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PATR发动机关键技术与性能提升途径初探

  • Meng Zheng Zhang
  • , Dian Duo Liu
  • , Hai Bo Ma
  • , Guang Xi Li
  • , Xiang Yi Nan
  • Xi’an Aerospace Propulsion Institute

科研成果: 期刊稿件文章同行评审

14 引用 (Scopus)

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
39
9
DOI
出版状态已出版 - 1 9月 2018
已对外发布

关键词

  • Approach
  • Critical technology
  • Performance
  • Pre-cooling air turbo rocket

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