Propellant Feeding System of a Liquid Rocket With Multiple Engines
Multiengine first stages are the new trend in recent rockets. Reusability and an oxygen/methane based engine complete this picture. ArianeGroup wants to develop its own rocket following these principles. This thesis presents the study of the feeding system for a seven Prometheus engine rocket. Sever...
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| Format: | Others |
| Language: | English |
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KTH, Rymdteknik
2020
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-276460 |