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

[fltsim.0]
title=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=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=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=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= 600000.000
empty_weight= 74170.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 0.000, 0.000, 0.000

max_number_of_stations =50

station_load.0 =130000.000000, 0.000000, 0.000000, 0.000000, Station 1

;Moments of Inertia
empty_weight_pitch_MOI  = 18000000.000
empty_weight_roll_MOI   = 5500000.000
empty_weight_yaw_MOI    = 16300000.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[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              = -4.000
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        = 30.000
aileron_down_limit      = 20.000
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     =0.90
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


[fuel]
Center1 = 0.000, 0.000, -7.000, 19545.000, 3.000
Center2 = 0.000, 0.000, 6.000, 3300.000, 0.000
LeftMain = 0.000, -35.000, -4.000, 16720.000, 3.000
LeftAux = -8.000, -52.000, -3.000, 500.000, 0.000
RightMain = 0.000, 35.000, -4.000, 16720.000, 3.000
RightAux = -8.000, 52.000, -3.000, 500.000, 0.000
fuel_type = 2.000000
number_of_tank_selectors=1
electric_pump = 1

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1500.0
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


[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              = 40.000
rated_N2_rpm            = 29920.000
static_thrust           = 57275.000
afterburner_available   = 0
reverser_available      = 1.000


[jet_engine]
thrust_scalar =1.000


[Views]
eyepoint = 90.0, -2.65, 2.25


[contact_points]

        //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)

point.0=1,  87.42,   0.00, -15.80, 1181.1, 0, 3.500, 40.0, 1.7, 2.5, 0.7200, 15.0, 15.0, 0, 0.0, 0.0
point.1=1, -19.50, -32.00, -16.10, 1574.8, 1, 4.167, 20.0, 2.3, 2.5, 0.7500, 15.0, 15.0, 2, 0.0, 0.0
point.2=1, -19.50,  32.00, -16.10, 1574.8, 2, 4.167, 20.0, 2.3, 2.5, 0.7500, 15.0, 15.0, 3, 0.0, 0.0
point.3=2, -14.17, -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, -14.17,  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 = 0.000
static_cg_height = 15.000
gear_system_type=0


[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


[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


[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI


[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second


[TailHook]
tailhook_length=1                             ;(feet)
tailhook_position=-15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0


[folding_wings]
wing_fold_system_type=4                       ;0=None
fold_rates=0.075,0.075	                          ;Percent per second


[LIGHTS]
;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.1  =2,  -33.00,   -0.00,  -9.80, fx_beaconb ,
light.2  =2,  -35.0, -56.0,  -4.0, fx_smoke_b52h   
light.3  =2,  -35.0, -62.0,  -4.0, fx_smoke_b52h   
light.4  =2,  -25.0, -30.0,  -4.0, fx_smoke_b52h
light.5  =2,  -25.0, -35.0,  -4.0, fx_smoke_b52h
light.6  =2,  -25.0,  32.0,  -4.0, fx_smoke_b52h   
light.7  =2,  -25.0,  38.0,  -4.0, fx_smoke_b52h   
light.8  =2,  -35.0,  58.0,  -4.0, fx_smoke_b52h 
light.9  =2,  -35.0,  64.0,  -4.0, fx_smoke_b52h 


[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


[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


[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1


[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



[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=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 20.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.850
drag_scalar= 0.850
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 2.000, 0.000
flaps-position.3= 5.000, 0.000
flaps-position.4= 10.000, 0.000
flaps-position.5= 15.000, 0.000
flaps-position.6= 25.000, 0.000
flaps-position.7= 30.000, 0.000
flaps-position.8= 40.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.800
extending-time= 20.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.00
drag_scalar= 1.00
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 2.000, 0.000
flaps-position.3= 5.000, 0.000
flaps-position.4= 10.000, 0.000
flaps-position.5= 15.000, 0.000
flaps-position.6= 25.000, 0.000
flaps-position.7= 30.000, 0.000
flaps-position.8= 40.000, 0.000
