Exclusive: Advanced Combined Cycle Powered Vehicle

Future application of combined cycle propulsion technology

  • ZHANG Xuhui
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  • China Academy of Launch Vehicle Technology, Beijing 100076, China

Received date: 2019-11-01

  Revised date: 2020-03-21

  Online published: 2020-08-05

Abstract

Combined cycle propulsion combines two or more single types of power organically, with integrate each other in structure and complements each other in function, greatly expanding flight envelope and improving flight efficiency. It has important applications in near space hypersonic vehicle, reusable space transportation system and other fields. This paper introduces the basic classification and working principle of combined cycle propulsion, reviews the application of combined cycle propulsion technology in near space hypersonic vehicle and reusable space transportation system, and summarizes the development trend and main key technologies of combined cycle propulsion vehicle.

Cite this article

ZHANG Xuhui . Future application of combined cycle propulsion technology[J]. Science & Technology Review, 2020 , 38(12) : 15 -24 . DOI: 10.3981/j.issn.1000-7857.2020.12.002

References

[1] Chiesa S, Grassi M, Russo G, et al. A small-scale lowcost technology demonstrator of a reusable launch vehicle[C]//AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies. Capua:AIAA, 2005.
[2] Hank J M, Franke M E, Eklund D R. TSTO Reusable Launch Vehicles Using Airbreathing Propulsion[C]//42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Sacramento:AIAA, 2006.
[3] 王璐, 韩洪涛, 王友利. 2017年国外高超声速技术发展回顾[J]. 国际太空, 2018(3):41-45.
[4] 彭小波. 组合循环动力技术在天地往返领域的发展与应用[J]. 导弹与航天运载技术, 2013(1):78-82.
[5] 彭小波. 组合动力飞行器技术发展[J]. 导弹与航天运载技术, 2016(5):1-6.
[6] Foster R W, Escher W J D, Robinson J W, et al. Studies of an extensively axisymmetric rocket based combined cycle (RBCC) engine powered single-stage-to-orbit (SSTO) vehicle[C]//AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference. Monterey:AIAA, 1989.
[7] Snyder L E, Escher D W, DeFrancesco R L, et al. Turbine based combination cycle (TBCC) propulsion subsystem integration[C]//40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Fort Lauderdale:AIAA, 2004.
[8] Aggarwal R, Lakhara K, Sharma P B, et al. SABRE Engine:Single Stage to Orbit Rocket Engine[J]. International Journal of Innovative Research in Science, Engineering and Technology, 2015, 10(4):10360-10366.
[9] Ehrlich C F. Early studies of RBCC applications and lessons learned for today[C]//36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Huntsville:AIAA, 2000.
[10] Hyde E H, Escher W J D, Roddy J E. Marquardt's Mach 4.5 supercharged ejector ramjet high-performance aircraft engine project[C]//36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Huntsville:AIAA, 2000.
[11] Morris C E K. National Aero-Space Plane achievements and U.S. space-launch goals[C]//6th AIAA International Aerospace Planes and Hypersonics Technologies Conference. Chattanooga:AIAA, 1995.
[12] Burns B R A. HOTOL space transport for the twenty first century[J]. Proceedings of the Institute of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 1990, 204(2):101-110.
[13] Schaber R, Schwab R R. Hypersonic propulsion considerations for a flying testbed[C]//AIAA/ASME/SAE/ASEE 27th Joint Propulsion Conference. Sacramento:AIAA, 1991.
[14] Longstaff R, Bond A. The Skylon Project[C]//17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. San Francisco:AIAA, 2011.
[15] 张连庆, 刘博, 李浩悦."佩刀" 发动机技术进展分析[C]//中国航天第三专业信息网第三十八届技术交流会暨第二届空天动力联合会议. 大连, 2017.
[16] Hellman B M, Bradford J, St. Germain B, et al. Two stage to orbit conceptual vehicle designs using the SABRE engine[C]//SPACE Conferences and Exposition. Long Beach:AIAA, 2016.
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