[fltsim.0]
title=B-1x Stealth
sim=B-1X
model=
panel=
sound=
texture=
KB_checklists=
kb_reference=
atc_heavy=1
atc_id=
atc_airline=
ui_manufacturer="Rockwell"
ui_type="Prototype Stealth Bomber"
ui_typerole="Classified Airliner"
ui_createdby="Dunken Avionics"
description = Not Available For Disclosure.....
[CameraDefinition.001]
Title = "Right 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=20
HeadingPanRate=60
InitialXyz=0.94, 0.0, 0.0
InitialPbh=2, 0, 0
[General]
atc_type = Rockwell
atc_model = B-1x Stealth
editable = 1
performance = Classified Prototype you decide what it can do .....
Category = Airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 477000.0 //(pounds)
empty_weight = 182000.0 //(pounds)
reference_datum_position = 0, 0, 0 //(feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -1, 0, 0 //(feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 4
station_load.0 = 385.0, 60.0, -1.5, 4 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 385.0, 60.0, 1.5, 4 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 785.0, 40.0, -1.5, 4 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 985.0,-20.0, 0, 0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Pilot"
station_name.1 = "Co-Pilot"
station_name.2 = "Crew Quarters"
station_name.3 = "Weapons"
;Moments of Inertia
empty_weight_pitch_MOI = 6500000
empty_weight_roll_MOI = 1851855
empty_weight_yaw_MOI = 4345730
empty_weight_coupled_MOI = 0
CG_forward_limit = 0.000
CG_aft_limit = 1.000
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 2, 14.2, -16.2, -1.3, fx_f20_strobe
light.1 = 2, 14.2, -16.2, -1.3, fx_f20_beacon
light.2 = 2, 14.2, 16.5, -1.3, fx_f20_strobe
light.3 = 2, 14.2, 16.5, -1.3, fx_f20_beacon
light.4 = 2, -55.0, 0, 21.0, fx_f20_strobe
light.5 = 2, -55.0, 0, 21.0, fx_f20_beacon
light.6 = 4, 64.5, 0, 4.5, fx_f20_vclight_red
light.7 = 4, 5.0, 11.3, -3.0, fx_f20_vclight_red
light.8 = 4, 5.0, 11.3, -3.0, fx_f20_vclight_red
light.9 = 4, 5.0, -11.5, -3.0, fx_f20_vclight_red
light.10 = 4, 5.0, -11.5, -3.0, fx_f20_vclight_red
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine.0 = -25.000, -15.000, 0.000 //(feet) longitudinal, lateral, vertical distance from reference datum
engine.1 = -25.000, -10.000, 0.000 //(feet) longitudinal, lateral, vertical distance from reference datum
engine.2 = -25.000, 10.000, 0.000 //(feet) longitudinal, lateral, vertical distance from reference datum
engine.3 = -25.000, 15.000, 0.000 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = -0 //Minimum percent throttle. Generally negative for turbine reverser
max_contrail_temperature = -50
[TurbineEngineData]
fuel_flow_gain = 0.006 //Gain on fuel flow
inlet_area = 60.000 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 9875.000 //RPM, second stage compressor rated value
static_thrust = 78000.000 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 0 //Thrust reverser available?
