[fltsim.0]
title = Super Stallion MAR
sim = ch-53e
model =
panel =
sound =
texture =
kb_checklists =
kb_reference =
atc_id =
atc_airline =
ui_manufacturer = "Sikorsky"
ui_type = "CH-53 Super Stallion"
ui_variation = "US Marines"
ui_typerole = "Rotorcraft"
ui_createdby = "Dunken Avionics"
description = "Classified Marine Edition"
[fltsim.1]
title = Super Stallion NAV
sim = ch-53e
model =
panel =
sound =
texture = 1
kb_checklists =
kb_reference =
atc_id =
atc_airline =
ui_manufacturer = "Sikorsky"
ui_type = "CH-53E"
ui_variation = "US Navy"
ui_typerole = "Rotorcraft"
ui_createdby = "Dunken Avionics"
description = "Classified Navy Edition"
[fltsim.2]
title = Super Stallion MARINEONEnd53
sim = ch-53e
model =
panel =
sound =
texture = marineonend53
kb_checklists =
kb_reference =
atc_id =
atc_airline = Marine One
ui_manufacturer = "Air Force One Marine One"
ui_type = "Sikorsky CH-53E ND"
ui_variation = "Presidential Edition"
ui_typerole = "Rotorcraft"
ui_createdby = "Dunken Avionics"
description = "Classified Presidential Edition"
[Views]
eyepoint = 13.2, 2.0, 1.8
[CameraDefinition.001]
Title = "Left Seat"
Guid = {8ff6c134-098d-409f-baec-caba3f683f98}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=100
HeadingPanRate=100
InitialXyz=-1.3, 0.0, 0.0
InitialPbh=2, 0, 0
[CameraDefinition.002]
Title = "Center Console"
Guid = {4B8BEE17-EB6C-42c9-BDC4-28A31364680D}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.7
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.65, 0.2, -0.4
InitialPbh=48.0, 0, 0
[CameraDefinition.003]
Title = "Overhead Panel"
Guid = {E153F994-4F5A-4982-865C-3C9C8E964048}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.3
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.65, 0.1, -0.4
InitialPbh=-56.0, 0, 0
[CameraDefinition.004]
Title = "Map"
Guid = {827A0F00-69CD-4fdc-8E9D-A0EBC3AE953C}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.9
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-1.08, -0.36, 0.3
InitialPbh=7.0, 0, 0
[CameraDefinition.005]
Title = "Side Door"
Guid = {222921D1-DDF1-4deb-93E1-791BE12FE7AB}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=80
HeadingPanRate=80
InitialXyz=-0.8, 0.4, -4.2
InitialPbh=19, 0, 110
[CameraDefinition.006]
Title = "Rear Door"
Guid = {9A2A4D53-3090-4b10-B0C2-2FFDF4065E86}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=80
HeadingPanRate=80
InitialXyz=0.0, 0.25, -7.5
InitialPbh=25, 0, 190
[General]
atc_type = Helicopter
atc_model = Helicopter
performance = "Classified"
editable = 1
Category = Helicopter
[WEIGHT_AND_BALANCE]
max_gross_weight = 28000 // (pounds)
empty_weight = 10500 // (pounds)
reference_datum_position = 0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 350, -15.0, -2.8, 2.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 350, -15.0, 2.8, 2.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 0, -26.4, 0.0, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 0, -30.1, 0.0, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 0, -33.4, 0.0, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 0, -38.0, 0.0, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Co-Pilot"
station_name.1 = "Pilot"
station_name.2 = "Radar"
station_name.3 = "Classified 1"
station_name.4 = "Classified 2"
station_name.5 = "cargo Hold"
;Moments of Inertia
empty_weight_pitch_MOI = 158750
empty_weight_roll_MOI = 63184
empty_weight_yaw_MOI = 150000
empty_weight_coupled_MOI = 0
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
electric_always_available = 0
[Auxiliary Power Unit]
available = 1
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 1, -2.90, -12.70, 1.67, fx_f20_beacon
light.1 = 1, -2.90, 12.70, 1.67, fx_f20_beacon
light.2 = 2, -2.90, -12.70, 1.67, fx_f20_strobe
