[fltsim.0]
title=Boeing B-52H 60-042
sim=b52h
model=
panel=
sound=
texture=
kb_checklists=B-52h_check
kb_reference=B-52h_ref
atc_id=60042
atc_airline=Air Force
atc_flight_number=42
atc_heavy=1
atc_parking_types=CARGO
ui_manufacturer=Boeing
ui_type=B-52H
ui_variation=U.S. Air Force
description=High altitude, long range strategic bomber,\nstationed at Barksdale AFB, Louisiana (KBAD).\n
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
[fltsim.1]
title=Boeing B-52H 60-047
sim=b52h
model=
panel=
sound=
texture=60-047
kb_checklists=B-52h_check
kb_reference=B-52h_ref
atc_id=60047
atc_airline=Air Force
atc_flight_number=47
atc_heavy=1
atc_parking_types=CARGO
ui_manufacturer=Boeing
ui_type=B-52H
ui_variation=U.S. Air Force 60-047
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
visual_damage=1
description=Since it became operational in 1955, the B-52 has been the main long-range heavy bomber of the Strategic Air Command. It first flew on Apr. 15, 1952. Nearly 750 B-52s were built when production ended in Oct. 1963. Textures by Bill Baldwin. This model is stationed at\nBarksdale AFB, Louisiana (KBAD).\n
[General]
atc_type=BOEING
atc_model=B52
editable=1
performance=Engines: 8Ч Pratt & Whitney TF33-P-3/103 turbofans, 17,000 lbf ea\nLength: 159 ft 4 in\nHeight: 40 ft 8 in\nWingspan: 185 ft 0 in\nWing area: 4,000 ftІ\nEmpty weight: 185,000 lb\nMax empty fuel weight: 265,000 lb\nMax takeoff weight: 488,000 lb\nFuel capacity: 33,284 US gal\nMaximum speed: mach .95\nService ceiling 50,000 ft\nNormal Range:\n8,000 nm @ FL420W, mach .88\n8,200 nm @ FL410, mach .88\nNormal Cruise: FL410E/FL420W @ mach .88\nArmament: Approximately 78,900 pounds mixed ordnance\nCrew: 5 (pilot, copilot, radar navigator/bombardier, navigator, and Electronic Warfare Officer)\nOriginal aircraft designer: Mike Stone\nEureka, Missouri\[email protected]\nCorrected flight dynamics and data by:\nDouglas E. Trapp\nFS Flight Dynamics Engineer\nArlington, Texas\[email protected]\nOctober 2008\n
Category=airplane
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000
[weight_and_balance]
// ACM V2.5
max_gross_weight = 488000.000
empty_weight = 185000.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
empty_weight_pitch_MOI = 16000000.000
empty_weight_roll_MOI = 3800000.000
empty_weight_yaw_MOI = 12000000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit = 0.000
CG_aft_limit = 1.000
max_number_of_stations = 15
//Payload= 80,000 lbs
station_load.0 = 220.0, 70.0, 2.0, 16.0
station_load.1 = 220.0, 70.0, -2.0, 16.0
station_load.2 = 220.0, 65.0, 2.0, 16.5
station_load.3 = 220.0, 65.0, -2.0, 16.5
station_load.4 = 220.0, 60.0, 0.0, 16.5
station_load.5 = 78900.0, 0.0, 0.0, -14.0
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -36.36, -92.76, -0.44, fx_navredh ,
light.1 = 3, -36.36, 92.76, -0.44, fx_navgreh ,
light.2 = 3, -90.69, 0.00, 3.81, fx_navwhih ,
light.3 = 2, -36.46, -92.76, -0.44, fx_strobeh ,
light.4 = 2, -36.46, 92.76, -0.44, fx_strobeh ,
light.5 = 4, 59.22, 0.00, 6.08, fx_vclighth,
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 1
electric_pump = 0
//33,284 US Gal = 223,003 lb
LeftMain = 16.450, -20.870, -4.000, 16642.000, 0.000
RightMain = 16.450, 20.870, -4.000, 16642.000, 0.000
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 0.700
min_throttle_limit = -0.25
engine.0 = -9.250, -58.670, -1.620
engine.1 = 10.580, -33.070, -0.130
engine.2 = 10.580, 33.070, -0.130
engine.3 = -9.250, 58.670, -1.620
[SMOKESYSTEM]
