[fltsim.0]
title=A6M5 Zero Model 52 Fighter/Bomber
sim=A6M5_Zero
model=
panel=
sound=
texture=
KB_checklists=a6m5_zero_check
description=The Japanese Navy had been flying this improved version of the Zero since late 1943. \nThis aircraft was part of the " Shikishima-Tai" the first Kamikaze unit, Philippines 25 October 1944
ui_manufacturer=WW2
ui_type=A6M5 Zero Model 52 Fighter/Bomber
ui_variation=Fighter/Bomber of the 301st Hikotaki
atc_heavy=0
atc_id=02 112
atc_airline=Zero
atc_flight_number=

[WEIGHT_AND_BALANCE]
empty_weight= 4136.000

reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000

max_number_of_stations=50

station_load.0= 170.000, -3.000, 0.000, 3.000

;Moments of Inertia
empty_weight_pitch_MOI= 4155.770
empty_weight_roll_MOI= 2615.220
empty_weight_yaw_MOI= 5324.540
empty_weight_coupled_MOI= 0.000
max_gross_weight= 5748.400
CG_forward_limit= 0.000
CG_aft_limit= 1.000


[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= 125.860
compression_ratio= 7.000
number_of_cylinders= 14
max_rated_rpm= 2600.000
max_rated_hp= 1130.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.035
turbocharged= 1
max_design_mp= 43.700
min_design_mp= 1.000
critical_altitude= 20000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar= 1.000
idle_rpm_mechanical_efficiency_scalar= 1.000
max_rpm_friction_scalar= 1.000
idle_rpm_friction_scalar= 1.000

[propeller]
thrust_scalar=1.0
propeller_type= 0
propeller_diameter= 10.063
propeller_blades= 3
propeller_moi= 26.745
beta_max= 49.000
beta_min= 29.000
min_gov_rpm= 1400.000
prop_tc= 0.010
gear_reduction_ratio= 1.714
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather= 0.000
power_absorbed_cf= 0.000
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000

[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= 1.000, -20.210, 0.000, -1.550, 3200.000, 0.000, 0.300, 180.000, 0.400, 2.500, 0.800, 7.500, 5.000, 0.000, 0.000, 1850.414
point.1= 1.000, 1.410, -5.760, -6.600, 2200.000, 1.000, 1.050, 0.000, 0.500, 2.500, 0.830, 2.500, 4.000, 2.000, 0.000, 1850.414
point.2= 1.000, 1.410, 5.760, -6.600, 2200.000, 2.000, 1.050, 0.000, 0.500, 2.500, 0.830, 2.500, 8.250, 3.000, 0.000, 1850.414
point.3= 2.000, 0.000, -20.000, -1.250, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, 0.000, 20.000, -1.250, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -20.250, 0.000, 1.000, 2400.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 2.410, 0.000, -2.080, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_cg_height= 5.600
static_pitch= 13.970

[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=-2.5,0.000000,2.4

[LIGHTS]
panel=0.00, 0.30, -0.80, fx_vclight

[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
atc_type=Zero
atc_model=Zero
[fuel]
Center1= 0.600, 0.000, 0.000, 15.800, 0.000
LeftMain= -1.600, -2.300, -1.200, 58.100, 0.000
LeftAux= -1.300, -9.800, -0.500, 10.600, 0.000
RightMain= -1.600, 2.300, -1.200, 58.100, 0.000
RightAux= -1.300, 9.800, -0.500, 10.600, 0.000
External1= -2.100, 0.000, -3.300, 87.200, 0.000
fuel_type= 1.000
number_of_tank_selectors= 1
[airplane_geometry]
wing_area= 209.000
wing_span= 36.083
wing_root_chord= 6.417
wing_dihedral= 6.998
wing_incidence= 1.000
wing_twist= 0.000
oswald_efficiency_factor= 0.763
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 24.000
htail_span= 11.000
htail_pos_lon= -18.833
htail_pos_vert= 0.000
htail_incidence= -1.000
htail_sweep= 0.000
vtail_area= 15.000
vtail_span= 4.416
vtail_sweep= 0.000
vtail_pos_lon= -18.833
vtail_pos_vert= 0.583
elevator_area= 13.000
aileron_area= 20.400
rudder_area= 13.060
elevator_up_limit= 26.001
elevator_down_limit= 26.001
aileron_up_limit= 21.497
aileron_down_limit= 20.346
rudder_limit= 28.997
elevator_trim_limit= 19.996
spoiler_limit= 0.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000
[GeneralEngineData]
engine_type= 0
Engine.0= 6.250, 0.000, 0.000
fuel_flow_scalar= 1.000
[Reference Speeds]
flaps_up_stall_speed= 74.000
full_flaps_stall_speed= 59.200
cruise_speed= 252.980
[keyboard_response]
elevator= 350.000, 500.000
aileron= 450.000, 1000.000
rudder= 200.000, 1000.000
[autopilot]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 700.000
autothrottle_available= 0
pitch_takeoff_ga= 8.000
[direction_indicators]
direction_indicator.0=1,0
[Flaps.0]
type= 1
span-outboard= 0.125
extending-time= 5.000
system_type= 0
damaging-speed= 175.000
blowout-speed= 265.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 14.000, 0.000
flaps-position.2= 28.000, 0.000
flaps-position.3= 42.000, 0.000
flaps-position.4= 55.000, 0.000