Numerical Study of the Working Process in the Reducing Gas Generator of the Upper Stage Oxygen - Methane Engine
This article deals with the problems of creating a reducing gas generator of the liquid rocket engine (LRE) of upper stage using advanced fuel components, namely oxygen + liquid natural gas. Relevance of the work is justified by the need to create and develop of environmentally friendly missile syst...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | Russian |
| Published: |
MGTU im. N.È. Baumana
2016-06-01
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| Series: | Aèrokosmičeskij Naučnyj Žurnal |
| Subjects: | |
| Online Access: | https://aerospace.elpub.ru/jour/article/view/25 |