[fltsim.0] title=A6M2 Zero sim=A6M2_Zero model= panel= sound= texture= KB_checklists=a6m2_zero_check ui_manufacturer=Mitsubishi ui_type=A6M2 Zero ui_variation=Japanese Navy description=When the war began, the Zero gave enemy pilots a rude shock. No Allied fighter could match the Zero's phenomenal maneuverability and climb, or its range. Some thought the Zero was invincible, but the Zero got its performance through light construction - and a lack of armor or self-sealing tanks. The Zero pilot learned to use the plane's outstanding maneuverability to out-turn and- in some cases - out-climb Allied aircraft. Even when the U.S. introduced faster and more powerful fighters, pilots could never underestimate the Zero - in the hands of a skilled pilot, it was always a dangerous adversary against any American fighter. [WEIGHT_AND_BALANCE] empty_weight = 3704 // (pounds) reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = 170, -3.0, 0.0, 3.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 3673.15 empty_weight_roll_MOI = 2788.86 empty_weight_yaw_MOI = 7226.17 empty_weight_coupled_MOI=0.00 max_gross_weight=5811.00 [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.11 ;Percent per second [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [piston_engine] power_scalar = 1.0 cylinder_displacement=125.85700 compression_ratio=7.200 number_of_cylinders=14 max_rated_rpm=2600.00 max_rated_hp=940.00 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.03500 turbocharged=1 max_design_mp=39.870 min_design_mp=1.00 critical_altitude=14400.00 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=1.080 idle_rpm_mechanical_efficiency_scalar=1.00 max_rpm_friction_scalar=1.00 idle_rpm_friction_scalar=1.00 [propeller] thrust_scalar = 1.0 propeller_type=0 propeller_diameter=9.500 propeller_blades=3 propeller_moi=22.500 beta_max=45.00 beta_min=25.00 min_gov_rpm=1400.00 prop_tc=0.0100 gear_reduction_ratio=1.7100 fixed_pitch_beta=0.00 low_speed_theory_limit=80.00 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.00 beta_feather=0.00 power_absorbed_cf=0.00 defeathering_accumulators_available=0 prop_reverse_available=0.00 minimum_on_ground_beta=0.00 minimum_reverse_beta=0.00 [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [electrical] max_battery_voltage = 24.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps = 60.0 [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) point.0=1, -20.21, 0.00, -1.60, 3200, 0, 0.30,180.0, 0.40, 2.5, 0.80, 7.5, 5.00, 0, 0, 135 point.1=1, 1.41, -5.76, -6.55, 2200, 1, 1.05, 0.0, 0.50, 2.5, 0.83, 2.5, 4.00, 2, 0, 135 point.2=1, 1.41, 5.76, -6.55, 2200, 2, 1.05, 0.0, 0.50, 2.5, 0.83, 2.5, 8.25, 3, 0, 135 point.3=2, 0.00,-20.00, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5 point.4=2, 0.00, 20.00, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6 point.5=2, -20.25, 0.00, 1.00, 2400, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9 point.6=2, 2.41, 0.00, -2.08, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4 static_cg_height = 5.56 //(feet) altitude of CG when at rest (altitude when loaded on ground) static_pitch = 13.70 //degrees (pitch when loaded on ground) gear_system_type=1 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.125 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=14 // degrees, KIAS flaps-position.2=28 // degrees, KIAS flaps-position.3=42 // degrees, KIAS flaps-position.4=55 // degrees, KIAS damaging-speed=172 // KIAS blowout-speed=260 // KIAS [TailHook] tailhook_length=4 ;(feet) tailhook_position = -17.5, 0.0, -0.5 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust = 1.0 [Views] eyepoint=-2.27, 0.00, 2.9 [LIGHTS] panel=0.00, 0.35, -0.80, fx_vclight light.0=3, 0.40,-19.30, 0.70, fx_navred light.1=3, 0.40, 19.30, 0.70, fx_navgre light.2=3,-21.60, 0.00, 0.00, fx_navwhi [General] performance=Weight: 3,704 \/ 5,313 lbs\nEngine: Nakajima NK1C Sakae 12\n14-cyl. air-cooled radial, 950 hp\nMax speed: 331 mph @ 14,930 ft\nCeiling: 32,810 ft\nInitial climb rate: 4,517 ft\/min\nRange: 1,160 mi at 152 mph or\nwith drop tanks, 1,930 miles\n [fuel] Center1= 0.60, 0.00, 0.00, 38.30, 0.00 LeftMain= -1.60, 2.30,-1.20, 50.20, 0.00 RightMain=-1.60,-2.30,-1.20, 50.20, 0.00 External1=-2.10, 0.00,-3.30, 87.20, 0.00 fuel_type=1 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=230.00 wing_span=39.416667 wing_root_chord=8.50 wing_dihedral=6.998291 wing_incidence=0.999756 wing_twist=0.00 oswald_efficiency_factor=0.697175 wing_winglets_flag=0 wing_sweep=5.00 wing_pos_apex_lon=2.80 wing_pos_apex_vert=-1.00 htail_area=24.00 htail_span=15.40 htail_pos_lon=-13.50 htail_pos_vert=0.80 htail_incidence=-0.999756 htail_sweep=20.00 vtail_area=15.00 vtail_span=4.10 vtail_sweep=0.00 vtail_pos_lon=-14.80 vtail_pos_vert=1.70 elevator_area=13.00 aileron_area=20.400 rudder_area=13.0600 elevator_up_limit=26.000825 elevator_down_limit=26.000825 aileron_up_limit=21.497376 aileron_down_limit=20.345731 rudder_limit=28.997394 elevator_trim_limit=19.996227 spoiler_limit=0.00 spoilerons_available=0 aileron_to_spoileron_gain=0.00 min_ailerons_for_spoilerons=0.00 min_flaps_for_spoilerons=0.00 [brakes] toe_brakes_scale=0.48420 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.00 flap_limit_power=0.00 flap_limit_idle=0.00 [GeneralEngineData] engine_type=0 Engine.0=6.2500, 0.00, 0.00 fuel_flow_scalar=1.00 min_throttle_limit=0.00 [Reference Speeds] flaps_up_stall_speed=74.00 full_flaps_stall_speed=59.200 cruise_speed=152.00 max_indicated_speed=460.00 [keyboard_response] elevator=150.00,250.00 aileron= 150.00,250.00 rudder= 150.00,250.00 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=700.00 autothrottle_available=1 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=1.500 max_pitch_velocity_lo_alt_breakpoint=20000.00 max_pitch_velocity_hi_alt_breakpoint=28000.00 max_bank=25.00 max_bank_acceleration=1.800 max_bank_velocity=3.00 max_throttle_rate=0.100 nav_proportional_control=9.00 nav_integrator_control=0.2500 nav_derivative_control=0.00 nav_integrator_boundary=2.500 nav_derivative_boundary=0.00 gs_proportional_control=9.5200 gs_integrator_control=0.2600 gs_derivative_control=0.00 gs_integrator_boundary=0.700 gs_derivative_boundary=0.00 yaw_damper_gain=0.00 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=6.930556 [stall_warning] type=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0
