[fltsim.0]
title=Lockheed C-5 Galaxy Eagle
sim=C5a
model=
panel=
sound=
texture=
checklists=
ui_manufacturer=Lockheed
ui_type=C5A
ui_variation=C5-B GALAXY Eagle
atc_heavy=0
atc_id=N5A5EA
atc_airline=Eagle
atc_flight_number=5CA
description=The Galaxy is one of the world's largest aircraft. It is almost as long as a football field and as high as a six-story building and has a cargo compartment about the size of an eight-lane bowling alley. The C-5 is the only aircraft that can transport any of the Army's combat equipment, including the 74-ton (66,600-kilogram) mobile scissors bridge, tanks and helicopters.\n
[General]
atc_type=LOCKHEED
atc_model=C5
editable=1
performance=Cruise Speed\n0.85 Mach 565 mph 910 km\/h\n\nEngine options\nPratt & Whitney PW4062\nRolls-Royce RB211-524H\nGeneral Electric CF6-80C2B5F\n\nMaximum Range\n7,325 nm 13,570 km\n\nMaximum Certified Operating Altitude 45,100 ft 13,747 m\n\nFuel Capacity\n57,285 gal 216,840 L\n\nBasic Operating Weight 403,486 lb 182,020 kg\n\nLength\n231 ft, 10 in 70.6 m\n\nWingspan\n211 ft, 5 in 64.4 m\n\nHeight\n63 ft, 8 in 19.4 m\n\nSeating Typical 3-class configuration - 416\nTypical 2-class configuration - 524
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
[WEIGHT_AND_BALANCE]
max_gross_weight = 875000.000
empty_weight = 401100.000
reference_datum_position = 83.500, 0.000, 0.000
empty_weight_CG_position = -90.500, 0.000, 0.000
max_number_of_stations = 50
station_load.0 = 40000.000, -80.000, 0.000, 0.000
;Moments of Inertia
empty_weight_roll_MOI = 15352310.000
empty_weight_pitch_MOI = 24223159.000
empty_weight_yaw_MOI = 39531785.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[fuel]
Center1 = -83.500, 0.000, -7.000, 19545.000, 3.000
Center2 = -193.500, 0.000, 6.000, 3300.000, 0.000
LeftMain = -112.000, -35.000, -4.000, 16720.000, 3.000
LeftAux = -118.500, -52.000, -3.000, 500.000, 0.000
RightMain = -112.000, 35.000, -4.000, 16720.000, 3.000
RightAux = -118.500, 52.000, -3.000, 500.000, 0.000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
[airplane_geometry]
wing_area = 5825.000
wing_span = 211.400
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 = 1
wing_sweep = 37.500
wing_pos_apex_lon = -68.200
wing_pos_apex_vert = 0.000
htail_area = 1470.000
htail_span = 72.800
htail_pos_lon = -210.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 37.500
vtail_area = 1060.000
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 = 230.000
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
[Reference Speeds]
flaps_up_stall_speed = 140.000
full_flaps_stall_speed = 112.000
cruise_speed = 505.000
[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, -6.900
Engine.1 = -76.000, -38.900, -10.400
Engine.2 = -76.000, 38.900, -10.400
Engine.3 = -107.500, 69.500, -6.900
fuel_flow_scalar = 1.000
[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 60.000
rated_N2_rpm = 29920.000
static_thrust = 56750.000
afterburner_available = 0
reverser_available = 1
[jet_engine]
thrust_scalar =1.000
[autopilot]
use_no_default_bank=1
use_no_default_pitch=1
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;
[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, -18.400, 2000.000, 0.000, 2.000, 70.000, 2.500, 1.500, 0.900, 9.000, 8.000, 0.000, 220.000, 2029.000
point.1 = 1.000, -114.000, -17.900, -20.500, 2000.000, 1.000, 2.000, 13.000, 3.000, 2.500, 0.900, 11.000, 9.000, 2.000, 220.000, 2029.958
point.2 = 1.000, -114.000, 17.900, -20.500, 2000.000, 2.000, 2.000, 13.000, 3.000, 2.500, 0.900, 11.000, 9.000, 3.000, 220.000, 2029.958
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 = -1.000
static_cg_height = 18.000
[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, -98.30, -111.56, 2.22, fx_navredh ,
light.1 = 3, -98.30, 111.56, 2.22, fx_navgreh ,
light.2 = 3, -198.05, 0.00, 14.05, fx_navwhih ,
light.3 = 2, -98.30, -111.56, 2.22, fx_strobeh ,
light.4 = 2, -98.30, 111.56, 2.22, fx_strobeh ,
light.5 = 2, -198.97, 0.00, 51.62, fx_strobeh ,
light.6 = 1, -15.05, 0.00, 17.65, fx_beaconh ,
light.7 = 1, -50.22, 0.00, -13.05, fx_beaconb ,
light.8 = 4, 26.24, 0.00, 9.19, fx_vclighth,
[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= 2
span-outboard= 0.800
extending-time= 15.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.100
drag_scalar= 0.100
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 25.000, 0.000
flaps-position.5= 35.000, 0.000
flaps-position.6= 45.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.800
extending-time= 25.000
system_type= 1
damaging-speed= 200.000
blowout-speed= 250.000
lift_scalar= 0.700
drag_scalar= 0.900
pitch_scalar= 0.900
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000
[Flaps.2]
type= 1
span-outboard= 0.800
extending-time= 2.000
system_type= 1
damaging-speed= 200.000
blowout-speed= 250.000
lift_scalar= 0.700
drag_scalar= 0.900
pitch_scalar= 0.900
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 10.000, 0.000
flaps-position.3= 15.000, 0.000
flaps-position.4= 20.000, 0.000
flaps-position.5= 25.000, 0.000
flaps-position.6= 30.000, 0.000
flaps-position.7= 35.000, 0.000
flaps-position.8= 40.000, 0.000
