Design and Experimental Investigation on Gas Oxygen/Kerosene Ejector Rocket for RBCC Application
The ejector rocket is one of the core components of the rocket based combined cycle propulsion system, and must be capable of variable working conditions. In order to meet technical requirements for RBCC application, the variable duty operating ejector rocket using the gas Oxygen/Kerosene was design...
| Format: | Article |
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| Language: | zho |
| Published: |
EDP Sciences
2018-06-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/pdf/2018/03/jnwpu2018363p558.pdf |