Updated to match changes in radiostack.[ch]xx

[flightgear.git] / src / FDM / JSBSim / FGRocket.h

diff --git a/src/FDM/JSBSim/FGRocket.h b/src/FDM/JSBSim/FGRocket.h
index db4c2700fac3c550e3bc7ec47d128407fd5e15f5..58142fb494e4a00c07477b4b24e17feffe25ac58 100644 (file)
--- a/src/FDM/JSBSim/FGRocket.h
+++ b/src/FDM/JSBSim/FGRocket.h
@@ -94,6 +94,10 @@ CLASS DOCUMENTATION
     @see FGEngine
     @see FGPropulsion
     @see FGTank
+    @see <a href="http://cvs.sourceforge.net/cgi-bin/viewcvs.cgi/jsbsim/JSBSim/FGRocket.h?rev=HEAD&content-type=text/vnd.viewcvs-markup">
+         Header File </a>
+    @see <a href="http://cvs.sourceforge.net/cgi-bin/viewcvs.cgi/jsbsim/JSBSim/FGRocket.cpp?rev=HEAD&content-type=text/vnd.viewcvs-markup">
+         Source File </a>
 */
 
 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
@@ -116,20 +120,20 @@ public:
       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. */
-  float GetChamberPressure(void) {return PC;}
+  double GetChamberPressure(void) {return PC;}
 
 private:
-  float SHR;
-  float maxPC;
-  float propEff;
-  float kFactor;
-  float Variance;
-  float PC;
-  void Debug(void);
+  double SHR;
+  double maxPC;
+  double propEff;
+  double kFactor;
+  double Variance;
+  double PC;
+  void Debug(int from);
 };
 
 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%