[jet_engine]
thrust_scalar = 1.0
[flight_tuning]
cruise_lift_scalar = 3.5
parasite_drag_scalar = 0.8
induced_drag_scalar = 0.8
elevator_effectiveness = 1.0
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 2.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[fuel]
LeftMain = 1, -3.0, 0, 12546.0, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 1, 3.0, 0, 12546.0, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux = 0, -6.0, 0, 4482.0, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = 0, 6.0, 0, 4482.0, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftTip = 0, -9.0, 0, 1322.0, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightTip = 0, 9.0, 0, 1322.0, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1 = 0, 0, 1, 17164.0, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2 = 0, 0, 1, 3300.0, 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 = 0.08 //Percent of max quantity per second, i.e. about 1 minute for full fuel
[Flaps.0]
type= 1
span-outboard = 0.8
extending-time = 8.0
system_type = 1
damaging-speed = 800.00
blowout-speed = 900.000
lift_scalar= 0.1
drag_scalar= 0.5
pitch_scalar = 0
flaps-position.0 = 0.000, 0.000
flaps-position.1 = 10.714, 600.000
flaps-position.2 = 19.260, 500.000
flaps-position.3 = 36.430, 400.000
flaps-position.4 = 45.000, 300.000
flaps-position.5 = 60.000, 275.000
flaps-position.6 = 60.000, 250.000
[Flaps.1]
type= 1
span-outboard= 0.8
extending-time= 8.0
system_type= 1
damaging-speed = 800.00
blowout-speed = 900.00
lift_scalar = 0.1
drag_scalar = 0.5
pitch_scalar = 0
flaps-position.0 = 0.000, 0.000
flaps-position.1 = 0.000, 0.000
flaps-position.2 = 0.000, 0.000
flaps-position.3 = 0.000, 0.000
flaps-position.4 = 0.000, 0.000
flaps-position.5 = 10.000, 275.000
flaps-position.6 = 25.000, 250.000
[Flaps.2]
type= 2
span-outboard = 0.8
extending-time = 8.0
system_type = 1
damaging-speed = 800.00
blowout-speed = 900.00
lift_scalar = 0.3
drag_scalar = 0.5
pitch_scalar = 0
flaps-position.0 = 0.000, 0.000
flaps-position.1 = 0.000, 0.000
flaps-position.2 = 0.000, 0.000
flaps-position.3 = 0.000, 0.000
flaps-position.4 = 0.000, 0.000
flaps-position.5 = 10.000, 275.000
flaps-position.6 = 25.000, 250.000
[Flaps.3]
type= 2
span-outboard = 0.8
extending-time = 8.0
system_type = 1
damaging-speed = 800.00
blowout-speed = 900.00
lift_scalar = 0.3
drag_scalar = 0.5
pitch_scalar = 0
flaps-position.0 = 0.000, 0.000
flaps-position.1 = 0.000, 0.000
flaps-position.2 = 0.000, 0.000
flaps-position.3 = 0.000, 0.000
flaps-position.4 = 0.000, 0.000
flaps-position.5 = 15.000, 275.000
flaps-position.6 = 25.000, 250.000
[airplane_geometry]
wing_area = 1946.000
wing_span = 136.680
wing_root_chord = 24.600
wing_dihedral = -1.940
wing_incidence = 0.000
wing_twist = 0.000
oswald_efficiency_factor = 0.65
wing_winglets_flag = 0
wing_sweep = 15.000
wing_pos_apex_lon = 11.375
wing_pos_apex_vert = 0.000
htail_area = 350.000
htail_span = 44.840
htail_pos_lon = -37.720
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 42.500
vtail_area = 161.000
vtail_span = 15.890
vtail_sweep = 50.000
vtail_pos_lon = -33.560
vtail_pos_vert = 5.850
elevator_area = 150.000
aileron_area = 245.000
rudder_area = 81.000
elevator_up_limit = 12.000
elevator_down_limit = 10.000
aileron_up_limit = 5.000
aileron_down_limit = 5.000
rudder_limit = 10.000
elevator_trim_limit = 18.000
spoiler_limit = 70.000
aileron_to_spoileron_gain = 1.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 1
auto_spoiler_available=0
spoiler_extension_time=1.250000
positive_g_limit_flaps_up=9.000000
positive_g_limit_flaps_down=9.000000
negative_g_limit_flaps_up=-9.000000
negative_g_limit_flaps_down=-9.000000
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 500
engine_generator_map = 1,1,1,1
electric_always_available = 1
autopilot = 1, 25, 17
avionics_bus = 2, 85, 17
avionics = 1, 85, 17
pitot_heat = 2, 15, 17
additional_system = 2, 100, 17
marker_beacon = 1, 2, 17
gear_warning = 2, 2, 17
fuel_pump = 2, 25, 17
starter0 = 2, 100, 17
starter1 = 2, 100, 17
starter2 = 2, 100, 17
starter3 = 2, 100, 17
light_nav = 2, 5, 17
light_beacon = 2, 5, 17
light_landing = 2, 5, 17
light_taxi = 2, 5, 17
light_strobe = 2, 5, 17
light_panel = 2, 5, 17
auto_brakes = 2, 15, 17
standby_vacuum = 2, 15, 17
hydraulic_pump = 2, 2, 17
fuel_transfer_pump = 2, 5, 17
light_recognition = 2, 5, 17
