[fltsim.0]
title=Curtiss P-40N 15000 th
sim=P-40n
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=
atc_id_color=0xffffffff
ui_manufacturer=Curtiss
ui_type=P-40N
ui_variation=15.000 th aircraft
description= Aircraft by Krzysztof Malinowski kmalin@lodz.mm.pl, repaint Jindrich Barta bartajindrich@seznam.cz

[WEIGHT_AND_BALANCE]
empty_weight=6200                       // (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 =  6181.10
empty_weight_roll_MOI  =  4396.69
empty_weight_yaw_MOI   =  8475.84



[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

[propeller]
thrust_scalar=1.0                       ;Percent per second

[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, -15.71, 0.0, -3.05, 3200.000, 0.000, 0.380, 45.000, 0.450, 2.500, 0.900, 1.000, 4.000, 0.000, 200.000, 398.935
point.1=1.000, 2.290, -4.420, -7.950, 2200.000, 1.000, 1.350, 0.000, 0.640, 2.500, 0.860, 5.500, 6.500, 2.000, 200.000, 427.429
point.2=1.000, 2.290, 4.420, -7.950, 2200.000, 2.000, 1.350, 0.000, 0.640, 2.500, 0.860, 5.500, 5.000, 3.000, 200.000, 427.429
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=7.650
static_pitch=12.300


[Views]
eyepoint=-3.10,0.0,1.85


[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=10					// degrees, KIAS
flaps-position.2=20					// degrees, KIAS
flaps-position.3=30					// degrees, KIAS
damaging-speed=203					// KIAS
blowout-speed=307					// KIAS


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