[fltsim.0]
title=BH1118
sim=BH1118
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=CONVAIR
ui_type=B-58 HUSTLER STRATEGIC BOMBER
ui_variation=
atc_heavy=0
atc_id=BH1118
atc_airline=Air Force
atc_flight_number=
description=FS2002\/2004 FSDSV2 CONVAIR B-58 HUSTLER The B-58 was first flown on November 11, 1956, and was the world's first supersonic bomber. She was nicknamed the Hustler because she was fast and beautiful. On December 15, 1959, a B-58 was flown 1,680 miles in 80 minutes. (That's 21 miles per minute!)\nModel\nBy JRLucariny\nhttp:\/\/lucariny.sites.uol.com.br

[lights]
light.0= 4,  21.50, 0.00, 2.20, fx_vclight

light.11= 6, -33.8,  -21.6,  -1.1, fx_bob_burn_Blue
light.12= 6, -37.3,  -21.6,  -1.80, fx_F14_Burnerflame,
light.13= 7, -33.8,   21.6,  -1.1, fx_bob_burn_Blue
light.14= 7, -37.3,   21.6,  -1.80, fx_F14_Burnerflame,

light.15= 6, -11.2, -12.7,  -2.8, fx_bob_burn_Blue
light.16= 6, -15.3, -12.7,  -3.2, fx_F14_Burnerflame,
light.17= 7, -11.2,  12.3,  -2.8, fx_bob_burn_Blue
light.18= 7, -15.3,  12.3,  -3.2, fx_F14_Burnerflame,

[SmokeSystem]
Smoke.0= -37.0, -21.6, -1.80, fx_smoke_f6
Smoke.1= -37.0,  21.6, -1.80, fx_smoke_f6
Smoke.2= -14.0, -12.7, -3.20, fx_smoke_f6
Smoke.3= -14.0,  12.7, -3.20, fx_smoke_f6
Smoke.4= -37.0, -21.6, -1.80, fx_smoke_f6
Smoke.5= -37.0,  21.6, -1.80, fx_smoke_f6
Smoke.6= -14.0, -12.7, -3.20, fx_smoke_f6
Smoke.7= -14.0,  12.7, -3.20, fx_smoke_f6

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[General]
performance=CREW:  3\nDIMENSIONS:\nLength 96.75 ft (29.49 m)\nWingspan 56.83 ft (17.32 m)\nHeight 31.42 ft (9.58 m)\nWing Area 1,542 ft2 (143.25 m2)\nWEIGHTS:\nEmpty 55,560 lb (25,200 kg)\nMax Takeoff 163,000 lb (73,935 kg)\nPROPULSION:\nPowerplant  four General Electric J-79 afterburning turbojets\nThrust 42,000 lb (186.83 kN) 64,000 lb (284.70 kN) with afterburner\nPERFORMANCE:\nMax Level Speed at altitude: 1,385 mph (2,230 km\/h) at 40,000 ft (12,190 m), Mach 2.1\nService Ceiling 60,000 ft (18,290 m)\nRange 1,735 nm (3,220 km) 4,845 nm (8,975 km) with in-flight refueling\nARMAMENT:\nGun one 20-mm T-171E3 Vulcan rotary cannon in a radar-aimed tail barbette\nStations one external hardpoint for a disposable centerline pod\nAir-to-Air Missile none\nAir-to-Surface Missile none\nBomb various nuclear bombs
atc_type=Convair
atc_model=B58
Category=airplane

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.00, 0.00, 0.00
empty_weight_CG_position= -8.00, 0.00, 0.00
max_number_of_stations=10
station_load.0=0.00, 0.00, 0.00, 0.00
empty_weight= 55560.00
empty_weight_roll_MOI=   285950.00
empty_weight_pitch_MOI=  181905.00
empty_weight_yaw_MOI=    285200.00
empty_weight_coupled_MOI= 0.00
max_gross_weight= 163000.00
//CG_forward_limit= 0.00
//CG_aft_limit= 1.00

[fuel]
Center1=    0.00,  0.00, 0.00, 3600.00, 0.00
LeftMain= -10.00,  0.00, 0.00, 2200.00, 0.00
LeftAux=  -15.00,-22.667,0.00, 1400.00, 0.00
RightMain=-10.00,  0.00, 0.00, 2200.00, 0.00
RightAux= -15.00, 22.667,0.00, 1400.00, 0.00
fuel_type=2
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area= 1338.00
wing_span= 56.833
wing_root_chord= 47.083
wing_dihedral= -3.0
wing_incidence= 0.00
wing_twist= 0.00
oswald_efficiency_factor= 0.834
wing_winglets_flag= 0
wing_sweep= 60.00
wing_pos_apex_lon= 9.00
wing_pos_apex_vert= 1.00
htail_area= 0.00
htail_span= 0.00
htail_pos_lon= 0.00
htail_pos_vert= 0.00
htail_incidence= 0.00
htail_sweep= 0.00
vtail_area= 210.00
vtail_span= 15.00
vtail_sweep= 45.00
vtail_pos_lon= -29.00
vtail_pos_vert= 6.00
elevator_area= 75.00
aileron_area= 75.00
rudder_area= 34.00
elevator_up_limit= 27.502
elevator_down_limit= 20.626
aileron_up_limit= 19.481
aileron_down_limit= 14.897
rudder_limit= 23.491
elevator_trim_limit= 19.481
spoiler_limit= 59.989
spoilerons_available= 0
aileron_to_spoileron_gain= 0.00
min_ailerons_for_spoilerons= 0.00
min_flaps_for_spoilerons= 0.00
auto_spoiler_available=0
spoiler_extension_time=1.000000
positive_g_limit_flaps_up=9.341880
positive_g_limit_flaps_down=0.000000
negative_g_limit_flaps_up=-6.205128
negative_g_limit_flaps_down=0.000000

