[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