[fltsim.0]
title=CH-46 Stealth
sim=CH46
model=
panel=
sound=
texture=
atc_ID=
atc_airline=
atc_flight_number=
ui_manufacturer="Skunkworks"
ui_type="CH-46 Stealth"
ui_variation="Covert Operations"
ui_typerole="Stealth Helicopter"
ui_createdby="Dunken-Industries"
description=CH-46 was first introduced in 1964 as a dual rotor heavy lift helicopter. Over 600 airframes were built, this one is one of the legendary "black Helocopters" used by the C.I.A, it has been retro fitted with state of the art stealth / radar / whisper modes make this a urban weapon of the future...Now.
[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="Skunkworks"
atc_model=CH-46 Stealth
performance= "classified does not exsist"
editable=1
Category=Helicopter
[Views]
eyepoint=13.43, 2.0, 1.8
[WEIGHT_AND_BALANCE]
max_gross_weight = 38392 // (pounds)
empty_weight = 10963 // (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 = 485, 15.0, -2.0, 1.5 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 485, 15.0, 2.0, 1.5 // 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
[Lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0= 1, -19.9, 0, 8.9, fx_f20_beacon,
light.1= 2, -19.9, 0, 8.9, fx_f20_strobe,
light.2= 1, 2.0, 0, -4.93, fx_f20_beacon,
light.3= 2, 2.0, 0, -4.93, fx_f20_strobe,
light.4= 1, 12.5, 0, 6.28, fx_f20_beacon,
light.5= 2, 12.5, 0, 6.28, fx_f20_strobe,
light.6= 3, -17.0, 0, 10.0, fx_f20_vclight_red
light.7= 3, 16.0, 0, 8.0, fx_f20_vclight_red
light.8 = 5, 22.1, -0.33, -2.0, fx_landing,
light.9 = 5, 22.1, 0.33, -2.0, fx_landing,
[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
[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 = 1.0
side_drag_force_cf = 1.0
pitch_damp_cf = -4.0
pitch_stability_cf = 0.5
cruise_lift_scalar = 9.998
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 = 16.0, 0, 8.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -17.0, 0, 10.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 = -17.0, 0, 10.0 //(feet) longitudinal, lateral, vertical distance from reference datum
min_throttle_limit = 0.0; //Minimum percent throttle. Generally negative for turbine reverser
fuel_flow_scalar= 1.850 //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 = 29650 //RPM, second stage compressor rated value
static_thrust = 2850 //Lbs, max rated static thrust at Sea Level
ThrustSpecificFuelConsumption = 2.0 //Thrust specific fuel consumption
[turboshaft_engine]
power_scalar = 1.0 //Scalar on Turboprop power
maximum_torque = 1335 //Maximum torque available (ft-lbs)
rated_shaft_hp = 2263 //rated HP of shaft
PowerSpecificFuelConsumption = 2.0 //Brake power specific fuel consumption (turboshaft only)
[MainRotor]
Position = 16.0, 0, 8.0 //Longitudinal, Lateral, Vertical feet from datum
Radius = 38.51 //feet
max_disc_angle = 7.0
static_pitch_angle = 3
static_bank_angle = 0
RatedRpm = 450
Number_of_blades = 4
Weight_per_blade = 250.0
inflow_vel_reference = 58.0
weight_to_moi_factor=0.563
[SecondaryRotor]
Position = -17.0, 0, 10.0 //Longitudinal, Lateral, Vertical feet from datum
Radius = 38.51 //feet
max_disc_angle = 7.0
static_pitch_angle = 4
static_bank_angle = 0
RatedRpm = 450
Number_of_blades = 3
Weight_per_blade = 250.0
inflow_vel_reference = 58.0
weight_to_moi_factor=0.563
[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 ;Main / Hoist door
exit.1 = 0.17 ;Rear ramp
exit.2 = 0.4 ;Pilot
[fuel]
Center1 = 1.5, 0.0, -1.0, 125.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2 = 1.5, -1.0, -1.0, 125.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center3 = 1.5, 1.0, -1.0, 125.0, 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]
point.0 = 1, 15.80, 0.00, -6.60, 4500, 0, 0.75,140, 0.38, 1.26, 0.5, 0, 0, 2, 00, 500 ; nose wheel center
point.1 = 1, -7.42, -6.35, -7.15, 4500, 1, 0.80, 0, 0.37, 1.25, 0.5, 0, 0, 3, 00, 500 ; aft wheel left
point.2 = 1, -7.42, 6.35, -7.15, 4500, 2, 0.80, 0, 0.37, 1.25, 0.5, 0, 0, 3, 00, 500 ; aft wheel right
point.3 = 4, 15.80, 0.00, -3.0, 4500, 0, 0.75,140, 0.38, 1.26, 0.5, 0, 0, 2, 00, 500 ; nose float
point.4 = 4, -7.42, -6.35, -4.2, 4500, 1, 0.80, 0, 0.37, 1.25, 0.5, 0, 0, 3, 00, 500 ; left float
point.5 = 4, -7.42, 6.35, -4.2, 4500, 2, 0.80, 0, 0.37, 1.25, 0.5, 0, 0, 3, 00, 500 ; right float
point.6 = 2, 18.60, 0.00, -3.0, 4500, 0, 0.00, 0, 0.0, 0.0, 0.0, 0, 0, 5, 0, 0 ; scrape fuse front
point.7 = 2, -7.50, -6.68, -4.2, 4500, 0, 0.00, 0, 0.0, 0.0, 0.0, 0, 0, 6, 0, 0 ; scrape fuse aft left
point.8 = 2, -7.50, 6.68, -4.2, 4500, 0, 0.00, 0, 0.0, 0.0, 0.0, 0, 0, 9, 0, 0 ; scrape fuse aft right
point.9 = 2, -18.50, 0.00, -3.0, 4500, 0, 0.00, 0, 0.0, 0.0, 0.0, 0, 0, 9, 0, 0 ; scrape fuse aft
point.10= 5, 0.00, 0.00, 0.00, 0, 0, 0.00, 0, 0.0, 0.0, 0.0, 1, 1, 0, 0, 0 ; Water rudder
static_pitch = -1.0
static_cg_height = 6.65
max_number_of_points = 11
gear_system_type = 1
[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 = 600.0 //Knots True (KTAS)
max_indicated_speed = 3529.0 //Knots True (KTAS)
max_mach=5.64
[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=95.000000
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 =1.0
differential_braking_scale = 1.5
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 //Breakpoint speeds (knots) on the keyboard increments of control surfaces.
aileron = 200, 1000 //Breakpoint speeds (knots) on the keyboard increments of control surfaces.
rudder = 200, 1000 //Breakpoint speeds (knots) on the keyboard increments of control surfaces.
[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=5.150000
vacuum_type=1
electric_backup_pressure=5.150000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=2