[fltsim.0] title=A6M5 Zero sim=A6M5_Zero model= panel= sound= texture= KB_checklists=a6m5_zero_check ui_manufacturer=Mitsubishi ui_type=A6M5 Zero ui_variation=Japanese Navy description=The Japanese Navy had been flying this improved version of the Zero since late 1943. Its added horsepower, speed, and armament made it even more dangerous than the A6M2. Its slightly smaller, thicker-skinned wing gave it better diving qualities, but it still suffered from some of the A6M2's old problems. While slightly more maneuverable than a Hellcat at low to medium speeds, it was still lightly built and more vulnerable to battle damage than the Grumman. [WEIGHT_AND_BALANCE] empty_weight = 4136 // (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 = 4155.77 empty_weight_roll_MOI = 2615.22 empty_weight_yaw_MOI = 7824.54 empty_weight_coupled_MOI=0.00 max_gross_weight=6459.00 [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=125.8600 compression_ratio=7.00 number_of_cylinders=14 max_rated_rpm=2600.00 max_rated_hp=1130.00 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.03500 turbocharged=1 max_design_mp=43.70 min_design_mp=1.00 critical_altitude=20000.00 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=1.130 idle_rpm_mechanical_efficiency_scalar=1.00 max_rpm_friction_scalar=1.00 idle_rpm_friction_scalar=0.70 [propeller] thrust_scalar = 1.0 propeller_type=0 propeller_diameter=10.062500 propeller_blades=3 propeller_moi=26.74500 beta_max=49.00 beta_min=29.00 min_gov_rpm=1400.00 prop_tc=0.0100 gear_reduction_ratio=1.71400 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, -1.55, 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, -6.60, 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, -6.60, 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 = 5.60 //(feet) altitude of CG when at rest (altitude when loaded on ground) static_pitch = 13.97 //degrees (pitch when loaded on ground) gear_system_type=1 [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 [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=175 // KIAS blowout-speed=265 // KIAS [Views] eyepoint=-2.5,0.000000,2.4 [LIGHTS] panel=0.00, 0.30, -0.80, fx_vclight //light.0=3, -0.50,-18.10, 0.70, fx_navred //light.1=3, -0.50, 18.10, 0.70, fx_navgre light.0=3, 0.30, -17.80, 0.70, fx_navred light.1=3, 0.30, 17.80, 0.70, fx_navgre light.2=3,-21.60, 0.00, 0.00, fx_navwhi [General] performance=Weight: 4,136 \/ 6,025 lbs\nEngine: Nakajima NK1F Sakae 21\n14-cyl. air-cooled radial, \n1,130 hp \nMax speed: 351 mph @ 19,685 ft\nCeiling: 38,520 ft\nInitial climb rate: 3,150 ft\/min\nRange: 1,194 miles or\nwith drop tanks, 2,000 miles\n [fuel] Center1= 0.600, 0.000, 0.00, 15.80, 0.00 LeftMain= -1.600,-2.300,-1.20, 58.10, 0.00 LeftAux= -1.300,-9.800,-0.50, 10.60, 0.00 RightMain=-1.600, 2.300,-1.20, 58.10, 0.00 RightAux= -1.300, 9.800,-0.50, 10.60, 0.00 External1=-2.100, 0.000,-3.30, 87.20, 0.00 fuel_type=1 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=229.00 wing_span=36.00 wing_root_chord=8.20 wing_dihedral=6.998291 wing_incidence=0.999756 wing_twist=0.00 oswald_efficiency_factor=0.762605 wing_winglets_flag=0 wing_sweep=5.00 wing_pos_apex_lon=2.50 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=4.0 vtail_sweep=20.00 vtail_pos_lon=-14.60 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=250.00 max_indicated_speed=760.500 [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=0 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=1.500000 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 [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
