[fltsim.0]
title=AI B-52D
sim=b-52_1
model=1
panel=
sound=
texture=1
kb_checklists=
kb_reference=
atc_id=1
atc_airline=Air Force
atc_flight_number=1
atc_heavy=1
atc_parking_types=MIL_COMBAT
ui_manufacturer=Boeing
ui_type=AI B-52
ui_variation=1
description=¥
atc_parking_codes=M002,B52
[fltsim.1]
title=AI B-52D Camouflge
sim=b-52_1
model=2
panel=
sound=
texture=2
kb_checklists=
kb_reference=
atc_id=2
atc_airline=Air Force
atc_flight_number=2
atc_heavy=1
atc_parking_types=MIL_COMBAT
ui_manufacturer=Boeing
ui_type=AI B-52
ui_variation=2
description=¥
atc_parking_codes=M002,B52
[fltsim.2]
title=AI B-52G Camouflge-1
sim=b-52_1
model=3
panel=
sound=
texture=3
kb_checklists=
kb_reference=
atc_id=3
atc_airline=Air Force
atc_flight_number=3
atc_heavy=1
atc_parking_types=MIL_COMBAT
ui_manufacturer=Boeing
ui_type=AI B-52
ui_variation=3
description=¥
atc_parking_codes=M002,B52
[fltsim.3]
title=AI B-52G Camouflge-2
sim=b-52_1
model=4
panel=
sound=
texture=4
kb_checklists=
kb_reference=
atc_id=4
atc_airline=Air Force
atc_flight_number=4
atc_heavy=1
atc_parking_types=MIL_COMBAT
ui_manufacturer=Boeing
ui_type=AI B-52
ui_variation=4
description=¥
atc_parking_codes=M002,B52
[fltsim.4]
title=AI B-52G Strakelet
sim=b-52_1
model=5
panel=
sound=
texture=5
kb_checklists=
kb_reference=
atc_id=5
atc_airline=Air Force
atc_flight_number=5
atc_heavy=1
atc_parking_types=MIL_COMBAT
ui_manufacturer=Boeing
ui_type=AI B-52
ui_variation=5
description=¥
atc_parking_codes=M002,B52
[General]
atc_type=BOEING AIRCRAFT
atc_model=B52
editable=1
performance=¥\t\t¥\n¥\t¥\n¥\t¥\n¥\t¥
[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
electric_pump=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 = -4.500
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
max_indicated_speed=497.671875
max_mach=0.919971
[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
min_throttle_limit=-0.250000
[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]
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;
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
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
[contact_points]
point.0=1, -27.42, 0.00, -15.60, 1181.1, 0, 4.521, 90.0, 1.63, 2.5, 0.7235, 4.0, 4.0, 0, 0.0, 0.0
point.1=1, -119.50, -19.00, -16.20, 1574.8, 1, 4.521, 0.0, 1.91, 2.5, 0.5470, 6.9, 6.9, 2, 0.0, 0.0
point.2=1, -119.50, 19.00, -16.20, 1574.8, 2, 4.521, 0.0, 1.91, 2.5, 0.5470, 7.1, 7.1, 3, 0.0, 0.0
point.3=2, -114.17, -47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -114.17, 47.33, 0.00, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -83.33, 0.00, 2.50, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.0, 0.00, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
static_pitch = 0.0
static_cg_height = 15.0
//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)
max_number_of_points=21
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.1=2, -109.00, -0.00, -9.80, fx_beaconb ,
light.2=4, -19.60, 0.00, 2.65, fx_vclighth ,
light.3 =7, -115.0, -56.0, -4.0, fx_smoke_b52
light.4 =7, -115.0, -62.0, -4.0, fx_smoke_b52
light.5 =7, -105.0, -30.0, -4.0, fx_smoke_b52
light.6 =7, -105.0, -35.0, -4.0, fx_smoke_b52
light.7 =7, -105.0, 32.0, -4.0, fx_smoke_b52
light.8 =7, -105.0, 38.0, -4.0, fx_smoke_b52
light.9 =7, -115.0, 58.0, -4.0, fx_smoke_b52
light.10 =7, -115.0, 64.0, -4.0, fx_smoke_b52
[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
[brakes]
toe_brakes_scale=1.241798
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[tailhook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=1.0