public void CalculateConstants(CelestialBody body, float speed, double altitude)
{
double atmosphereTemperatureOffset = 0;
atmoTemp = body.GetFullTemperature(altitude, atmosphereTemperatureOffset);
density = body.GetDensity(staticPressurekPa, atmoTemp);
mach = CalculateMachNumber(body, speed, staticPressurekPa, density);
staticPressurekPa = body.GetPressure(altitude);
convectiveMachScale = Math.Pow(UtilMath.Clamp01(
(mach - PhysicsGlobals.NewtonianMachTempLerpStartMach) / (PhysicsGlobals.NewtonianMachTempLerpEndMach - PhysicsGlobals.NewtonianMachTempLerpStartMach)),
PhysicsGlobals.NewtonianMachTempLerpExponent);
}
