//5:53 PM 3/9/2005 Version 2.1 for FS9 [fltsim.0] title=ALPHA RA-5C Vigilante sim=RA-5C model= panel= sound= texture= KB_checklists=vigilante_check kb_reference= ui_manufacturer=North American ui_type=RA-5C Vigilante ui_variation=USS Ranger atc_id_color=0x00000000 visual_damage=1 atc_parking_types=MIL_COMBAT description=© ALPHA Simulations 2005\n\nNorth American RA-5C Vigilante\n\nPlanned in late 1950's as a successor to the AJ-1 Savage, the Vigilante prototype first flew in 1958 and was decades ahead of its time, with many 'firsts' such as a digital computer, INS, slab tail and variable inlets and much more. Although conceived as a bomber, the USAF soon adopted the nuclear strike role which meant the A-5 was used solely for the recon role. The RA-5C was used in Vietnam (18 were lost) and continued in service until 1980. atc_heavy=0 atc_id= atc_airline= atc_flight_number= atc_id_font=Verdana,-11,1,600,0 [General] performance=Model: M Davies\nPanel: P Perrott\nTextures: M Davies\nFlight Model: J McDaniel\n\nLength: 76 ft 0 in\nSpan: 53 ft 0.4 in\nWing area: 754 sq ft\nWeight: Empty: 43,608 lbs\s loaded, 68,088 lbs.\nPower: (2) GE J79-GE-10 Turbojet, 17,860 lbs thrust with afterburners\nRange: 3,000 miles\nMax Speed: Mach 2.1 @ 36,000 ft\nService Ceiling: 48,400 ft.\nArmament: None editable=1 atc_type= atc_model= Category=airplane [weight_and_balance] max_gross_weight = 68088.00 empty_weight = 43608.00 reference_datum_position = 0.00, 0.00, 0.00 empty_weight_CG_position = 0.00, 0.00, 0.00 empty_weight_pitch_MOI = 172817.00 empty_weight_roll_MOI = 77250.00 empty_weight_yaw_MOI = 145928.00 empty_weight_coupled_MOI = 0.00 CG_forward_limit = 0.00 CG_aft_limit = 1.00 max_number_of_stations = 2 station_load.0 =200.00, 28.70, 0.00, 0.81, Station 1 station_load.1 =200.00, 22.08, 0.00, 1.52, Station 2 [smokesystem] smoke.0 = -30.00,-3.00, -0.70, fx_smoke_f6 smoke.1 = -30.00, 3.00, -0.70, fx_smoke_f6 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 4, 29.60, 0, 1.28, fx_vclight light.1= 4, 23.42, 0, 2.09, fx_vclight light.2= 1, -9.5, 0, 2.20, fx_beacon light.3= 1, -7.70, 0, -3.80, fx_beacon //afterburner effects light.13= 6, -24.7, -3.1, -0.90, fx_Bob_Burn_blue , // Eng1 Afterburner light.14= 6, -28.3, -3.0, -1.30, fx_F14_Burnerflame , // Eng1 Afterburner Flame light.15= 6, -24.7, 3.1, -0.90, fx_Bob_Burn_blue , // Eng2 Afterburner light.16= 6, -28.3, 3.0, -1.30, fx_F14_Burnerflame , // Eng2 Afterburner Flame light.17= 6, -26.0, -3.1, -0.70, fx_Bob_small_Blueflame , // Eng1 Blueflame, light.18= 6, -26.0, 3.0, -0.70, fx_Bob_small_Blueflame , // Eng2 Blueflame, [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 0.60 min_throttle_limit = 0.00 engine.0 = -24.70, -3.10, -0.70 engine.1 = -24.70, 3.10, -0.70 [TurbineEngineData] fuel_flow_gain= 0.002 inlet_area= 13.40 rated_N2_rpm= 29920.00 static_thrust= 17860.00 afterburner_available= 1 reverser_available= 0.00 [Reference Speeds] flaps_up_stall_speed= 123.00 full_flaps_stall_speed= 93.00 cruise_speed= mach 0.94 //320 indicated at 37,000 max_indicated_speed=1600.00 max_mach=2.50 max_level_speed=1205 //Knots over the ground at 36,000 ft. [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 = 0 //Simple flight model Center1 = 0.00, 0.00, 0.00, 460.00, 0.00 Center2 = 0.00, 0.00, 0.00, 500.00, 0.00 Center3 = 0.00, 0.00, 0.00, 130.00, 0.00 LeftMain = 0.00,-9.00, 0.00, 830.00, 0.00 RightMain = 0.00, 9.00, 0.00, 830.00, 0.00 External1 = 0.00,-9.00,-3.00, 295.00, 0.00 External2 = 0.00, 9.00,-3.00, 295.00, 0.00 [contact_points] static_pitch = 1.220 static_cg_height = 7.620 tailwheel_lock = 0 gear_system_type = 1 point.0 = 1, 17.20, 0.00, -8.20, 2000.00, 0.00, 1.10, 25.00, 0.20, 2.00, 0.80, 5.00, 5.00, 0.00, 300.00, 325.00 point.1 = 1, -5.00, -5.70, -7.80, 3000.00, 1.00, 1.50, 0.00, 0.40, 2.50, 0.80, 5.00, 5.00, 2.00, 300.00, 325.00 point.2 = 1, -5.00, 5.70, -7.80, 3000.00, 2.00, 1.50, 0.00, 0.40, 2.50, 0.80, 5.00, 5.00, 3.00, 300.00, 325.00 //scrape point.3 = 2, -12.30, -27.00, 1.20, 1500.