摘要
PATR engine is a combined propulsion system which aims at high speed delivery platform in near space and TSTO horizontal take-off launcher. Because of wide working range, less modal conversion, high thrust weight ratio and superior performance, PATR is a important research direction of combined cycle. The PATR propulsion system and it’s characteristic are introduced, the critical technologies affecting system development are analyzed, including system design, efficient heat transfer, high performance turbomachinery, materials and processes. On this basis, the ways to improve the performance are proposed, such as optimizing system scheme and component parameters.
| 投稿的翻译标题 | Preliminary Analysis on Critical Technology and Performance Improvement of PATR Engine |
|---|---|
| 源语言 | 繁体中文 |
| 页(从-至) | 1921-1927 |
| 页数 | 7 |
| 期刊 | Tuijin Jishu/Journal of Propulsion Technology |
| 卷 | 39 |
| 期 | 9 |
| DOI | |
| 出版状态 | 已出版 - 1 9月 2018 |
| 已对外发布 | 是 |
关键词
- Approach
- Critical technology
- Performance
- Pre-cooling air turbo rocket
学术指纹
探究 'PATR发动机关键技术与性能提升途径初探' 的科研主题。它们共同构成独一无二的指纹。引用此
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