Research and development of rotating detonation engine system for the sounding rocket flight experiment S520-31
Clicks: 211
ID: 34632
2019
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| Reference Key |
kasahara2019researchaip
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|---|---|
| Authors | Kasahara, J. |
| Journal | AIP Conference Proceedings |
| Year | 2019 |
| DOI |
10.1063/1.5115842
|
| URL | |
| Keywords | Keywords not found |
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