N2O-Cooled Aerospike for a Hybrid Rocket Motor: Nitrous Oxide Characterization and Additive Manufacturing (AIAA 2017-4979)
Joint propulsion conference
01.01.2017
17 pages
Aufsatz (Konferenz)
Englisch
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Nitrous Oxide Hybrid Rocket Motor Fuel Regression Rate Characterization AIAA Paper
British Library Conference Proceedings | 2007
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