[fltsim.0] title=A3-b Heavy Attack Skywarrior sim=A3-D HA model= panel= sound= texture= ui_manufacturer=Douglas kb_checklists= description=Douglas A-3 (A3D) Skywarrior Biggest and heaviest aircraft ever designed for routine use from an aircraft carrier, the Skywarrior was the Navy's first twin-jet nuclear bomber and has been in service for over twenty years. Design of this truly great aircraft was undertaken in early 1947 in answer to an RFP (Request for Proposals) circulated to selected aircraft manufacturers by the Bureau of Aeronautics. At that time the aircraft was intended for use aboard the new super carrier being planned by the Navy, and the RFP specified that the bomber was to be capable of carrying a 10,000-lb (4,536-kg) nuclear device a distance of 2,000 naut miles (3,700 km) and then return to its carrier. Furthermore, gross weight was not to exceed 100,000 lb. (45,360 kg) and power was to be supplied by two new turbojets in the 10,000 lb. (4,536 kg) thrust class.also to provide surface surveillance and intelligence collection, electronic warfare, coordinated search and rescue, and fleet support missions, including air wing tanking atc_id_color=0000000000 visual_damage=0 [General] performance=Specifications Manufactured by Douglas Length 76 ft. 4 in. 23.27 meters Wingspan 72 ft. 6 in. 22.1 meters Height 22 ft. 9.5 in. 6.95 meters Wingarea 812 sq. ft. 75.43 sq. m. Empty Weight 39,409 lbs. 17,876 kg. Loaded Weight 70,000 lbs. 31,751 kg. Maximum Weight 82,000 lbs. 37,195 kg. Wing loading 86.2 lb./sq. ft. 420.9 kg./sq. m. Power loading 2.8 lb./lb. Propulsion No. of Engines 2 Powerplant Pratt & Whitney J57-P-10 Thrust (each engine) 10,500 lb. no injection 12,400 lb. water injection Performance Range 2100 miles 3381 km. cruise speed 520 mph 837 km/h max. speed 610 mph 982 km/h service ceiling 41,000 ft. 12,495 m Dimensions, weights and performance for A-3B editable=0 [Flaps.0] type=1 span-outboard=0.500000 extending-time=10.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=13.330818,0.000000 flaps-position.2=26.661636,0.000000 flaps-position.3=39.992454,0.000000 [GeneralEngineData] engine_type=1 Engine.0=-6.250000,-3.750000,0.416667 Engine.1=-6.250000,3.750000,0.416667 fuel_flow_scalar=1.000000 min_throttle_limit=-0.199951 [TurbineEngineData] fuel_flow_gain=0.002000 inlet_area=10.550000 rated_N2_rpm=29920.000000 static_thrust=10275.000000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=95.000000 full_flaps_stall_speed=76.000000 cruise_speed=475.687304 max_indicated_speed=437.960938 max_mach=0.900000 [Views] eyepoint=14.191015,-0.907210,3.626312 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.20,0.28 ;Percent per second [exits] number_of_exits=3 exit_rate.0=0.4 ;Percent per second [TailHook] tailhook_length=5 ;(feet) tailhook_position=-17.0, 0.0, -0.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=5.0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 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 [weight_and_balance] // ACM V1.0 pl5 max_gross_weight = 39831 empty_weight = 26554 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 229000 empty_weight_roll_MOI = 203386 empty_weight_yaw_MOI = 327143 empty_weight_coupled_MOI = 1300 max_number_of_stations = 1 station_load.0 = 0.000000,0.000000,0.000000,0.000000 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -7.2, -25.7, 0.7, fx_navred , light.1 = 3, -7.2, 