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
2023-01-01
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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