@param pe nozzle exit pressure
@return thrust coefficient times chamber pressure */
float Calculate(float pe);
+
+ /** Gets the chamber pressure.
+ @return chamber pressure in psf. */
+ float GetChamberPressure(void) {return PC;}
private:
float SHR;
float propEff;
float kFactor;
float Variance;
+ float PC;
void Debug(void);
};