[fltsim.0] title=A-12A sim=A-12A model= panel= sound= texture= panel_alias = sound_alias = kb_checklists= kb_reference= atc_id=367 atc_id_color=0x00000000 atc_parking_code = atc_airline= atc_flight_number= ui_manufacturer=General Dynamics ui_type=A-12A ui_variation=US Navy description=Stealthy Naval Attack Plane. ui_createdby="Piglet's Peculiar Planes" visual_damage=1 atc_heavy=0 atc_id_font=Verdana,-11,1,600,0 [General] atc_type=General Dynamics atc_model=A-12A performance= editable=1 Category=airplane [pitot_static] vertical_speed_time_constant = 2 pitot_heat=1.000000 [weight_and_balance] // ACM V2.5 max_gross_weight =60000.0 empty_weight =28000.00000 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0.250, 0.000, 0.000 empty_weight_pitch_MOI =113298.46000 empty_weight_roll_MOI =73368.98000 empty_weight_yaw_MOI =147205.11000 empty_weight_coupled_MOI =0.00000 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations =4 station_load.0= 2000, 0.000, -3.000, 0.000, GBU-24_PAVEWAY station_load.1= 2000, 0.000, 3.000, 0.000, GBU_24_PAVEWAY station_load.2= 500, 0.000, -10.000, 0.000, GBU-31_JDAM station_load.3= 500, 0.000, 10.000, 0.000, GBU-31_JDAM [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 1, -1.93, 0.00, 2.5, fx_beacon light.1 = 1, 7.75, 0.00, -2.85, fx_beacon [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type =1 fuel_flow_scalar =1.00000 min_throttle_limit =0.01000 engine.0 =-12.700, -1.900, 0.000 engine.1 =-12.700, 1.900, 0.000 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 EngineFire=fx_engfire_f18 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type =2 number_of_tank_selectors =1 electric_pump =1 fuel_dump_rate =0.00190 LeftAux = 0.000, -8.000, -0.840, 150.000, 0.000 LeftMain = 0.000, -8.000, -0.840, 350.000, 0.000 RightMain = 0.000, 8.000, -0.840, 350.000, 0.000 RightAux = 0.000, 8.000, -0.840, 150.000, 0.000 LeftTip = 0.000, -15.000, -0.840, 300.000, 0.000 RightTip = 0.000, 15.000, -0.840, 300.000, 0.000 anemometer_pump=0 engine_driven_pump=1 manual_pump=0 [contact_points] static_pitch = 3.000 static_cg_height = 6.860 tailwheel_lock =0 gear_system_type =1 max_number_of_points =9 point.0= 1, 19.470, 0.000, -7.730, 2500, 0, 1.800, 50.000, 0.450, 2.222, 0.600, 3.000, 4.000, 0, 225.0, 275.0 point.1= 1, -1.833, -10.450, -6.820, 2500, 1, 2.000, 0.000, 0.350, 2.286, 0.600, 3.000, 4.000, 2, 225.0, 275.0 point.2= 1, -1.833, 10.450, -6.820, 2500, 2, 2.000, 0.000, 0.350, 2.286, 0.600, 3.500, 4.500, 3, 225.0, 275.0 point.3= 2, -0.004, -35.609, -1.530, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5 point.4= 2, 0.004, 35.453, -1.441, 2575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6 point.5= 2, -18.319, 0.000, -0.637, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9 point.6= 2, 3.777, 0.000, -1.454, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4 point.7= 5, -3.900, 0.000, 0.000, 2000, 0, 0.000, 40.000, 0.000, 0.000, 1.000, 1.000, 1.200, 0 point.8= 5, 3.900, 0.000, 0.000, 2000, 0, 0.500, 40.000, 0.000, 0.000, 1.000, 1.000, 1.000, 0 [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [airplane_geometry] wing_area =888.00000 wing_span =70.00000 wing_root_chord =18.32000 wing_dihedral =0.00000 wing_incidence =0.00000 wing_twist =0.00000 oswald_efficiency_factor =0.89160 wing_winglets_flag =0 wing_sweep =35.00000 wing_pos_apex_lon =14.06947 wing_pos_apex_vert =0.00000 htail_area =50.00000 htail_span =25.00000 htail_pos_lon =-25.89000 htail_pos_vert =0.00000 htail_incidence =0.00000 htail_sweep =30.00000 vtail_area =60.45000 vtail_span =8.27000 vtail_sweep =25.00000 