Volume 31 Issue 04
Apr.  2005
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Guo Hongjie, Liang Guozhu, Ma Bin, et al. Preliminary investigation on detonation wave ignition technique[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(04): 375-380. (in Chinese)
Citation: Guo Hongjie, Liang Guozhu, Ma Bin, et al. Preliminary investigation on detonation wave ignition technique[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(04): 375-380. (in Chinese)

Preliminary investigation on detonation wave ignition technique

  • Received Date: 17 Oct 2003
  • Publish Date: 30 Apr 2005
  • The relative merits of several ignition techniques of liquid propellant rocket engine were analyzed. The feasibility of each ignition technique applicable to multi-chamber multi-run ignition system of future advanced propulsion system was discussed. The structural configurations of application scenarios of ignition techniques were considered. Preliminary investigation on detonation wave ignition technique was made and a simplified theoretically analytical model for the mixture of gaseous hydrogen and gaseous oxygen was established. The applicable schemes of the detonation wave ignition for liquid rocket engine were analyzed. The analysis results show that the detonation wave technique can product high pressure ratio and high temperature ratio by low pressure premix detonative gases. The detonation wave propagates with high mach number, and the detonation wave ignition source arrives each ignition place immediately. The detonation wave ignition technique has unique synchronic characteristic and simple structural configuration. It is suitable to multi-chamber multi-run synchronic ignition of liquid propellant rocket engine.

     

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  • [1] urawski R L, Green J M. Catalytic ignition of hydrogen and oxygen propellants . AIAA-88-3300,1988 [2] Fuller P N. Advanced ignition systems final report . NASA N71-35152, NASA-CR-119928,1971 [3] 森元. 氢氧火箭发动机及其低温技术[M]. 北京:国防工业出版社,1995 Zhu Senyuan. Hydrogen/oxygen rocket engine and low temperature technology[M]. Beijing:National Defense Industry Press,1995 (in Chinese) [4] mmich H, Caporicci M. Status of the FESTIP rocket propulsion technology programme . AIAA-97-3311,1997 [5] 国舟,童晓艳,梁国柱,等. 液体火箭发动机气动谐振点火技术的研究 . 宇航学报,2001,22(4):81~84 Zhang Guozhou, Tong Xiaoyan, Liang Guozhu, et al. Investigation on gas dynamic resonance ignition technology for liquid propellant rocket engine[J]. Journal of Astronautics, 2001, 22(4):81~84(in Chinese) [6] 国柱,马 彬,张国舟,等. 气动谐振点火技术研究[J]. 推进技术,2001,22(4):286~289 Liang Guozhu, Ma Bin, Zhang Guozhou, et al. Investigation on gas dynamic resonance tube ignition method[J]. Journal of Propulsion Technology, 2001, 22(4):286~289 (in Chinese) [7] tabinsky L. Analytical and experimental study of resonance ignition tubes . NASA N74-17646,1973 [8] Bollinger L, Fong M, Edse R. Experimental measurements and theoretical analysis of detonation induction distances[J]. ARS Journal, 1961,31(5):588~595 [9] 晓艳,张国舟,马 彬,等. 多推力室的气动谐振点火器研究[J]. 推进技术,2002,23(5):402~405 Tong Xiaoyan, Zhang Guozhou, Ma Bin, et al. Research on gas dynamic resonace igniters of multi-thruster [J]. Journal of Propulsion Technology, 2002,23(5):402~405 (in Chinese) [10] 一白,刘 宇,覃粒子,等. 气氧酒精多管点火器试验研究[J]. 北京航空航天大学学报,2003,29(1):54~58 Wang Yibai, Liu Yu, Qin Lizi, et al. Experimental studies on gas-oxygen/alcohol multi-pipe igniter[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003,29(1):54~58 (in Chinese) [11] iou L C. Combustion-wave ignition for rocket engines . NASA 92-20043,1992 [12] Lockheed Martin. Allied Signal Aerospace, Rocketdyne. X-33 Phase II annual performance report . NASA-CR-205695,1997 [13] Walter S K. Research & technology 1998 . NASA TM-1999-208815, 1999 [14] 红杰,梁国柱,马 彬,等. 爆震波点火技术基本特性实验[J]. 推进技术,2005,26(1):76~79 Guo Hongjie, Liang Guozhu, Ma Bin, et al. Preliminary experimental investigation on detonation wave ignition technique[J]. Journal of Propulsion Technology,2005, 26(1):76~79(in Chinese) [15] 红杰,梁国柱,马 彬,等. 爆震波多管点火技术试验测试研究 . 见:第五届海内外华人航天科技研讨会 . 西安,2004 Guo Hongjie, Liang Guozhu, Ma Bin. et al. Experimental testing investigation on detonation wave ignition technique . In:The 5th Global Chinese Symposium on Space Science and Technique . Xian, 2004(in Chinese) [16] enner S S,Williams F A. Detonation and two phase flow[M]. New York:Academic Press, 1962. 47~63
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