smoke.0= -19.250, -58.670, -1.620, fx_smoke_f6
smoke.1= 20.580, -33.070, -0.130, fx_smoke_f6
smoke.2= 20.580, 33.070, -0.130, fx_smoke_f6
smoke.3= -19.250, 58.670, -1.620, fx_smoke_f6
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
windshield_rain_effect_available = 1
[contact_points]
static_pitch = 0.000
static_cg_height = 10.000
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 9
point.0 = 1.000, 29.000, 0.000, -10.800, 2000.000, 0.000, 2.000, 40.000, 0.500, 3.000, 0.700, 10.000, 10.000, 0.000, 220.000, 250.000
point.1 = 1.000, -28.000, -5.000, -10.600, 2000.000, 1.000, 2.000, 0.000, 0.500, 3.000, 0.700, 10.000, 10.000, 2.000, 220.000, 250.000
point.2 = 1.000, -28.000, 5.000, -10.600, 2000.000, 2.000, 2.000, 0.000, 0.500, 3.000, 0.700, 10.000, 10.000, 3.000, 220.000, 250.000
point.3 = 1.000, -34.000, -77.500, -10.000, 2000.000, 0.000, 2.000, 0.000, 0.500, 4.000, 0.700, 6.000, 6.000, 1.000, 220.000, 250.000
point.4 = 1.000, -34.000, 77.500, -10.000, 2000.000, 0.000, 2.000, 0.000, 0.500, 4.000, 0.700, 6.000, 6.000, 1.000, 220.000, 250.000
point.5 = 2.000, -41.867, -92.674, -0.885, 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.6 = 2.000, -41.035, 92.674, -0.885, 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.7 = 2.000, -89.691, 0.000, 0.556, 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.8 = 2.000, 68.422, 0.000, 0.114, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[airplane_geometry]
//ACM_AREAW1// 0,0,0,10.7292,3.1284,3.1284,2.4005,12.5935,6.2571,6.2571
//ACM_AREAW2// 4.8010,14.0347,9.3856,9.3856,7.2017,15.8989,12.5142,12.5142,9.6022,17.5093
//ACM_AREAW3// 15.7271,15.7271,12.0031,19.2889,18.7712,18.7712,14.4034,20.6455,21.8999,21.8999
//ACM_AREAW4// 16.8043,22.2558,25.0284,25.0284,19.2049,23.9507,28.1569,28.1569,21.6056,25.5613
//ACM_AREAH1// 0,0,0,8.6089,0.8848,0.8848,0.7968,8.6324,1.6850,1.6850
//ACM_AREAH2// 1.5089,8.5719,2.5703,2.5703,2.3905,8.6801,3.5399,3.5399,3.1874,8.7040
//ACM_AREAH3// 4.3403,4.3403,3.9842,8.8126,5.3098,5.3098,4.7810,8.7517,6.1949,6.1949
//ACM_AREAH4// 5.5777,8.9448,7.0798,7.0798,6.3748,8.9686,7.9649,7.9649,7.1715,8.9924
//ACM_AREAV1// 0,0,0,8.0906,0.7860,0.7860,0.7077,8.0633,1.5721,1.5721
//ACM_AREAV2// 1.4155,8.1204,2.3585,2.3585,2.1236,8.3466,3.2293,3.2293,2.8315,8.5733
//ACM_AREAV3// 3.9307,3.9307,3.5392,8.7152,4.7170,4.7170,4.2472,8.9413,5.5032,5.5032
//ACM_AREAV4// 4.9551,8.9988,6.2894,6.2894,5.6630,9.1407,7.0756,7.0756,6.3709,9.2825
//ACM_CAREAW1// 14.0783,14.0783,16.1674,18.3134,15.6428,15.6428,17.3677,19.4064,17.2070,17.2070
//ACM_CAREAW2// 18.5680,20.4993,18.7712,18.7712,19.7684,21.5923,20.3355,20.3355,20.9687,22.6854
//ACM_CAREAW3// 21.8999,21.8999,22.1690,23.7784,23.4640,23.4640,23.3694,24.8715,25.0284,25.0284
//ACM_CAREAW4// 24.5697,25.9645,26.5928,26.5928,25.7700,27.0575,28.1569,28.1569,26.4626,28.1506
//ACM_CAREAH1// 0.0842,0.0842,7.5611,8.5242,0.8848,0.8848,7.7656,8.4271,1.7697,1.7697
//ACM_CAREAH2// 7.8859,8.5837,2.7395,2.7395,7.8369,8.5710,3.5399,3.5399,7.9569,8.7276
//ACM_CAREAH3// 4.4249,4.4249,7.8234,8.7150,5.3944,5.3944,8.0282,8.8716,6.1949,6.1949
//ACM_CAREAH4// 8.2327,8.8590,7.0798,7.0798,8.2684,8.9308,8.0495,8.0495,8.5578,9.1721
//ACM_CAREAV1// 0.0842,0.0842,7.1824,8.1827,0.7013,0.7013,7.3829,8.1843,1.5721,1.5721
//ACM_CAREAV2// 7.4140,8.4399,2.2739,2.2739,7.5296,8.1884,3.1447,3.1447,7.7301,8.5284
//ACM_CAREAV3// 3.8461,3.8461,7.9305,8.6152,4.7170,4.7170,8.0459,8.5325,5.5032,5.5032
