[fltsim.0]
title=P40 Tomahawk
sim=P40STUD
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=CURTISS
ui_type=P-40B
ui_variation=Tamahawk
description=P-40B Tomahawk USAAC flown by George Welch, 1 of 2 P-40's that made it into the air during the attack at Pearl Harbor on Dec. 7th, 1941
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.1]
title=P40B Flying Tiger
sim=P40STUD
model=
panel=
sound=
texture=tiger
kb_checklists=
ui_manufacturer=CURTISS
ui_type=P-40B Flying Tiger
ui_variation=Flying Tiger
description=Early Pacific Theatre of Operations "Screamin Demons 7th" of the 7th Air Force
Based in Micronesia. 1941
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.2]
title=P40 KittyHawk
sim=P40STUD
model=
panel=
sound=
texture=Kitty
kb_checklists=
ui_manufacturer=CURTISS
ui_type=P-40 KittyHawk
ui_variation=KittyHawk
description=Flown By the RAAF during the Defense of Australia from Japanese invading Forces in WW II
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[fltsim.3]
title=P40N Pink Lady
sim=P40STUD
model=
panel=
sound=
texture=Pink
kb_checklists=
ui_manufacturer=CURTISS
ui_type=P-40N
ui_variation=Pink Lady
description=This Was actually Tan, only to be faded to Pink
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=

[WEIGHT_AND_BALANCE]
empty_weight= 6300.000

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= 7856.000
empty_weight_roll_MOI= 6245.000
empty_weight_yaw_MOI= 10254.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 8238.800
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= 138.000
compression_ratio= 6.100
number_of_cylinders= 12
max_rated_rpm= 3000.000
max_rated_hp= 1300.000
fuel_metering_type= 0
cooling_type= 1
normalized_starter_torque= 0.035
turbocharged= 1
max_design_mp= 54.000
min_design_mp= 1.000
critical_altitude= 24000.000
emergency_boost_type= 3
emergency_boost_mp_offset= 10.000
emergency_boost_gain_offset= 0.800
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[propeller]
thrust_scalar=1.0                       ;Percent per second
propeller_type= 0
propeller_diameter= 11.500
propeller_blades= 3
propeller_moi= 39.920
beta_max= 65.000
beta_min= 23.000
min_gov_rpm= 1800.000
prop_tc= 0.010
gear_reduction_ratio= 2.237
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, -15.710, 0.000, -3.105, 3200.000, 0.000, 0.380, 45.000, 0.450, 2.500, 0.900, 1.000, 4.000, 0.000, 200.000, 673.424
point.1= 1.000, 2.290, -4.420, -8.050, 2200.000, 1.000, 1.350, 0.000, 0.800, 2.500, 0.660, 5.500, 6.500, 2.000, 200.000, 721.524
point.2= 1.000, 2.290, 4.420, -8.050, 2200.000, 2.000, 1.350, 0.000, 0.800, 2.500, 0.660, 5.500, 5.000, 3.000, 200.000, 721.524
point.3= 2.000, 1.079, -19.300, 0.000, 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, 1.079, 19.300, 0.000, 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, -18.250, 0.000, -0.910, 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, 5.410, 0.000, -6.200, 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= 8.050
static_pitch= 12.300
gear_system_type=1


[Views]
eyepoint=-2.80,0.0,1.80


[LIGHTS]
panel=0.00, 0.45, -2.00, fx_vclight

[General]
performance=P-40F Specifications\nSpan\t37 ft  4 in\nLength\t33 ft  4 in\nHeight\t12 ft  4 in\nWing Area\t236 sq ft\nEmpty Weight  6,590 lb\nLoaded Weight  9,350 lb\nMax. Speed 364 mph\nCruise Speed 290 mph\nCeiling 33,500 ft\nRate of Climb 3,250 fpm\nRange 575 miles\nPowerplant Packard V-1650-1 of 1,300 hp
atc_type=
atc_model=

[fuel]
Center1= 1.000, 0.000, -1.000, 71.300, 0.000
Center2= -4.000, 0.000, 0.000, 68.700, 0.000
LeftMain= 0.000, -4.000, -1.000, 24.600, 0.000
RightMain= 0.000, 4.000, -1.000, 24.600, 0.000
External1= 0.000, 0.000, -4.000, 105.600, 0.000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area= 253.000
wing_span= 39.333
wing_root_chord= 6.417
wing_dihedral= 8.696
wing_incidence= 1.000
wing_twist= 0.000
oswald_efficiency_factor= 0.699
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= 5.417, 0.000, 0.000
fuel_flow_scalar= 1.000
min_throttle_limit=0.000000

[Reference Speeds]
flaps_up_stall_speed= 81.000
full_flaps_stall_speed= 64.800
cruise_speed= 251.933
max_indicated_speed=740.000000

[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[direction_indicators]
direction_indicator.0=1,0

[Flaps.0]
type= 1
span-outboard= 0.125
extending-time= 5.000
system_type= 0
damaging-speed= 203.000
blowout-speed= 307.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 30.000, 0.000

[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[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