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