N2O-Cooled Aerospike for a Hybrid Rocket Motor: Nitrous Oxide Characterization and Additive Manufacturing
53rd AIAA/SAE/ASEE Joint Propulsion Conference
2017-01-01
Conference paper
Electronic Resource
English
British Library Conference Proceedings | 2017
|Restartable Hybrid Rocket Motor using Nitrous Oxide
AIAA | 2006
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