[fltsim.0]
title=Ki-43-IIb Oscar
sim=Ki43IIb_Oscar
model=
panel=
sound=
texture=
ui_manufacturer=Nakajima
ui_type=Ki-43-2B (Oscar)
ui_variation=Japanese Army
description=The Hayabusa (Peregrine falcon) was Japan's most numerous fighter. The army equivalent of the Mitsubishi Zero was even lighter and more maneuverable than its navy counterpart, and it shared many of the same strengths and weaknesses. 

[WEIGHT_AND_BALANCE]
empty_weight = 4211.0     // (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,   -1.3, 0.0, 2.0		//Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI = 4049.00  //slug-ft^2
empty_weight_roll_MOI  = 2586.00  //slug-ft^2
empty_weight_yaw_MOI   = 7230.00  //slug-ft^2
empty_weight_coupled_MOI=0.00
max_gross_weight=5710.00

[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=107.7800
compression_ratio=7.00
number_of_cylinders=14
max_rated_rpm=3000.00
max_rated_hp=1130.00
fuel_metering_type=2
cooling_type=0
normalized_starter_torque=0.03500
turbocharged=1
max_design_mp=45.67
min_design_mp=3.00
critical_altitude=11000.00
emergency_boost_type=2
emergency_boost_mp_offset=6.00
emergency_boost_gain_offset=0.3500
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=0.90

[propeller]
thrust_scalar = 1.0
propeller_type=0
propeller_diameter=11.00
propeller_blades=3
propeller_moi=44.45800
beta_max=65.00
beta_min=13.00
min_gov_rpm=1400.00
prop_tc=0.0100
gear_reduction_ratio=2.00
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
point.0=1, -18.80,   0.00, -3.05, 1600, 0, 0.30, 90.0, 0.30, 0.3, 0.80, 4.0, 3.0, 0
point.1=1,   2.14,  -5.62, -6.90, 2200, 1, 1.00,  0.0, 0.50, 1.0, 0.88, 6.5, 7.5, 2
point.2=1,   2.14,   5.62, -6.90, 2200, 2, 1.00,  0.0, 0.50, 1.0, 0.88, 5.0, 6.5, 3
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, -21.25,   0.00, -0.00, 1200, 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_pitch = 10.93     //degrees (pitch when loaded on ground)
static_cg_height = 6.11   //(feet) altitude of CG when at rest (altitude when loaded on ground)
gear_system_type=1

[Views]
eyepoint=-2.4, 0.0, 2.1  //(feet) longitudinal, lateral, vertical distance from reference datum




[General]
performance=Weight: 4,211 / 5,710 lbs Engine: Nakajima Sakae 21 14-cyl. radial air-cooled, 1,130 hp Max speed: 329 mph @ 13,125 ft Ceiling: 36,750 ft Initial climb rate: 3,250 ft/min Range: 1,095 miles or with drop tanks, 1,990 miles.

[fuel]
Center1=  1.00, 0.00,-1.00, 71.0, 0.00
Center2= -4.00, 0.00, 0.00, 25.0, 0.00
LeftMain= 0.00,-4.00,-1.00, 24.0, 0.00
RightMain=0.00, 4.00,-1.00, 24.0, 0.00
fuel_type=1
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area=230.00
wing_span=35.50
wing_root_chord=8.80
wing_dihedral=8.695679
wing_incidence=1.00
wing_twist=0.00
oswald_efficiency_factor=0.699052
wing_winglets_flag=0
wing_sweep=0.00
wing_pos_apex_lon=3.00
wing_pos_apex_vert=-1.30
htail_area=24.00
htail_span=14.60
htail_pos_lon=-17.10
htail_pos_vert=0.50
htail_incidence=-0.999756
htail_sweep=15.00
vtail_area=15.00
vtail_span=4.20
vtail_sweep=20.00
vtail_pos_lon=-17.30
vtail_pos_vert=1.20
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

[Flaps.0]
type=1
span-outboard=0.500
extending-time=5.00
system_type=1
flaps-position.0=0.00,0.00
flaps-position.1=10.007663,0.00
flaps-position.2=20.015326,0.00
flaps-position.3=30.022988,0.00

[GeneralEngineData]
engine_type=0
Engine.0=8.00, 0.00, 0.00
fuel_flow_scalar=0.50
min_throttle_limit=0.00

[Reference Speeds]
flaps_up_stall_speed=81.00
full_flaps_stall_speed=64.800
cruise_speed=200.00
max_indicated_speed=460.00
//Max_level_speed=290.0  (329 mph)

[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=1000.00
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=0.250
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

[LIGHTS]
panel=0.00, 0.15, -0.80, fx_vclight

light.0=3,  1.00, -18.80, 0.00, fx_navred
light.1=3,  1.00,  18.80, 0.00, fx_navgre
light.2=3,-20.70,   0.00, 5.40, fx_navwhi


[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