[contact_points]
point.0= 1, 26.0, -0.50, -10.0, 1574.80, 0.00, 1.00, 51.96, 0.40, 2.50, 0.85, 5.00, 5.00, 0.00, 0.00, 0.00
point.1= 1, 26.0, 0.50, -10.0, 1574.80, 0.00, 1.00, 51.96, 0.40, 2.50, 0.85, 5.00, 5.00, 0.00, 0.00, 0.00

point.2= 1, -14.60, -8.10, -9.80, 2755.90, 1.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 2.00, 0.00, 0.00
point.3= 1, -14.60, -7.20, -9.80, 2755.90, 1.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 2.00, 0.00, 0.00
point.4= 1, -14.60, -6.10, -9.80, 2755.90, 1.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 2.00, 0.00, 0.00
point.5= 1, -14.60, -5.20, -9.80, 2755.90, 1.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 2.00, 0.00, 0.00
point.6= 1, -12.20, -8.10, -9.80, 2755.90, 1.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 2.00, 0.00, 0.00
point.7= 1, -12.20, -7.20, -9.80, 2755.90, 1.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 2.00, 0.00, 0.00
point.8= 1, -12.20, -6.10, -9.80, 2755.90, 1.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 2.00, 0.00, 0.00
point.9= 1, -12.20, -5.20, -9.80, 2755.90, 1.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 2.00, 0.00, 0.00

point.10= 1, -14.60, 8.10, -9.80, 2755.90, 2.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 3.00, 0.00, 0.00
point.11= 1, -14.60, 7.20, -9.80, 2755.90, 2.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 3.00, 0.00, 0.00
point.12= 1, -14.60, 6.10, -9.80, 2755.90, 2.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 3.00, 0.00, 0.00
point.13= 1, -14.60, 5.20, -9.80, 2755.90, 2.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 3.00, 0.00, 0.00
point.14= 1, -12.20, 8.10, -9.80, 2755.90, 2.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 3.00, 0.00, 0.00
point.15= 1, -12.20, 7.20, -9.80, 2755.90, 2.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 3.00, 0.00, 0.00
point.16= 1, -12.20, 6.10, -9.80, 2755.90, 2.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 3.00, 0.00, 0.00
point.17= 1, -12.20, 5.20, -9.80, 2755.90, 2.00, 1.60, 0.00, 0.40, 2.50, 0.51, 5.00, 5.00, 3.00, 0.00, 0.00

point.18= 2, -33.0, -28.30, 0.10, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00
point.19= 2, -33.0, 28.30, 0.10, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00
point.20= 2, -52.70, 0.00, 4.50, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00
point.21= 2, 40.50, 0.00, -1.60, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00
point.22= 2, 3.50, -12.30, -5.50, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00
point.23= 2, 3.50, 12.30, -5.50, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00
static_pitch= -1.00
static_cg_height= 10.00
gear_system_type=0

[GeneralEngineData]
engine_type= 1
Engine.0= -33.80, -21.60, -1.10
Engine.1= -11.20, -12.70, -2.80
Engine.2=  11.20,  12.70, -2.80
Engine.3= -33.80,  21.60, -1.10
fuel_flow_scalar= 1.0
min_throttle_limit=0.00

[TurbineEngineData]
fuel_flow_gain= 0.90
inlet_area= 21.70
rated_N2_rpm= 29920.00
static_thrust= 16000.00
afterburner_available= 2
reverser_available= 0
afterburner_throttle_threshold = 0.90

[Reference Speeds]
flaps_up_stall_speed= 120.00
full_flaps_stall_speed=120.00
cruise_speed= 532.00		//knots over the ground at 40,000 feet.(293 indicated)
max_indicated_speed=1610.00
max_mach=2.50
max_level_speed= mach 2.10	//at 40,000 feet.


[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=70,130
aileron=70,130
rudder=70,130

[Views]
eyepoint=21.20, -0.50, 2.20

[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

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.00
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=125.00
pitch_takeoff_ga=8.00
max_pitch=10.00
max_pitch_acceleration=1.00
max_pitch_velocity_lo_alt=2.00
max_pitch_velocity_hi_alt=1.500
max_pitch_velocity_lo_alt_breakpoint=20000.00
max_pitch_velocity_hi_alt_breakpoint=28000.00
max_bank=25.00
max_bank_acceleration=1.80
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.90

[direction_indicators]
direction_indicator.0=3,0

[jet_engine]
thrust_scalar=1.00

[flight_tuning]
cruise_lift_scalar=1.00
pitch_stability=1.00
roll_stability=1.00
yaw_stability=1.00
parasite_drag_scalar=1.00
induced_drag_scalar=1.00
elevator_effectiveness=1.00
aileron_effectiveness=1.00
rudder_effectiveness=1.00
elevator_trim_effectiveness=1.00
aileron_trim_effectiveness=1.00
rudder_trim_effectiveness=1.00


[brakes]
toe_brakes_scale=1.237098
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.00
flap_limit_power=0.00
flap_limit_idle=0.00

[hydraulic_system]
normal_pressure=0.00

[stall_warning]
type=1
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[Flaps.0]
type=1
span-outboard=0.50
extending-time=0.00
system_type=0

[pitot_static]
pitot_heat=1.00

[vacuum_system]
max_pressure=5.00
vacuum_type=1
electric_backup_pressure=0.00
engine_map=1,1,1,1

[pneumatic_system]
max_pressure=0.00
bleed_air_scalar=0.00

[deice_system]
structural_deice_type=0