light.3 = 2, -2.90, 12.70, 1.67, fx_f20_strobe
light.4 = 2, -52.50, -4.00, 16.65, fx_f20_strobe
light.5 = 1, -52.50, -4.00, 16.65, fx_f20_beacon
light.6 = 1, 10.95, 0, -3.20, fx_f20_beacon
light.7 = 2, 10.95, 0, -3.20, fx_f20_strobe
light.8 = 4, 0, 0, 12, fx_vclight_grn
light.9 = 4, 16.70, 1, 4.87, fx_vclight_grn
light.10= 4, 16.70, -1, 4.87, fx_vclight_grn
[Helicopter]
reference_length = 85.0
reference_frontal_area = 125.0
reference_side_area = 308
side_aero_center = -38.0
lift_aero_center = -34.0
right_trim_scalar = 0.0
correlator_available = 1
governed_pct_rpm_ref = 1.0
governor_pid = 0.25, 0, 0.9, 0.01, 0.15
rotor_brake_scalar = 8.0
torque_scalar = 20.0
tail_rotor_translating_scalar = 0.5
cyclic_roll_control_scalar = 1.5
cyclic_pitch_control_scalar = 2.0
pedal_control_scalar = 0.4
collective_on_rotor_torque_scalar = 0.4
[fuselage_aerodynamics]
drag_force_cf = 0.01
side_drag_force_cf = 0.01
pitch_damp_cf = -4.0
pitch_stability_cf = 0.5
roll_damp_cf = -6.0
yaw_damp_cf = -0.8
yaw_stability_cf = 0.27
[GeneralEngineData]
engine_type = 3 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 2.0, -8.0, 8.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 2.0, 8.0, 8.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 = -45.0, -1.0, 8.0 //(feet) longitudinal, lateral, vertical distance from reference datum
min_throttle_limit = 0.0; //Minimum percent throttle. Generally negative for turbine reverser
fuel_flow_scalar = 1.85 //Fuel flow scalar
[TurbineEngineData]
fuel_flow_gain = 0.013 //Gain on fuel flow
inlet_area = 3.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 9875.0 //RPM, second stage compressor rated value
static_thrust = 28875.0 //Lbs, max rated static thrust at Sea Level
ThrustSpecificFuelConsumption = 0.85 //Thrust specific fuel consumption
[turboshaft_engine]
power_scalar = 1.85 //Scalar on Turboprop power
maximum_torque = 4800.0 //Maximum torque available (ft-lbs)
rated_shaft_hp = 5800.0 //rated HP of shaft
PowerSpecificFuelConsumption = 1.0 //Brake power specific fuel consumption (turboshaft only)
[MainRotor]
Position = 1.0, 0.0, 8.0 //Longitudinal, Lateral, Vertical feet from datum
Radius = 38.0 //feet
max_disc_angle = 7.3
static_pitch_angle = 4
static_bank_angle = 0
RatedRpm = 450
Number_of_blades = 6
Weight_per_blade = 258.0
inflow_vel_reference = 58.0
weight_to_moi_factor = 0.563
[SecondaryRotor]
Position = -45.0, 0.0, 8.0 //Longitudinal, Lateral, Vertical feet from datum
Radius = 10.0 //feet
max_disc_angle = 7.3
static_pitch_angle = 4
static_bank_angle = 0
RatedRpm = 450
Number_of_blades = 4
Weight_per_blade = 150.0
inflow_vel_reference = 58.0
weight_to_moi_factor = 0.563
[fuel]
Center1 = 1.0, 0.0, -1.0, 450.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2 = 1.0, -10.0, -1.0, 250.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center3 = 1.0, 10.0, -1.0, 250.0, 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 = 3
electric_pump = 1
fuel_dump_rate = 0.00287 //Percent of max quantity per second, i.e. about 1 minute for full fuel
[contact_points]
static_pitch = -4.0
static_cg_height = 7.75
max_number_of_points = 12
gear_system_type = 1
point.0 = 1, 20.3, 0.0, -4.5, 6500, 0, 1.15, 75, 0.90, 1.8, 0.6, 3, 3, 2, 250, 300 ; nose wheel
point.1 = 1, -7.1, -6.3, -5.9, 6500, 1, 1.8, 0, 0.90, 1.8, 0.6, 3, 3, 3, 250, 300 ; left wheel
point.2 = 1, -7.1, 6.3, -5.9, 6500, 2, 1.8, 0, 0.90, 1.8, 0.6, 3, 3, 3, 250, 300 ; right wheel
point.3 = 4, 20.3, 0.0, -4.0, 6500, 0, 1.15, 75, 0.90, 1.8, 0.6, 3, 3, 2, 250, 300 ; nose wheel
point.4 = 4, -7.1, -6.3, -6.0, 6500, 1, 1.8, 0, 0.90, 1.8, 0.6, 3, 3, 3, 250, 300 ; left wheel
point.5 = 4, -7.1, 6.3, -6.0, 6500, 2, 1.8, 0, 0.90, 1.8, 0.6, 3, 3, 3, 250, 300 ; right wheel
point.6 = 2, 19.5, 0.0, -2.0, 6500, 0, 0.0, 0, 0.0, 0.0, 0.0, 0, 0, 5, 250, 300 ; scrape nose fuse