vtail_pos_lon =-25.44000 vtail_pos_vert =0.10000 elevator_area =30.00000 aileron_area =45.00000 rudder_area =15.00000 elevator_up_limit =30.00000 elevator_down_limit =20.00000 aileron_up_limit =23.00000 aileron_down_limit =23.00000 rudder_limit =30.00000 elevator_trim_limit =20.00000 spoiler_limit =45.00000 aileron_to_spoileron_gain =0.00000 spoiler_handle_available =1 min_ailerons_for_spoilerons =0.00000 min_flaps_for_spoilerons =0.00000 spoilerons_available =0 auto_spoiler_available=0 positive_g_limit_flaps_up=8.50000 negative_g_limit_flaps_up=-6.80000 positive_g_limit_flaps_down=5.95000 negative_g_limit_flaps_down=-5.10000 load_safety_factor=1.00000 spoiler_extension_time=1.00000 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 engine_generator_map = 1,1 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [flight_tuning] cruise_lift_scalar=1.00000 parasite_drag_scalar=1.00000 induced_drag_scalar=1.00000 elevator_effectiveness=1.00000 aileron_effectiveness=1.00000 rudder_effectiveness=1.00000 pitch_stability=1.00000 roll_stability=1.00000 yaw_stability=1.00000 elevator_trim_effectiveness=1.00000 aileron_trim_effectiveness=1.00000 rudder_trim_effectiveness=1.00000 hi_alpha_on_roll =1.00000 hi_alpha_on_yaw =1.00000 p_factor_on_yaw =0.00000 torque_on_roll =0.00000 gyro_precession_on_roll =0.00000 gyro_precession_on_yaw =0.00000 [TurbineEngineData] fuel_flow_gain=0.00200 inlet_area=2.00000 rated_N2_rpm=10000.00000 static_thrust=13000.00000 afterburner_available =0 afterburner_throttle_threshold =0.00000 reverser_available=0 ThrustSpecificFuelConsumption =0.60000 AfterBurnThrustSpecificFuelConsumption =0.60000 [jet_engine] thrust_scalar=1.00000 [tailhook] tailhook_length= 7.000 tailhook_position= -3.500, 0.000, -2.300 [launch_assistance] launch_bar_pivot = 18.89, 0.0, -4.68 launch_bar_lug = 20.492, 0.0, -6.778 [Views] eyepoint=16.41, 0, 2.52 [Radios] // availiable, standby frequency, has glide slope Audio.1=1 Com.1=1,0 Com.2=1,0 Nav.1=1,0,1 Nav.2=1,0,0 Adf.1=1,0 Transponder.1=1 Marker.1=1 Adf.2=0,0 [direction_indicators] direction_indicator.0=1, 0 [exits] number_of_exits = 2 exit_rate.0 = 0.8 exit_rate.1 = 1.8 [autopilot] autopilot_available=1 use_no_default_bank =1 use_no_default_pitch =1 flight_director_available=0 default_vertical_speed=1000 autothrottle_available=0 autothrottle_arming_required =0 autothrottle_takeoff_ga =1 autothrottle_max_rpm =90 pitch_takeoff_ga=8 default_pitch_mode =0 default_bank_mode =0 max_pitch =10 max_pitch_acceleration =1 max_pitch_velocity_lo_alt =2 max_pitch_velocity_hi_alt =1.5 max_pitch_velocity_lo_alt_breakpoint =20000 max_pitch_velocity_hi_alt_breakpoint =28000 max_bank=25 max_bank_acceleration =1.8 max_bank_velocity =3 max_throttle_rate =0.1 nav_proportional_control =9 nav_integrator_control =0.25 nav_derivative_control =0 nav_integrator_boundary =2.5 nav_derivative_boundary =0 gs_proportional_control =9.52 gs_integrator_control =0.26 gs_derivative_control =0 gs_integrator_boundary =0.7 gs_derivative_boundary =0 yaw_damper_gain =0 [Reference Speeds] flaps_up_stall_speed=138.00000 full_flaps_stall_speed=128.00000 cruise_speed=401.10000 max_indicated_speed =710.00000 max_mach =0.85000 [gear_warning_system] gear_warning_available =0 pct_throttle_limit =0.10000 flap_limit_idle =33.75000 flap_limit_power =16.87500 [brakes] toe_brakes_scale =0.95000 parking_brake =1 auto_brakes=0 hydraulic_system_scalar=0.00000 differential_braking_scale=1.00000 [stall_warning] // 0 = None, 1 = Suction, 2 = Electric. type = 2 stick_shaker=1 [hydraulic_system] electric_pumps = 0 engine_map = 1, 1, 