// GENERAL
maxSpeed=800;
enginePower=1.193;
landingAOA=__EVAL(3*3.1415/180);
landingSpeed=215;
stallSpeed=148;
stallWarningTreshold=0.1;
wheelSteeringSensitivity=1.5;
airBrake=1;
airBrakeFrictionCoef=2.5;
flaps=1;
flapsFrictionCoef=0.32;
gearsUpFrictionCoef=0.6;
airFrictionCoefs0[]=
{
	0.0,0.0,0.0
};
airFrictionCoefs1[]=
{
	0.1,0.5,0.0066
};
airFrictionCoefs2[]=
{
	0.001,0.005,0.000068
};
angleOfIndicence=__EVAL(-2*3.1415/180);
envelope[]=
{
	0.00,0.05,0.60,0.90,1.40,1.80,2.10,2.40,2.88,3.65,4.50,5.45,6.48,7.61,8.10,8.30,8.40,8.30,8.00,7.60,7.00
}; 
altNoForce=11000;
altFullForce=2500;
thrustCoef[]=
{
	1.22,1.28,1.34,1.35,1.35,1.4,1.49,1.01,0.57,0.37,0.26,0.16,0.10,0.00,0.00,0.00,0.00
};
aileronSensitivity=0.7;
aileronCoef[]=
{
	0,0.11,0.445,0.81,1.0,1.05,1.1,1.15,1.2,1.3,1.3,1.33,1.35,1.34,1.29,1.2,0.800
};
elevatorSensitivity=0.85;
elevatorCoef[]=
{
	0,0.14,0.54,0.62,0.588,0.56,0.54,0.52,0.489,0.430,0.38,0.35,0.300,0.25,0.2,0.150,0.1
};
rudderInfluence=0.95;
rudderCoef[]=
{
	0.00,0.89,1.50,2.10,2.50,3.00,3.60,3.90,4.00,3.60,1.80
};
aileronControlsSensitivityCoef= 3.6;
elevatorControlsSensitivityCoef=2.0;
rudderControlsSensitivityCoef=3.8;
draconicForceXCoef=12.0;
draconicForceYCoef=1.0;
draconicForceZCoef=1.0;
draconicTorqueXCoef[]=
{
	4.8,5,5.5,6.2,7,7.7,9.4,11.1,12,14,15
};
draconicTorqueYCoef[] =
{
	12,10,6,2,0.2,0,0,0,0,0,0,0,0,0,0,0,0
};