navwhih ,
light.3 = 2, -135.73, -99.50, 11.03, fx_strobeh ,
light.4 = 2, -135.73, 99.50, 11.03, fx_strobeh ,
light.5 = 1, -15.75, 0.00, 19.41, fx_beaconh ,
light.6 = 1, -57.86, 0.00, -6.68, fx_beaconb ,
light.7 = 4, 4.71, 0.00, 16.41, fx_vclighth,
light.8 = 5, -54.31, -19.36, 0.61, fx_landing,
light.9 = 5, -54.25, -19.39, 0.61, fx_landing
light.10 = 5, -54.25, -19.42, 0.61, fx_landing
light.11 = 5, -54.31, 19.36, 0.61, fx_landing,
light.12 = 5, -54.25, 19.39, 0.61, fx_landing
light.13 = 5, -54.25, 19.42, 0.61, fx_landing
light.14 = 5, -53.06, -17.77, 0.46, fx_landing,
light.15 = 5, -53.03, -17.74, 0.46, fx_landing
light.16 = 5, -53.03, -17.80, 0.46, fx_landing
light.17 = 5, -53.06, 17.77, 0.46, fx_landing,
light.18 = 5, -53.03, 17.74, 0.46, fx_landing
light.19 = 5, -53.03, 17.80, 0.46, fx_landing
[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
[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
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[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
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 25.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.700
drag_scalar= 0.900
pitch_scalar= 0.900
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 5.000, 0.000
flaps-position.3= 10.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
[Flaps.1]
type= 2
span-outboard= 0.800
extending-time= 2.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.300
drag_scalar= 0.100
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[brakes]
toe_brakes_scale=1.241798
parking_brake=1
auto_brakes=4
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[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
[stall_warning]
type=1
stick_shaker=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[deice_system]
structural_deice_type=1
