Experimental Performance Analysis of a Toroidal Aerospike Nozzle Integrated with a N2O/HTPB Hybrid Rocket Motor
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
2010-01-01
Conference paper
Electronic Resource
English
DESIGN OF A N~20/HTPB HYBRID ROCKET MOTOR UTILIZING A TOROIDAL AEROSPIKE NOZZLE
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