//5:12 PM 12/8/2004 [fltsim.0] title=ALPHA A-3 Skywarrior sim=Alpha_A-3 model= panel= sound= texture= KB_checklists=skywarrior_check kb_reference= ui_manufacturer=ALPHA ui_type=A-3 Skywarrior ui_variation=A-3B, VAQ-133 #610 (Wizzards), USS Kittyhawk description=© ALPHA Simulations 2005\n\nDouglas A-3 Skywarrior\n\nThe A-3B Skywarrior was the largest carrier-based aircraft of its time, designed to operate from the Forrestal-class supercarriers. Intended as a strategic attack aircraft, the Skywarrior was designed for long range, with a thin, high-aspect ratio wing. Recon, ECM, and tanker versions were also built, with the EKA-3B combination ECM / tanker remaining in service up to the time of the first Gulf War. The length of the Skywarrior's service life is a testament to the soundness of the original clean, efficient design. atc_id_color=0x00000000 atc_heavy=0 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 atc_id= atc_airline= atc_flight_number= atc_parking_types=MIL_COMBAT [fltsim.1] title=ALPHA A-3 Skywarrior - camo sim=Alpha_A-3 model= panel= sound= texture=camo KB_checklists=skywarrior_check kb_reference= ui_manufacturer=ALPHA ui_type=A-3 Skywarrior ui_variation=RA-3B, VAP-62, SE Asia, late 1960's description=© ALPHA Simulations 2005\n\nDouglas A-3 Skywarrior\n\nThe A-3B Skywarrior was the largest carrier-based aircraft of its time, designed to operate from the Forrestal-class supercarriers. Intended as a strategic attack aircraft, the Skywarrior was designed for long range, with a thin, high-aspect ratio wing. Recon, ECM, and tanker versions were also built, with the EKA-3B combination ECM\/tanker remaining in service up to the time of the first Gulf War. The length of the Skywarrior's service life is a testament to the soundness of the original clean, efficient design. atc_id_color=0x00000000 atc_heavy=0 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 atc_id= atc_airline= atc_flight_number= atc_parking_types=MIL_COMBAT [General] performance=Model: AlphaSim\nPanel: H Pralle\nTextures: D Swart\nFlight Model: J. McDaniel\n\nLength: 76 ft 4 in\nSpan: 72 ft 6 in\nWing area: 812 sq ft\nWeight: Empty: 39,409 lbs\s loaded, 82,000 lbs.\nPower: (2) Pratt & Whitney J-57-P-10 Turbojet, 10,500 lbs thrust\nRange: 2,900 miles\nMax Speed: 610 m.p.h @ 10,000 ft\nService Ceiling: 41,000 ft.\nArmament: (2) 20 mm trainable cannon, radar-aimed, and up to 12,000 lbs of ordnance in an internal weapons bay. editable=1 atc_type= atc_model= Category=airplane [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -33.20, 0.00, 17.55, fx_navwhi light.1 = 3, 6.89, 0.00, 4.75, fx_beacon ; top light.2 = 3, -4.60, 0.00, -3.12, fx_beacon ; btm light.3 = 4, 28.26, -1.64, 2.11, fx_vclight ; pilot light.4 = 4, 26.11, 1.61, 2.66, fx_vclight ; nav light.5 = 4, 23.10, -1.99, 3.05, fx_vclight ; crewchief [smokesystem] smoke.0 = -4.90, -13.91, -1.42, fx_eng_exhaust_gry smoke.1 = -4.90, 13.91, -1.42, fx_eng_exhaust_gry [weight_and_balance] // ACM V2.5 max_gross_weight = 82000 empty_weight = 39409 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 28670 empty_weight_roll_MOI = 199624 empty_weight_yaw_MOI = 279527 empty_weight_coupled_MOI = 0 CG_forward_limit = 0.00 CG_aft_limit = 1.00 max_number_of_stations = 3 station_load.0 = 200.00, 27.11,-1.49, 2.66, Station 1 station_load.1 = 195.00, 25.68, 1.58, 2.63, Station 2 station_load.2 = 5.00, 0.00, 0.00, 0.00, Station 3 [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 1.00 min_throttle_limit = 0.00 engine.0 = 0.00, -13.80, -1.50 engine.1 = 0.00, 13.80, -1.50 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=17.80 rated_N2_rpm=29920.00 static_thrust=11500.00 afterburner_available=0 reverser_available=0.00 [Reference Speeds] flaps_up_stall_speed=116.5 full_flaps_stall_speed=82.5 cruise_speed=520 mph //457 knots over the ground at 37,000 ft. (262 ind.) max_indicated_speed=685 max_mach=1.0 max_level_speed=610 mph //537 knots over the ground at 10,000 ft. (501 ind.) [effects] windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 electric_pump = 1 Center1 = 0, 0, 3, 1200, 0 LeftMain = 5,-10, 3, 1200, 0 RightMain= 5, 10, 3, 1200, 0 [contact_points] static_pitch = 4.59 static_cg_height = 6.61 tailwheel_lock = 0 gear_system_type = 1 max_number_of_points = 17 point.0 = 1, 25.40, 0.00, -9.10, 1574.80, 0.00, 1.25, 42.54, 0.50, 2.50, 0.70, 6.00, 6.00, 0.00, 0.00, 0.00 point.1 = 1, -2.10, -5.20, -6.80, 1875.17, 1.00, 1.70, 0.00, 0.30, 2.50, 0.69, 5.00, 5.00, 2.00, 0.00, 0.00 point.2 = 1, -2.10, 5.20, -6.80, 1875.17, 2.00, 1.70, 0.00, 0.30, 2.50, 0.69, 5.00, 5.00, 3.00, 0.00, 0.00 point.3 = 1, -18.90, 0.00, -3.70, 1574.80, 0.00, 0.10, 0.00, 0.10, 2.50, 1.00, 6.00, 0.00, 6.00, 0.00, 0.00 point.4 = 2, -13.10, -35.90, 1.80, 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.5 = 2, -13.10, 35.90, 1.80, 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.6 = 2, 38.10, 0.00, 0.40, 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.7 = 2, -30.10, 0.00, 0.20, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00 [keyboard_response] elevator = 150.00, 250.00 aileron = 150.00, 150.00 rudder = 150.00, 250.00 [airplane_geometry] wing_area = 812.00 wing_span = 72.50 wing_root_chord = 15.50 wing_dihedral = -7.00 wing_incidence = 0.00 wing_twist = 0.00 oswald_efficiency_factor = 0.85 wing_winglets_flag = 0 wing_sweep = 40.00 wing_pos_apex_lon = 15.50 wing_pos_apex_vert = 3.70 htail_area = 100.00 htail_span = 25.00 htail_pos_lon = -18.60 htail_pos_vert = 7.00 htail_incidence = 0.00 htail_sweep = 40.00 vtail_area = 120.00 vtail_span = 13.80 vtail_sweep = 55.00 vtail_pos_lon = -11.00 vtail_pos_vert = 4.60 elevator_area = 60.00 aileron_area = 80.00 rudder_area = 40.00 elevator_up_limit = 28.00 elevator_down_limit = 22.00 aileron_up_limit = 20.00 aileron_down_limit = 15.00 rudder_limit = 22.00 elevator_trim_limit = 18.00 spoiler_limit = 60.00 aileron_to_spoileron_gain = 0.00 spoiler_handle_available = 1 min_ailerons_for_spoilerons = 0.00 min_flaps_for_spoilerons = 0.00 spoilerons_available = 0 auto_spoiler_available=1 spoiler_extension_time=1.00 positive_g_limit_flaps_up=10.00 positive_g_limit_flaps_down=8.00 negative_g_limit_flaps_up=-8.00 negative_g_limit_flaps_down=-7.00 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 50 engine_generator_map = 1,1 electric_always_available = 0 flap_motor = 0, 5, 0 gear_motor = 0, 5, 0 autopilot = 0, 5, 0 avionics_bus = 0, 10, 0 avionics = 1, 5, 0 pitot_heat = 0, 2, 0 additional_system = 0, 20, 0 marker_beacon = 1, 2, 0 gear_warning = 0, 2, 0 fuel_pump = 0, 5, 0 starter1 = 0, 20, 0 light_nav = 0, 5, 0 light_beacon = 0, 5, 0 light_landing = 0, 5, 0 light_taxi = 0, 5, 0 light_strobe = 0, 5, 0 light_panel = 0, 5, 0 [exits] number_of_exits=1 exit_rate.0=0.5 [TailHook] tailhook_length = 4 tailhook_position = -15, 0, -1 cable_force_adjust = 1 [Views] eyepoint=27.0, -1.5, 3.75 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.00 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=100.00 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=1.50 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=0.00 [direction_indicators] direction_indicator.0=3,0 [brakes] toe_brakes_scale=1.07 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=1 flap_limit_power=25 flap_limit_idle=5 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=3000.00 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.11 ;Percent per second [Flaps.0] type= 1 span-outboard= 0.50 extending-time= 5.00 system_type= 0 damaging-speed= 350.00 blowout-speed= 500.00 lift_scalar= 1.00 drag_scalar= 1.00 pitch_scalar= 1.00 flaps-position.0= 0.00, 0.00 flaps-position.1= 10.00, 0.00 flaps-position.2= 20.00, 0.00 flaps-position.3= 35.00, 0.00 flaps-position.4= 50.00, 0.00 [Flaps.1] type= 2 span-outboard= 0.50 extending-time= 2.00 system_type= 0 damaging-speed= 300.00 blowout-speed= 350.00 lift_scalar= 1.00 drag_scalar= 1.00 pitch_scalar= 1.00 flaps-position.0=0 flaps-position.1=0.25 flaps-position.2=0.5 flaps-position.3=0.75 flaps-position.4=1.0 [Flaps.2] type= 2 span-outboard= 0.50 extending-time= 2.00 system_type= 0 damaging-speed= 300.00 blowout-speed= 350.00 lift_scalar= 1.00 drag_scalar= 1.00 pitch_scalar= 1.00 flaps-position.0=0 flaps-position.1=0.25 flaps-position.2=0.5 flaps-position.3=0.75 flaps-position.4=1.0 [pitot_static] pitot_heat=1.00 [vacuum_system] max_pressure=5.15 vacuum_type=2 electric_backup_pressure=0.00 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.00 bleed_air_scalar=1.00 [deice_system] structural_deice_type=0