point.7 = 2, -14.7, 0.0, -2.0, 6500, 0, 0.0, 0, 0.0, 0.0, 0.0, 0, 0, 6, 250, 300 ; scrape aft fuse
point.8 = 2, -39.4, 0.0, -2.0, 6500, 0, 0.0, 0, 0.0, 0.0, 0.0, 0, 0, 9, 250, 300 ; scrape boom
point.9 = 2, 0.0, -8.8, -2.0, 6500, 0, 0.0, 0, 0.0, 0.0, 0.0, 0, 0, 4, 250, 300 ; scrape left pylon
point.10 = 2, 0.0, 8.8, -2.0, 6500, 0, 0.0, 0, 0.0, 0.0, 0.0, 0, 0, 4, 250, 300 ; scrape right pylon
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
windshield_rain_effect_available = 1
[exits]
number_of_exits = 3
exit.0 = 0.4 // (0=Main 1=Cargo 2=Emergency)
exit.1 = 0.4 // (0=Main 1=Cargo 2=Emergency)
exit.2 = 0.4 // (0=Main 1=Cargo 2=Emergency)
[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
[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
direction_indicator.1 = 3,0
[Reference Speeds]
flaps_up_stall_speed = 0 //Knots True (KTAS)
full_flaps_stall_speed= 0 //Knots True (KTAS)
cruise_speed = 800.0 //Knots True (KTAS)
max_indicated_speed = 3500.0 //Knots True (KTAS)
max_mach = 3.0
[autopilot]
autopilot_available = 1
flight_director_available = 1
default_vertical_speed = 1800.000000
autothrottle_available = 0
pitch_takeoff_ga = 8.000000
max_pitch = 12.000000
max_pitch_acceleration = 1.000000
max_pitch_velocity_lo_alt = 0.1
max_pitch_velocity_hi_alt = 0.1
max_pitch_velocity_lo_alt_breakpoint = 20000.000000
max_pitch_velocity_hi_alt_breakpoint = 28000.000000
max_bank = 68.000000
max_bank_acceleration = 5.800000
max_bank_velocity = 8.000000
max_throttle_rate = 0.100000
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 = 0.000000
[yaw_string]
yaw_string_available = 1
[brakes]
toe_brakes_scale = 1.5
differential_braking_scale = 1.8
parking_brake = 1
[hydraulic_system]
normal_pressure = 3000.0 //PSI
engine_map = 1,1,1 //pumps on Eng1,2,3
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0 = 1,0
turn_indicator.1 = 1,0
[keyboard_response]
elevator = 100, 180 //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
aileron = 200, 1000 //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
rudder = 200, 1000 //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1.0
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[Sling.0]
hoist_extend_rate = 5 //Feet per second
hoist_retract_rate = -5 //Feet per second
position = -34.7, 6.7, 7.0 //Feet from datum
max_stretch = 2.0 //Max stretch distance at ultimate load
damping_ratio = 0.6 //0 for no damping to 1.0 for critically damped.
rated_load = 600 //Characteristics tension of cable in pounds
ultimate_load = 2250 //Breaking force in pounds
tolerance_angle=45 //Angle, in degrees, used to determine lateral breaking force limit
auto_pickup_range = 8 //Max Range, in feet, for auto-pickup
auto_pickup_max_speed = 8.5 //Maximum speed (feet per second) for auto-pickup
hoist_payload_station = 4 //Payload station in which the hoist will load in and out of. 1 is first station.
hoist_door=2 //Door associated with hoist. Must be open for use.
[Sling.1]
position = -30.5, 0.0, 0.0 //Feet from datum
max_stretch = 2.0 //Max stretch distance at ultimate load
damping_ratio = 0.75 //0 for no damping to 1.0 for critically damped.
rated_load = 10000 //Characteristics tension of cable in pounds
ultimate_load = 25000 //Breaking force in pounds
tolerance_angle=70 //Angle, in degrees, used to determine lateral breaking force limit
auto_pickup_range = 8 //Max Range, in feet, for auto-pickup
auto_pickup_max_speed = 8.5 //Maximum speed (feet per second) for auto-pickup
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available
[vacuum_system]
max_pressure = 5.15
vacuum_type = 1
electric_backup_pressure = 5.15
engine_map = 1,0,0,0
[pneumatic_system]
max_pressure = 18.0
bleed_air_scalar = 1.0
[deice_system]
structural_deice_type = 2