آناليز پايداري مخروطي راكتهاي دوار با تقارن محوري و راستاي نيروي جلوبرنده دلخواه همراه با جرم مستهلك كننده

Coning instability will be analyzed for a spinning axisymmetric rocket with general thrust direction and dissipative internal mass motion. This is a better analysis and simulation for the Slag hypothesis. In dynamical analysis, the stability zones are determined and the rocket system performance is simulated.