[fltsim.0] title=Northrop Grumman Stealth B-2A gmax sim=b2_Roger2K4 model= panel= sound= texture=gmax kb_checklists=b2_check kb_reference=b2_ref kb_notes=b2_notes atc_id=B2 ui_manufacturer=Northrop Grumman ui_type=Stealth B-2A ui_variation=Stealth B2 Spirit atc_heavy=0 atc_airline= atc_flight_number= description=The B-2 Spirit is a multi-role bomber capable of delivering both conventional and nuclear munitions. The B-2's low observability is derived from a combination of reduced infrared, acoustic, electromagnetic, visual and radar signatures. FS2004 pakage by Roger, www.rogernet.it roger@rogernet.it [pitot_static] vertical_speed_time_constant=100 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 1 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing // Anter Later Alt light.0=3, 2.00, 1.00, 9.00, fx_beaconb, light.2=1, -28.00, -74.00, 3.60, fx_navredm, light.3=1, -28.00, 74.00, 3.90, fx_navgrem , light.4=2, -28.00, 74.00, 2.00, fx_strobe , light.5=2, -28.00, -74.00, 2.00, fx_strobe , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [WEIGHT_AND_BALANCE] max_gross_weight=180000 // (pounds) empty_weight=100000 // (pounds) reference_datum_position=0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 ;Moments of Inertia empty_weight_pitch_MOI=3172439 empty_weight_roll_MOI=2262183 empty_weight_yaw_MOI=3337024 empty_weight_coupled_MOI=0 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=19.6 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=18000 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=0 //Thrust reverser available? [jet_engine] thrust_scalar=1.0 [contact_points] // long lat alt impact br radiu ang scom mcom time time point.0=1, 28.00, 0.20, -7.80, 1181.1, 0, 1.442, 55.02, 0.3, 1.5, 0.9, 4.0, 4.0, 0, 300.0, 350.0 point.1=1, -5.75, -18.48, -8.68, 1574.8, 1, 1.442, 0.00, 1.0, 3.5, 0.9, 6.9, 6.9, 2, 300.0, 350.0 point.2=1, -5.75, 18.68, -8.68, 1574.8, 2, 1.442, 0.00, 1.0, 3.5, 0.9, 7.1, 7.1, 3, 300.0, 350.0 point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -54.00, 0.00, 2.83, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 max_number_of_points=21 static_pitch=0.62 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=7.66 //feet, altitude of CG when at rest on the ground gear_system_type=0 //[Views] //eyepoint=23.324721,0.000000,2.832288 [direction_indicators] 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, 150 aileron=150, 150 rudder=150, 150 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=2200 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_max_rpm=90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8 use_no_default_bank=1 default_bank_mode=0 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 [airplane_geometry] wing_area=2137.0 //Square feet wing_span=94.75 //Feet wing_root_chord=18.0 //Feet wing_dihedral=6.2 //Degrees wing_incidence=1.0 //Degrees wing_twist=-0.5 //Degrees oswald_efficiency_factor=0.75 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=25.0 //Degrees, wing leading edge wing_pos_apex_lon=8.0 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_area=338.0 //Square feet htail_span=41.7 //Feet htail_pos_lon=-35.0 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_incidence=0.0 //Degrees htail_sweep=30.0 //Degrees, horizontal tail leading edge vtail_area=224.0 //Square feet vtail_span=20.0 //Feet, tip to body vtail_sweep=35.0 //Degrees, vertical tail leading edge vtail_pos_lon=-35.8 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=5.8 //Feet, vertical distance from reference point, positive going up elevator_area=70.5 //Square feet aileron_area=26.9 //Square feet rudder_area=56.2 //Square feet elevator_up_limit=22.5 //Degrees elevator_down_limit=19.5 //Degrees aileron_up_limit=20.0 //Degrees aileron_down_limit=20.0 //Degrees rudder_limit=26.0 //Degrees elevator_trim_limit=20.0 //Degrees spoiler_limit=60.0 //Degrees spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=3 //Aileron to spoileron gain min_ailerons_for_spoilerons=10 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=142.0 //Knots True (KTAS) full_flaps_stall_speed=113.0 //Knots True (KTAS) cruise_speed=477.0 //Knots True (KTAS) max_indicated_speed=640.000000 max_mach=0.950000 [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 [GeneralEngineData] engine_type=1 Engine.0=4.166667,-9.166667,-2.500000 Engine.1=4.166667,-8.333333,-2.500000 Engine.2=4.166667,8.333333,-2.500000 Engine.3=4.166667,9.166667,-2.500000 fuel_flow_scalar=0.324566 min_throttle_limit=0.000000 [Flaps.0] span-outboard=0.500000 extending-time=4.000000 flaps-position.0=0.000000,0.000000 flaps-position.1=5.549297,0.000000 flaps-position.2=10.098593,0.000000 flaps-position.3=20.647890,0.000000 flaps-position.4=25.197186,0.000000 flaps-position.5=30.746483,0.000000 flaps-position.6=40.295780,0.000000 damaging-speed=250 blowout-speed=300 lift_scalar=1.0 drag_scalar=1.0 pitch_scalar=1.0 system_type=0 type=1 [General] performance=Speed max.\tMach 0.95 \nCruise speed \tMach 0.8 VS 2200\nMotors \t\t4 GElec. F-118-GE-110 engines \nThrust \t\t19.000 pounds each engine \nLength \t\t69 feet (20.9 meters) \nHeight \t\t17 feet (5.1 meters) \nMax.tak.wei.\t336,500 pounds (152,635 kg) \nRange approx.\t6,000 nautical miles (9,600 km) \nCeiling Service\t35000 - 50000 atc_type=NORTHRUP atc_model=B2 [fuel] Center1=0.000000,0.000000,0.000000,1000.000000,0.000000 LeftMain=0.000000,0.000000,0.000000,2500.000000,0.000000 LeftAux=0.000000,0.000000,0.000000,1000.000000,0.000000 RightMain=0.000000,0.000000,0.000000,2500.000000,0.000000 RightAux=0.000000,0.000000,0.000000,1000.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 //***************************************************************** //***************************************************************** // Flight Dynamics by Ruggero Osto // roger@rogernet.it //***************************************************************** //***************************************************************** electric_pump=0 [brakes] toe_brakes_scale=0.885037 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 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 [Views] eyepoint=0.000000,0.000000,0.000000