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00 point.4 = 2, -12.30, 27.00, 1.20, 1500.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00 point.5 = 2, -27.20, 0.00, -2.50, 1500.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00 point.6 = 2, 42.40, 0.00, -1.80, 1500.00, 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, 250.00 rudder = 150.00, 250.00 [forcefeedback] gear_bump_nose_magnitude = 1000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2000 gear_bump_right_direction = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 450 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1 crash_magnitude1 = 2000 crash_direction1 = 1000 crash_magnitude2 = 2000 crash_direction2 = 9000 crash_period2 = 7500 crash_duration2 = 2500000 stick_shaker_magnitude = 2000 stick_shaker_direction = 0 stick_shaker_period = 111111 [airplane_geometry] wing_area = 754.00 wing_span = 54.210 wing_root_chord = 22.40 wing_dihedral = 2.00 wing_incidence = 0.00 wing_twist = 0.00 oswald_efficiency_factor = 0.880 wing_winglets_flag = 0 wing_sweep = 43.00 wing_pos_apex_lon = 9.50 wing_pos_apex_vert = 1.50 htail_area = 116.00 htail_span = 32.20 htail_pos_lon = -12.70 htail_pos_vert = -0.30 htail_incidence = -0.50 htail_sweep = 50.00 vtail_area = 50.00 vtail_span = 13.20 vtail_sweep = 50.00 vtail_pos_lon = -13.40 vtail_pos_vert = 1.50 elevator_area = 77.00 aileron_area = 25.00 rudder_area = 40.00 elevator_up_limit = 21.00 elevator_down_limit = 13.00 aileron_up_limit = 15.00 aileron_down_limit = 15.00 rudder_limit = 8.00 elevator_trim_limit = 18.00 spoiler_limit = 70.00 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=0 spoiler_extension_time=1.000000 positive_g_limit_flaps_up=9.017094 positive_g_limit_flaps_down=6.205128 negative_g_limit_flaps_up=-6.205128 negative_g_limit_flaps_down=-4.136752 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 300 engine_generator_map = 1,1 electric_always_available = 1 [TailHook] tailhook_length=6.5 tailhook_position=-18.35, 0.0, -1.0 cable_force_adjust=1.0 [folding_wings] wing_fold_system_type=4 fold_rates=0.12,0.11 [exits] number_of_exits=1 exit_rate.0=0.7 [Views] eyepoint=29.5,0.0,2.2 [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=125.00 pitch_takeoff_ga=8.00 max_pitch=10.00 max_pitch_acceleration=2.00 max_pitch_velocity_lo_alt=1.00 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=0.250 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.520 gs_integrator_control=0.260 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=1.0031 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=1 engine_map=1,1,0,0 normal_pressure=3000.00 [stall_warning] type=1 stick_shaker=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [General] atc_type= atc_model= performance= editable=1 [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 [Flaps.0] type= 1 span-outboard= 0.65 extending-time= 5.00 system_type= 1 damaging-speed= 230.00 blowout-speed= 250.00 lift_scalar= 1.00 drag_scalar= 0.00 pitch_scalar= 1.00 flaps-position.0= 0.00, 0.00 flaps-position.1= 20.00, 0.00 flaps-position.2= 40.00, 0.00 flaps-position.3= 60.00, 0.00 flaps-position.4= 70.00, 0.00 flaps-position.5= 80.00, 0.00 [Flaps.1] type= 2 span-outboard= 0.65 extending-time= 5.00 system_type= 1 damaging-speed= 230.00 blowout-speed= 250.00 lift_scalar= 0.00 drag_scalar= 1.00 pitch_scalar= 0.00 flaps-position.0= 0.00, 0.00 flaps-position.1= 1.00, 0.00 flaps-position.2= 15.00, 0.00 flaps-position.3= 30.00, 0.00 flaps-position.4= 50.00, 0.00 flaps-position.5= 80.00, 0.00 [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