N2O-HTPB Hybrid Rocket Combustion Modeling with Mixing Enhancement Designs
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
2013-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Numerical Modeling of Hybrid N2O-HTPB Combustion with Mixing Enhancers
British Library Conference Proceedings | 2013
|Combustion performance and scale effect from N2O/HTPB hybrid rocket motor simulations
Online Contents | 2013
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