; Localized 07/07/2003 12:46 ßã (GMT) 4:4.2.169 aircraft.cfg [fltsim.0] title=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=B-52 ui_variation=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, 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-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=B-52 ui_variation=2 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.2] title=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=B-52 ui_variation=3 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.3] title=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=B-52 ui_variation=4 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.4] title=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=B-52 ui_variation=5 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 Military Airplane Co atc_model=B52 editable=1 performance= Military Airplane Co\nLength: 159 ft\nLength: 159 ft\nHeight: 40 ft\nHeight: 40 ft\nWingspan: 185 feet\nSpeed: 650 mph\nCeiling: 50,000 feet\n [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 = 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 = -4.000 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 = 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 = 42750.000 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 //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 = 1.000, -25.000, 0.000, -15.80, 2000.000, 0.000, 2.000, 40.000, 2.500, 1.500, 0.900, 9.000, 8.000, 0.000, 220.000, 2029.000 point.1 = 1.000, -114.000, -17.500, -16.5, 2000.000, 1.000, 2.500, 0.000, 2.000, 2.500, 0.900, 11.000, 9.000, 2.000, 220.000, 2029.958 point.2 = 1.000, -114.000, 17.500, -16.5, 2000.000, 2.000, 2.500, 0.000, 2.000, 2.500, 0.900, 11.000, 9.000, 3.000, 220.000, 2029.958 point.3 = 2.000, -70.600, 0.000, 0.500, 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.4 = 2.000, -21.600, 79.500, 0.500, 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.5 = 2.000, -21.600, -79.500, 0.500, 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.6 = 2.000, 70.000, 0.000, 0.500, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 static_pitch= 0.000 static_cg_height= 15.000 gear_system_type=1 max_number_of_points=21 [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, -113.00, -0.00, -9.80, fx_beaconb , light.2 =4, -19.60, 0.00, 2.65, fx_vclighth , light.3 =2, -115.0, -56.0, -4.0, fx_smoke_b52 light.4 =2, -115.0, -62.0, -4.0, fx_smoke_b52 light.5 =2, -105.0, -30.0, -4.0, fx_smoke_b52 light.6 =2, -105.0, -35.0, -4.0, fx_smoke_b52 light.7 =2, -105.0, 32.0, -4.0, fx_smoke_b52 light.8 =2, -105.0, 38.0, -4.0, fx_smoke_b52 light.9 =2, -115.0, 58.0, -4.0, fx_smoke_b52 light.10 =2, -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= 1 span-outboard= 0.800 extending-time= 20.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 1.000 drag_scalar= 1.000 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= 1.000 drag_scalar= 1.000 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 [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