[fltsim.0] title=RQ-4B sim=RQ-4B model= panel=F86 sound= texture= checklists= ui_manufacturer=Northrop ui_type=RQ-4 Block 20 Global Hawk ui_variation=RQ-4B ui_typerole=Unmanned Aerial Vehicle ui_createdby=Kazunori Ito atc_airline=Air Force atc_flight_number=4B atc_heavy=0 atc_id=952001 description=The Block 20 Global Hawk (RQ-4B) is a High Altitude, Long Range, Unmanned Aerial Vehicle (UAV) operated by the U.S. Air Force.\nCreated by: Kazunori Ito\nPanel by: Bob Chicilon\nSound by: Aaron R. Swindle\n\nFlight Dynamics, Data and Modifications by:\nDouglas E. Trapp\nFS Flight Dynamics Engineer\nKC6ZOF@Yahoo.com\nJuly 2010\n [General] performance=Engine: Rolls Royce AE3007H (F137-AD-100) @ 8,917 lbf\nLength: 47.6 ft\nWing Span: 130.9 ft\nHeight: 15.4 ft\nMTOW: 32,250 lbs\nRamp Weight: 32,350 lbs\nPayload Weight: 3,000 lbs\nFuel Capacity: 2,694 US gal\nStructure: Aluminum and composite\nLoiter Velocity: 310 TAS\nHigh Altitude Cruise Speed: Mach .80\nMax Cruise Speed: Mach .85\nMax Altitude: 65,000 ft\nMaximum Endurance: 35 hrs\nFerry Range: 12,300 nm\n atc_type=NORTHROP atc_model=RQ4 editable=1 Category=airplane [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=50 station_load.0=3000.000000,0.000000,0.000000,0.000000 max_gross_weight=32250.000000 empty_weight=11300.000000 empty_weight_roll_MOI=2262183.000000 empty_weight_pitch_MOI=3172439.000000 empty_weight_yaw_MOI=3337024.000000 empty_weight_coupled_MOI=500.000000 [fuel] 18,050 lb fuel = 2,694 US gal Center1=0.000000,0.000000,0.000000,264.000000,0.000000 LeftMain=0.000000,-32.725000,0.000000,1215.000000,0.000000 RightMain=0.000000,32.725000,0.000000,1215.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.00 induced_drag_scalar=1.00 pitch_stability=2.000 roll_stability=2.000 yaw_stability=2.000 elevator_effectiveness=2.000 aileron_effectiveness=2.000 rudder_effectiveness=2.000 elevator_trim_effectiveness=2.000 aileron_trim_effectiveness=2.000 rudder_trim_effectiveness=2.000 [airplane_geometry] wing_area=608.364000 wing_span=130.905250 wing_aspect_ratio=25.000000 wing_root_chord=23.583333 wing_dihedral=2.000000 wing_incidence=0.000000 wing_twist=-0.499878 oswald_efficiency_factor=1.000000 wing_winglets_flag=0 wing_sweep=5.900000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=42.800000 htail_span=11.400000 htail_pos_lon=-50.000000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=2.000000 vtail_area=42.800000 vtail_span=11.400000 vtail_sweep=2.000000 vtail_pos_lon=-35.833333 vtail_pos_vert=17.083333 elevator_area=70.500000 aileron_area=60.000000 rudder_area=56.200000 elevator_up_limit=26.000825 elevator_down_limit=26.000825 aileron_up_limit=30.000070 aileron_down_limit=30.000070 rudder_limit=30.000070 elevator_trim_limit=19.996227 spoiler_limit=59.988681 spoilerons_available=1 aileron_to_spoileron_gain=3.000000 min_ailerons_for_spoilerons=10.000000 min_flaps_for_spoilerons=0.000000 auto_spoiler_available=0 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=3.000000 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-2.000000 [contact_points] point.0=1.000000,36.000000,0.000000,-8.833333,3149.606299,0.000000,0.906000,55.920000,0.430599,2.500000,1.219228,4.000000,4.000000,0.000000,0.000000,0.000000 point.1=1.000000,-4.750000,-8.583333,-9.083333,3149.606299,1.000000,0.906000,0.000000,0.430611,2.500000,1.066783,6.900000,6.900000,2.000000,0.000000,0.000000 point.2=1.000000,-4.750000,8.583333,-9.083333,3149.606299,2.000000,0.906000,0.000000,0.430611,2.500000,1.066783,7.100000,7.100000,3.000000,0.000000,0.000000 point.3=2.000000,-14.166667,-47.333333,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-14.166667,47.333333,0.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-54.000000,0.000000,2.833333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,42.666667,0.000000,-3.750000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=0.390015 static_cg_height=7.790762 gear_system_type=0 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=19.996227,0.000000 flaps-position.2=39.992454,0.000000 [GeneralEngineData] engine_type=1 Engine.0=-15.000000,0.000000,2.000000 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [SMOKESYSTEM] smoke.0=-25.000000,0.000000,2.000000, fx_smoke_f6 [TurbineEngineData] //Rolls Royce AE3007H (F137-AD-100) fuel_flow_gain=0.002000 inlet_area=3.625000 bypass_ratio=5.000000 rated_N1_rpm=7915.300000 rated_N2_rpm=22676.475000 static_thrust=8917.000000 afterburner_available=0 reverser_available=0 thrust_scalar=1.00 [Reference Speeds] flaps_up_stall_speed=125.000000 full_flaps_stall_speed=95.000000 cruise_speed=310.000000 max_indicated_speed=344.000000 max_mach=0.855000 [keyboard_response] elevator=0.000000,0.000000 aileron=0.000000,0.000000 rudder=0.000000,0.000000 [Views] eyepoint=19.300566,0.000000,-0.794578 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=112.000000 pitch_takeoff_ga=8.000000 use_no_default_bank=1 use_no_default_pitch=1 default_pitch_mode=0 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 [direction_indicators] direction_indicator.0=3,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //6=taxi light, 7=recognition light, 8=wing light, 9=logo light // Z, X, Y light.0=3, 0.82, 0.00, -0.30, fx_navred , light.1=2, 0.82, 0.00, -0.30, fx_strobe , light.2=3, -6.50, 0.00, -5.35, fx_navred , light.3=2, -6.50, 0.00, -5.35, fx_strobe , light.4=3, -5.35, 58.13, -4.20, fx_navgre , light.5=2, -5.35, 58.13, -4.20, fx_strobe , light.6=3, -5.35, -58.13, -4.20, fx_navred , light.7=2, -5.35, -58.13, -4.20, fx_strobe , light.8=3, -21.49, 0.00, -3.94, fx_navwhi , [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 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [brakes] toe_brakes_scale=0.700000 parking_brake=1 auto_brakes=4 [pitot_static] pitot_heat=1.000000 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=3000.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [deice_system] structural_deice_type=0