 ; Localized	07/07/2003 12:46 ŒßŒã (GMT)	4:4.2.169 	aircraft.cfg


[fltsim.0]
title=AI B-52H Camouflge
sim=b-52_1
model=1
panel=
sound=
texture=1
kb_checklists=
kb_reference=
atc_id=6
atc_airline=Air Force
atc_flight_number=6
atc_heavy=1
atc_parking_types=MIL_COMBAT
ui_manufacturer=Boeing
ui_type=AI B-52 
ui_variation=06 B-52H Camouflge
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, of which 170 were -Ds. The -Ds were modified to carry conventional bombs and Quail decoy missiles. 
atc_parking_codes=M002,B52

[fltsim.1]
title=AI B-52H 
sim=b-52_1
model=2
panel=
sound=
texture=2
kb_checklists=
kb_reference=
atc_id=7
atc_airline=Air Force
atc_flight_number=7
atc_heavy=1
atc_parking_types=MIL_COMBAT
ui_manufacturer=Boeing
ui_type=AI B-52 
ui_variation=07 B-52H  
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, of which 170 were -Ds. The -Ds were modified to carry conventional bombs and Quail decoy missiles. 
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 =40000.000000, -80.000000, 0.000000, 0.000000, Station 1

;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      = 1.000

[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= 1.000, -27.420, 0.000, -15.600, 1181.100, 0.000, 4.521, 90.000, 1.630, 2.200, 0.724, 4.000, 15.000, 0.000, 0.000, 0.000
point.1= 1.000, -119.500, -19.000, -16.000, 1574.800, 1.000, 4.521, 0.000, 1.890, 2.200, 0.547, 6.900, 15.000, 2.000, 0.000, 0.000
point.2= 1.000, -119.500, 19.000, -16.000, 1574.800, 2.000, 4.521, 0.000, 1.890, 2.200, 0.547, 7.100, 15.000, 3.000, 0.000, 0.000
point.3= 2.000, -114.170, -47.330, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -114.170, 47.330, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -83.330, 0.000, 2.500, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = 0.000
static_cg_height = 15.000


        //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  =7,  -115.0, -56.0,  -4.0, fx_smoke_b52h   
light.3  =7,  -115.0, -62.0,  -4.0, fx_smoke_b52h   
light.4  =7,  -105.0, -30.0,  -4.0, fx_smoke_b52h
light.5  =7,  -105.0, -35.0,  -4.0, fx_smoke_b52h
light.6  =7,  -105.0,  32.0,  -4.0, fx_smoke_b52h   
light.7  =7,  -105.0,  38.0,  -4.0, fx_smoke_b52h   
light.8  =7,  -115.0,  58.0,  -4.0, fx_smoke_b52h 
light.9  =7,  -115.0,  64.0,  -4.0, fx_smoke_b52h 



[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



[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
[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