//ACM_CAREAV4// 8.2466,8.7033,6.3740,6.3740,8.3624,8.7054,7.0756,7.0756,8.6471,9.1302
wing_area = 4000.000
wing_span = 185.000
wing_root_chord = 35.200
wing_dihedral = -4.000
wing_incidence = 2.000
wing_twist = -1.000
oswald_efficiency_factor = 0.500
wing_winglets_flag = 0
wing_sweep = 37.500
wing_pos_apex_lon = 49.000
wing_pos_apex_vert = 5.550
htail_area = 1200.000
htail_span = 52.250
htail_pos_lon = -60.000
htail_pos_vert = 0.000
htail_incidence = 0.000
htail_sweep = 42.000
vtail_area = 414.000
vtail_span = 23.200
vtail_sweep = 42.000
vtail_pos_lon = -51.400
vtail_pos_vert = 6.930
elevator_area = 127.000
aileron_area = 160.000
rudder_area = 50.000
elevator_up_limit = 30.000
elevator_down_limit = 25.000
aileron_up_limit = 25.000
aileron_down_limit = 5.000
rudder_limit = 30.000
elevator_trim_limit = 5.000
spoiler_limit = 60.000
aileron_to_spoileron_gain = 3.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.001
min_flaps_for_spoilerons = 0.000
spoilerons_available = 1
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1,1,1,1
electric_always_available = 0
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
[Reference Speeds]
flaps_up_stall_speed= 140.000
full_flaps_stall_speed= 110.000
cruise_speed= 350.000
max_mach = 0.96
max_indicated_speed = 350.0 //Red line (KIAS)
[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
[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 47.166
bypass_ratio=2.8
rated_N2_rpm= 29920.000
static_thrust= 34000.000
afterburner_available= 0
reverser_available= 1.000
[jet_engine]
thrust_scalar=1.000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=2000.0
autothrottle_available=1
autothrottle_arming_required = 1
autothrottle_max_rpm = 100
autothrottle_takeoff_ga = 1
pitch_takeoff_ga=8 ;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=16.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control = 18.0
gs_integrator_control = 0.33
gs_derivative_control = 0.00
gs_integrator_boundary = 0.70
gs_derivative_boundary = 0.00
yaw_damper_gain = 1.0
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 5.0 //Flap angle that activates warning at idle
flap_limit_power = 25.5 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.24 //Brake scalar
auto_brakes=4
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,1,1 //pumps on Eng1,2,3,4
[Views]
eyepoint=58.32, -1.72, 5.08 ; Longitude, Latitude and Vertical position from Reference Point, (FEET)
[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
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[exits]
number_of_exits = 2
exit_rate.0 = 2.0 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[stall_warning]
type=2
stick_shaker=1
[tailhook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=1.0
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 25 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 1 // degrees
flaps-position.2 = 5 // degrees
flaps-position.3 = 10 // degrees
flaps-position.4 = 20 // degrees
flaps-position.5 = 25 // degrees
flaps-position.6 = 30 // degrees
damaging-speed = 310 // KIAS
blowout-speed = 350 // KIAS
lift_scalar = 0.7
drag_scalar = 0.9
pitch_scalar= 0.9
system_type = 1 //Hydraulic
[flaps.1]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 2 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 1.0 // degrees
damaging-speed = 310 // KIAS
blowout-speed = 350 // KIAS
lift_scalar = 0.3
drag_scalar = 0.1
pitch_scalar= 0.1
system_type = 1 //Hydraulic
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=1