// Give modifier for fuel burn rate -- 1.0 is full burn (multiplied by throttle to get thrust and true burn rate)
private float calculateFuelBurnMod(float altitude, float altitudeResiliency)
{
float resultMod = 0.0f;
currentAirDensity = air.getDensityAtAltitude(altitude);
float resil = Mathf.Clamp(1.0f - altitudeResiliency, 0.0f, 1.0f);
resultMod = Mathf.Pow(currentAirDensity, resil);
currentBurnMod = resultMod;
return(resultMod);
}