Computation of Nozzle Flow in a N2O/HTPB Hybrid Rocket Motor
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
2007-01-01
Conference paper
Electronic Resource
English
Computation of Nozzle Flow in a N2O/HTPB Hybrid Rocket Motor AIAA Paper
British Library Conference Proceedings | 2007
|DESIGN OF A N~20/HTPB HYBRID ROCKET MOTOR UTILIZING A TOROIDAL AEROSPIKE NOZZLE
British Library Conference Proceedings | 2010
|Development of a N2O/HTPB hybrid rocket motor
AIAA | 1997
|Design of a small H2O2/HTPB hybrid sounding rocket motor
AIAA | 1996
|