25.7, 0.8, fx_navgre , light.2 = 3,-31.6, 0.0, 2.2, fx_navwhi , light.3 = 2, -7.4, -25.8, 0.7, fx_strobe , light.4 = 2, -7.4, 25.8, 0.8, fx_strobe , light.5 = 4, 17.183, 0.0, 2.0, fx_vclight, light.6 = 4, 17.183, -1.0, 2.0, fx_vclight, light.7 = 4, 17.183, 1.0, 2.0, fx_vclight, light.8 = 4, 16.583, 0.0, 2.0, fx_vclight, light.9 = 4, 16.583, -1.0, 2.0, fx_vclight, light.10 = 4, 16.583, 1.0, 2.0, fx_vclight, [smokesystem] smoke.0 = 0.00,-0.00, 10.00, fx_smoke_mig smoke.1 = 0.00,-0.00,-10.00, fx_smoke_mig [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 Center1 = -6.86, 0, -1.5, 405, 0 LeftMain = -1.8, -10, -1.5, 790, 0 RightMain = -1.8, 10, -1.5, 790, 0 [contact_points] static_pitch = 1 static_cg_height = 2.6 max_number_of_points = 7 point.0 = 1, 14.5, 0, -9, 1574.80315, 0, 0.776281, 41.82, 1.514752, 2.5, 2.301588, 5, 5, 0, 0, 0 point.1 = 1, -15, -6.083333, -6.9, 1574.80315, 1, 0.776281, 0, 0.773619, 2.5, 1.245392, 5, 5, 2, 0, 0 point.2 = 1, -14.916667, 5.083333, -6.9, 1574.80315, 2, 0.776281, 0, 0.773619, 2.5, 1.245392, 5, 5, 3, 0, 0 point.3 = 2.000000,-5.416667,-34.583333,4.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4 = 2.000000,-5.416667,34.583333,4.666667,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5 = 2.000000,-22.250000,0.000000,2.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6 = 2.000000,19.083333,0.000000,-0.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 [keyboard_response] elevator = 150.000000, 250.000000 aileron = 150.000000, 250.000000 rudder = 150.000000, 250.000000 [forcefeedback] gear_bump_nose_magnitude = 0 gear_bump_nose_direction = 0 gear_bump_nose_duration = 0 gear_bump_left_magnitude = 0 gear_bump_left_direction = 0 gear_bump_left_duration = 0 gear_bump_right_magnitude = 0 gear_bump_right_direction = 0 gear_bump_right_duration = 0 ground_bumps_magnitude1 = 0 ground_bumps_angle1 = 0 ground_bumps_intercept1 = 5# ground_bumps_slope1 = 0 ground_bumps_magnitude2 = 0 ground_bumps_angle2 = 0 ground_bumps_intercept2 = 0 ground_bumps_slope2 = 1# crash_magnitude1 = 10000 crash_direction1 = 1000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 [TailHook] tailhook_length=8 ;(feet) tailhook_position = -15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust = 1.0 [airplane_geometry] wing_area=537.000000 wing_span=43.333333 wing_root_chord=12.416667 wing_dihedral=2.999268 wing_incidence=-0.494385 wing_twist=-0.999756 oswald_efficiency_factor=0.750684 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.019170 wing_pos_apex_vert=0.000000 htail_area=54.000000 htail_span=14.666667 htail_pos_lon=-20.250000 htail_pos_vert=0.000000 htail_incidence=0.999756 htail_sweep=0.000000 vtail_area=37.000000 vtail_span=6.935416 vtail_sweep=0.000000 vtail_pos_lon=-18.833333 vtail_pos_vert=5.833333 elevator_area=13.500000 aileron_area=21.480000 rudder_area=6.290000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=30.000070 aileron_down_limit=30.000070 rudder_limit=30.000070 elevator_trim_limit=19.480565 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [brakes] toe_brakes_scale=1.000000 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=30.022988 flap_limit_idle=15.011494 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [fltsim.1] title=a3dpan sim=a3d model= panel=pan sound= texture= ui_manufacturer=Douglas kb_checklists= description=test atc_id_color=0000000000 visual_damage=0 ui_variation=test