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火箭基组合循环(RBCC)推进系统研究现状 被引量:9

Research status about rocket based combined cycle (RBCC) propulsion system
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摘要 对火箭基组合循环(RBCC)推进系统基本概念进行了介绍,并就此项技术在美国的研究现状做了比较详细的综述,指出了发展这种新型推进装置的关键技术,对国内在这方面的研究思路提出了建议。 The general conception of rocket based combined cycle (RBCC)is introduced , and the research status about it in American is described in more detail. And the key technologies of this kind of propulsion system is pointed out. Finally, the development suggestion about RBCC in China is put forwards.
出处 《固体火箭技术》 EI CAS CSCD 北大核心 2003年第3期1-3,6,共4页 Journal of Solid Rocket Technology
关键词 可重复使用航天器 火箭基组合循环推进系统 组合式发动机 现状 reusable space craft composite engine rocket based combined cycle
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参考文献16

  • 1Foster R, Escher W and Robinson J. Studies of an extensively asymmetric rocket based combined cycle (RBCC) engine powered SSTO vehicle[ R]. AIAA Paper 89-2294.
  • 2Carl F Ehrlich, Jr. Early studies of RBCC applications and lessons learned for today[ R]. AIAA Paper 2000-3105.
  • 3Hyde E H, Escher W J D and Roddy J E. Marquardt's Mach 4.5 supercharged ejector ramjet high-performance aircraft engine project[ R]. AIAA Paper 2000-3109.
  • 4Uwe Hueter, Jim Turner. Rocket based combined cycle activities in the advanced space transportation program office[ R]. AIAA Paper 99-2353.
  • 5Dalnes R L, Merlde C L. Computational fluid dynamic modeling of rocket based combined cycle engine flowflelds[ R].MAA Paper 94-3327.
  • 6Lehman M, Pal S, Broda J C and Santoro R J. Raman spectroscopy based study of RBCC ejector mode performance[ R]. AIAA Paper 99-0090.
  • 7Ruf J H. Benchmark of FDNS CFD ,code for direct connect RBCC test data[ R]. MAA Paper 2000- 3726.
  • 8Muller S, Clark Hawk W, Bakker P G, Parklnson D and Turner M. Mixing d supersonic jets in a RBCC strutjet propulsion system[ R]. AIAA Paper 99-2973.
  • 9Foelsche R O, Tsai C Y and Bakos R J. Experiments on a RBCC ejector scramjet with integrated, staged secondary-fuel injection[ R]. AIAA Paper 99-2242.
  • 10Matthew R Russell, Douglas Brocco S and Russell Daines L. Modeling and validation of an ejector primary rocket for shielded afterburnlng fuel injecion [ R ]. AIAA Paper 99-2241.

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