[fltsim.0] title=BA201 sim=BA201 model= panel= sound= texture= kb_checklists= atc_heavy=0 atc_airline= atc_flight_number= ui_manufacturer=Breda ui_type= BA201 ui_variation= Prototype MM451 description=Breda BA201 dive bomber\nFirst flight on July the 3rd, 1943\n only one prototype built-for description see file\n ground handling with engine stopped\nin flight:\nanimation of dive breaks, bomb bay doors and bomb release [General] performance=Length:11.09m\nWing span:13.0m\nHeight 3.10m\nWeight:MTOW 3650 kg\n Empty 2380 kg\nPower: Daimler Benz DB601 HP 1175\nDetails:\nMax speed 420 KmH\nService ceiling 8000 m\nRange 1200 Km\nArmament:2x12.7mm Breda Safat wing mounted machine guns\n 1x500 kg bomb. Category=airplane [weight_and_balance] max_gross_weight = 8455 empty_weight =5305 reference_datum_position = 0, 0, 0 empty_weight_CG_position =8.30,0,-0.52 empty_weight_pitch_MOI = 6668.43 empty_weight_roll_MOI = 5725.72 empty_weight_yaw_MOI = 10186.09 empty_weight_coupled_MOI = 0 max_number_of_stations = 2 station_load.0 = 170, -1.5, 0.0, 1.5 station_load.1 = 170, -3.0, 0.0, 1.5 [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 0 fuel_flow_scalar = 1.00 engine.0 = 10.19, 0, -0.11, min_throttle_limit=0.00 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 number_of_tank_selectors = 1 LeftMain = 0, -3.4, -1.5, 64, 0 RightMain = 0, 3.4, -1.5, 64, 0 External1 = 0, -8.8, -2.5, 56, 0 External2 = 0, 8.8, -2.5, 56, 0 electric_pump=1 [contact_points] //0 Class //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) static_pitch =11.5 static_cg_height =6.0 tailwheel_lock = 0 max_number_of_points = 7 point.0 = 1, -12.8, 0, -5.10, 2600, 0, 0.5, 35, 0.3, 2.5, 0.8, 0, 0, 0, 0, 0 point.1 = 1, 10.3, -9, -10.12, 2600, 1, 1.25, 0, 0.5, 2.5, 0.8, 5.0, 5.0, 2, 0, 0 point.2 = 1, 10.3, 9, -10.12, 2600, 2, 1.25, 0, 0.5, 2.5, 0.8, 5.0, 5.0, 3, 0, 0 point.3 = 2, 1, -22.5, 0.5, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, 1, 22.5, 0.5, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 //point.5 = 2, -24.25, 0, 0, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 //point.6 = 2, 12, 0, 0, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 gear_system_type=0 [keyboard_response] elevator = 230.0, 500.0 aileron = 230.0, 500.0 rudder = 200.0, 500.0 [Views] eyepoint=2.0, -0.015, 1.85 //(feet) longitudinal, lateral, vertical distance from reference datum [forcefeedback] NIL [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //6=taxi light, 7=recognition light, 8=wing light, 9=logo light light.0 = 4, 2.0, 0.0, 1.92, fx_vclight_s403.fx light.1 = 4, 2.0, 0.0, 1.92, fx_vclight_s403.fx light.2 = 2, -2.45,8.50,-1.90,fx_sm95_taxi.fx light.3=2 , -11.30,28.18,6.57,fx_sm95_taxi.fx [airplane_geometry] wing_area =280.0 wing_span = 45.25 wing_root_chord = 8.25 wing_dihedral = 10.99 wing_incidence = 0.99 wing_twist = 0.00 oswald_efficiency_factor =1.4 wing_winglets_flag = 0 wing_sweep = 0.00 wing_pos_apex_lon = 1.85 wing_pos_apex_vert = 0.00 htail_area = 24.00 htail_span = 11.00 htail_pos_lon = -18.75 htail_pos_vert = 0.00 htail_incidence = 0.00 htail_sweep = 0.00 vtail_area = 15.00 vtail_span = 4.42 vtail_sweep = 0.00 vtail_pos_lon = -18.75 vtail_pos_vert = 0.58 elevator_area = 13.00 aileron_area = 20.40 rudder_area = 13.060 elevator_up_limit = 26.00 elevator_down_limit = 26.00 aileron_up_limit = 21.40 aileron_down_limit = 20.20 rudder_limit = 28.00 elevator_trim_limit = 23.00 spoiler_limit = 60.0 aileron_to_spoileron_gain = 0.00 min_ailerons_for_spoilerons = 0.00 min_flaps_for_spoilerons = 0.00 spoilerons_available = 0 auto_spoiler_available=0 spoiler_extension_time=0.800000 positive_g_limit_flaps_up=7.000000 positive_g_limit_flaps_down=4.000000 negative_g_limit_flaps_up=-5.500000 negative_g_limit_flaps_down=-4.500000 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 electric_always_available =0//1 light_panel=0, 5, 17.0 light_nav = 0, 5, 17 [flight_tuning] cruise_lift_scalar=1 parasite_drag_scalar=1 induced_drag_scalar=1 elevator_effectiveness=1 aileron_effectiveness=1 rudder_effectiveness=1 pitch_stability=1 roll_stability=1.0 yaw_stability=1 elevator_trim_effectiveness=1 aileron_trim_effectiveness=1 rudder_trim_effectiveness=1 [piston_engine] power_scalar=1.0 cylinder_displacement=177.0 compression_ratio=6.50 number_of_cylinders=12 max_rated_rpm=2400.00 max_rated_hp=1200.00 fuel_metering_type=1 cooling_type=1 normalized_starter_torque=0.07 turbocharged=1 max_design_mp=34.84 min_design_mp=1.00 critical_altitude=15091.00 emergency_boost_type=0 emergency_boost_mp_offset=0.00 emergency_boost_gain_offset=0.00 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.00 idle_rpm_mechanical_efficiency_scalar=1.00 max_rpm_friction_scalar=1.00 idle_rpm_friction_scalar=1.00 [propeller] thrust_scalar=0.8 propeller_type=0 propeller_diameter=10.9 propeller_blades=3 propeller_moi=40.99 beta_max=20.0 beta_min=13.00 min_gov_rpm=337.5 prop_tc=0.010 gear_reduction_ratio=1 fixed_pitch_beta=30.00 low_speed_theory_limit=80.00 prop_sync_available=0 prop_deice_available=1 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=700.00 beta_feather=88.5 power_absorbed_cf=0.9 defeathering_accumulators_available=0 prop_reverse_available=0.00 minimum_on_ground_beta=1 minimum_reverse_beta=-14 rotation = 1 [exits] number_of_exits = 4 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 exit_rate.2 = 0.4 exit_rate.3 = 0.4 [tailhook] tailhook_length=4 tailhook_position=0.0, 0.0, 0.0 cable_force_adjust=1.0 [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.13 ;Percent per second [brakes] toe_brakes_scale=1.6 parking_brake=1 [Flaps.0] type=1 span-outboard=0.50 extending-time=7.0 system_type=1 flaps-position.0=0 flaps-position.1=12 flaps-position.2=24 flaps-position.3=60 [Reference Speeds] flaps_up_stall_speed=64 full_flaps_stall_speed=55 cruise_speed=190.0 max_indicated_speed=250.0 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1000.00 autothrottle_available=0 pitch_takeoff_ga=8.00 max_pitch=10.0 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=9.71 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 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=7.0 [stall_warning] type=0//1 stick_shaker=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0 [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=5.000000 engine_map=1,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=0
