In Silico Studies on Truncated Aerospike Nozzle with Optimum Cowl Length for Single Stage to Orbit Vehicles
25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
01.01.2023
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Assessment of Aerospike Nozzle for Single-Stage to Orbit Flight (AIAA 2015-3979)
British Library Conference Proceedings | 2015
|British Library Conference Proceedings | 1999
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