Rotating Detonation Combustion for Advanced Liquid Propellant Space Engines
Rotating (also termed continuous spin) detonation technology is gaining interest in the global research and development community due to the potential for increased performance. Potential performance benefits, thrust chamber design, and thrust chamber cooling loads are analyzed for propellant applic...
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| Principais autores: | , , , , , |
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| 格式: | Artigo |
| 語言: | Inglês |
| 出版: |
MDPI AG
2022-10-01
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| 叢編: | Aerospace |
| 主題: | |
| 在線閱讀: | https://www.mdpi.com/2226-4310/9/10/581 |
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