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...
Αποθηκεύτηκε σε:
| Κύριοι συγγραφείς: | , , , , , |
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| Μορφή: | Artigo |
| Γλώσσα: | Inglês |
| Έκδοση: |
MDPI AG
2022-10-01
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| Σειρά: | Aerospace |
| Θέματα: | |
| Διαθέσιμο Online: | https://www.mdpi.com/2226-4310/9/10/581 |
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