0, 0 normal_pressure =3000.00000 [attitude_indicators] // 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 2 [turn_indicators] // 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0 = 1 [direction_indicators] // 0=None, 1=Vac Gyro, 2=Elec Gyro, 3=EM Slave Compass, 4=Slave to other ind direction_indicator.0=2 [airspeed_indicators] airspeed_indicator.0 = 1, 0 [folding_wings] wing_fold_system_type=1 // Available fold_rates = 0.25,0.20 // Left,Right: 1/sec [AirWrench] Aircraft_Length=57.25000 Vmax_sl=577.00000 Vmax_ca=500.01348 V_rc=444.00000 Climb_Rate=29981.10791 Climb_Weight=28000.00000 Max_gforce=8.50000 Emergency_hp=0.00000 nose_position_lon=28.00000 ActualIncidence=1.00000 ActualTwist=0.00000 ActualTailIncidence=0.00000 Aircraft_Type=5 FlowCorrection=1.00000 JetAltitude=36000.00000 turboprop_critical_altitude=0.00000 target_roll_Vopt=405.50000 target_roll_rate=60.00000 pitch_damping=3.00000 yaw_damping=2.50000 elevator_scalar=1.00000 rudder_scalar=1.00000 dihedral_scalar=0.37500 Elevator_FF=30.00000 Aileron_FF=-30.00000 Roll_Response=30.00000 Adverse_Yaw=0.00000 Control_Response=100.00000 V_Max_Control=1001.17773 V_Zero_Control=2002.35546 Spin_Stability=65.00000 Stall_Stability=100.00000 Elevator_Propwash=0.00000 Rudder_Propwash=0.00000 spoiler_time=1.00000 afterburner_thrust=13000.00000 mach_scale=1.00000 spoiler_type=1 spoiler_cd=0.12000 spoiler_cl=0.00000 spoiler_cm=0.00000 flaps_type=0 flaps_cd_scalar=0.00000 flaps_cm_scalar=0.00000 vfe_enabled=1 gear_cd_scalar=0.00000 gear_cm_scalar=0.00000 cylinder_head_temperature=501.00000 exhaust_gas_temperature=1001.00000 fuel_pressure=450.00000 oil_pressure=50.00000 oil_temperature=201.00000 radiator_temperature=211.00000 exhaust_pressure_ratio=1.40000 interstage_turbine_temperature=1293.00000 knots_flag=1 cfs1_flag=0 laminar_flow=0 fixed_wing_pos=0 AirWrenchVersion=1.01.67 VSI_Weight=33000.00000 ReheatCutoff=1.50000 OptimumMach=0.90000 Power_Calibration=1.00000 weathervane=1.00000 ClAoA_S0=1.00000 ClAoA_S1=1.00000 ClAoA_S2=1.00000 prop_design_altitude=5000.00000 protect_airfile=0 critical_mach_number=0.80000 max_mach_cd0=60 mach_slope=6.00000 direct_edit_drag=0 cfs2_flag=0 ai_flag=0 fs8_flag=1 edit_tp_torque=0 direct_edit_mach=0 direct_edit_2dtab=0 range_est_alt=0.00000 range_est_rpm=0.00000 range_est_mp=29.92000 range_est_fuel=1800.00000 static_margin=0.05000 IdleRPM=0.00000 piston_research=0.00000 aileron_scalar=1.00000 sideslip_scalar=1.00000 prop_yaw_damping_scalar=1.00000 V_Max_RdrControl=817.05309 V_Zero_RdrControl=1634.10618 Roll_Off=0.00000 glide_ratio=9.11350 CritAoA=16.00000 ClAoA_k0=1.00000 ClAoA_k1=8.00000 ClAoA_k2=0.85000 ClAoA_k3=0.50000 prop_material_type=1 auto_flaps_enabled=1 lo_rpm_friction=1.00000 hi_rpm_friction=1.00000 contact_light_flags=0 cruise_attitude=0.00000 RAM_Jet_Effect=1.00000 Emulate_Turbojet=0 jet_idle_scalar=-1.00000 input_units=1 fs_version=6 keep_jet_air_defs=0 [vacuum_system] max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=0.150000 [GPWS] max_warning_height =0 sink_rate_fpm =-9999 excessive_sink_rate_fpm =-9999 climbout_sink_rate_fpm =-9999 flap_and_gear_sink_rate_fpm=-9999 [deice_system] structural_deice_type=1 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots [Pressurization] design_cabin_pressure = 10.9 ;PSI (~8000 feet) max_pressure_differential = 4.96 ;PSI [forcefeedback] gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1 crash_magnitude1=10000 crash_direction1=1000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 stick_shaker_magnitude=5000 stick_shaker_direction=0 stick_shaker_period=111111