light_wing = 2, 5, 17
light_logo = 2, 5, 17
[Auxiliary Power Unit]
available = 1
[exits]
number_of_exits = 3
exit.0 = 0.4, 36.6, -5.0, 3.0, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.1 = 0.4, -38.5, 4.5, -3.0, 1 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.2 = 0.4, 33.5, 3.5, -4.0, 2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
[Views]
eyepoint=63.0,-1.8,5.8
[Reference Speeds]
flaps_up_stall_speed = 142.0 //Knots True (KTAS)
full_flaps_stall_speed = 123.0 //Knots True (KTAS)
cruise_speed = 1000.00 //Knots True (KTAS)
max_mach = 4.50
max_indicated_speed = 2800.00 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=0.10
max_pitch_velocity_hi_alt=0.11
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=30,25,20,15,10
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
//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)
[contact_points]
point.0 = 1, 59.5, -1, -13, 5200, 0, 1.232, 40, 0.248, 2.5, 0.782, 8, 6, 0, 300, 350
point.1 = 1, 59.5, 1, -13, 5200, 0, 1.232, 40, 0.248, 2.5, 0.782, 8, 6, 0, 300, 350
point.2 = 1, -2.4, -5, -13.1, 5200, 1, 1.613, 0, 0.29, 2.5, 0.789, 9, 9, 2, 300, 350
point.3 = 1, -2.4, -8.5, -13.1, 5200, 1, 1.613, 0, 0.29, 2.5, 0.789, 9, 9, 2, 300, 350
point.4 = 1, -2.4, 5, -13.1, 5200, 2, 1.613, 0, 0.29, 2.5, 0.789, 9, 9, 3, 300, 350
point.5 = 1, -2.4, 8.5, -13.1, 5200, 2, 1.613, 0, 0.29, 2.5, 0.789, 9, 9, 3, 300, 350
point.6 = 2, -10.0, -12.2, -9.000, 5200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.7 = 2, -8.194, -71.078, -3.007, 5200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.8 = 2, -10.0, 12.200, -9.000, 5200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.9 = 2, -8.212, 71.190, -3.049, 5200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.10= 2, -51.56, 0.000, -4.174, 5200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.11= 2, 79.683, 0.000, -3.464, 5200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = 0
static_cg_height = 13
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 12
[keyboard_response]
elevator = 150.000000, 250.000000 //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
aileron = 150.000000, 150.000000 //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
rudder = 150.000000, 250.000000 //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
[forcefeedback]
gear_bump_nose_magnitude = 1000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 450
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 2000
crash_direction1 = 1000
crash_magnitude2 = 2000
crash_direction2 = 9000
crash_period2 = 7500
crash_duration2 = 2500000
stick_shaker_magnitude = 2000
stick_shaker_direction = 0
stick_shaker_period = 111111
[direction_indicators]
direction_indicator.0=3,0
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
differential_braking_scale = 1.3 //Delta on the amount of brake when the rudder pedals deflected
hydraulic_system_scalar = 1 //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure
auto_brakes = 4
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.01 //Percent throttle that activates warning
flap_limit_idle = 25.00 //Flap angle that activates warning at idle
flap_limit_power = 30.00 //Flap angle that activates warning at above idle
[hydraulic_system]
electric_pumps=1
engine_map=1,1,1,1
normal_pressure=3000.000000
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_dsb_heat
touchdown=fx_tchdwn_s, 1
windshield_rain_effect_available = 1
[stall_warning]
type=1
stick_shaker=2
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[VoiceAlerts]
LowFuelPct = 0.1, -1, 60 //Low Fuel limit (percent), Check BELOW, Check every 60 seconds
OverGLimit = 6.0, 1, 1 //High G limit, Check ABOVE, Check every 1 seconds
[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
[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
[GPWS]
max_warning_height = 1000
sink_rate_fpm = -1500
excessive_sink_rate_fpm = -2000
climbout_sink_rate_fpm = -100
flap_and_gear_sink_rate_fpm= -100
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[launch_assistance]
launch_bar_pivot = 0.90, 0.00, -0.09
launch_bar_lug = 0.90, 0.00, -4.09
[Pressurization]
design_cabin_pressure = 10.9 ;PSI (~8000 feet)
max_pressure_differential = 4.96 ;PSI
[pneumatic_system]
max_pressure = 18.000000
bleed_air_scalar = 1.000000
[deice_system]
structural_deice_type = 1