A Fundamental Study of a End-Burning Swirling-Flow Hybrid Rocket Engine using Low Melting Temperature Fuels (AIAA 2015-4138)
Joint propulsion conference
2015-01-01
8 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2016
|Scaling of Hybrid Rocket Motors with Swirling Oxidizer Injection (AIAA 2015-3833)
British Library Conference Proceedings | 2015
|British Library Conference Proceedings | 2015
|