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《Journal of Astronautics》 2001-04
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INVESTIGATION ON THE IGNITION METHODS OF AEROSPIKE NOZZLE ENGINE

Tong Xiaoyan Ma Bin Zhang Guozhou (Beijing University of Aeronautics and Astronautics,Beijing 100083)  
The ignition system of aerospike nozzle engine should provide sufficient ignition source for more than ten segmented small combustors simultaneously and sustain combustion after the injection of main propellant.This paper suggests three ignition methods for aerospike nozzle engine.Combustion wave ignition system can provide the ignition of aerospike nozzle engine under the condition of little electric energy input,while gas dynamic resonance ignition system can ignite the aerospike nozzle engine without external energy.The torch produced by using spark plug to ignite small combustion chamber also can realize this goal with the advantage of adequate practical experience.Finally,this paper provides the experimental data and technological methods of using gas dynamic resonance igniter to ignite the aerospike nozzle engine.
【Fund】: 863基金资助项目
【CateGory Index】: V432
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【References】
Chinese Journal Full-text Database 4 Hits
1 Yu Nanjia Zhang Guozhou Ma Bin (School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China);Investigation on methods of kerosene/oxygen ignition using gas dynamic resonance technique[J];Journal of Beijing University of Aeronautics and Astronautics;2003-09
2 Yu Nanjia Zhang Guozhou Song Yana(School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China) Cheng Shengqing(Beijing Aerospace Propulsion Institute, Beijing 100074, China);Research on synchronistic multi-ignitions of hydrogen-oxygen resonance ignitor[J];Journal of Beijing University of Aeronautics and Astronautics;2005-06
3 Song Yana Zhang Guozhou (School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China) Zhou Wenlu Huang Xiang (Beijing Aerospace Propulsion Institute, Beijing 100076, China);Investigation on head of novel chemical thruster for orbit maneuver[J];Journal of Beijing University of Aeronautics and Astronautics;2005-08
4 TONG Xiaoyan, ZHANG Guozhou, MA Bin, LIANG Guozhu, SONG Yana(School of Astronautics, Beijing Univ of Aeronautics and Astronautics, Beijing 100083,China);Research on gas dynamic resonance igniters of multithruster[J];Journal of Propulsion Technology;2002-05
【Co-references】
Chinese Journal Full-text Database 7 Hits
1 Liang Guozhu Zhang Zhenpeng Zhang Guozhou Cheng Xianchen (Beijing University of Aeronautics and Astronautics,School of Astronautics);Numerical Investigation of Gas Dynamic Resonance Tube Heating[J];JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS;1999-06
2 LIANG Guo zhu, MA Bin, ZHANG Guo zhou, CHENG Xian chen,ZHANG Zhen peng(School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083);Investigation on gas dynamic resonance tube ignition method[J];Journal of Propulsion Technology;2001-04
3 LIANG Guo zhu,MA Bin,CHENG Xian chen,ZHANG Guo zhou,ZHANG Zhen peng(Coll. of Astronautics,Beijing Univ. of Aeronautics and Astronautics,Beijing 100083,China);Preliminary experimental investigation on gas dynamic resonance tube heating effect[J];Journal of Propulsion Technology;2002-01
4 LIANG Guo zhu, AN lian, ZHANG Zhen peng (School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083,China);Numerical investigation on gas dynamic resonance tube heating oscillating flow process[J];Journal of Propulsion Technology;2002-02
5 TONG Xiaoyan, ZHANG Guozhou, MA Bin, LIANG Guozhu, SONG Yana(School of Astronautics, Beijing Univ of Aeronautics and Astronautics, Beijing 100083,China);Research on gas dynamic resonance igniters of multithruster[J];Journal of Propulsion Technology;2002-05
6 Liang Guozhu Zhang Guozhou Cheng Xianchen Ma Bin Zhang Zhenpeng(School of Astronautics,Beijing Univ.of Aeronautics and Astronautics,Beijing,100083);PRELIMINARY INVESTIGATION ON GAS DYNAMIC RESONANCE IGNITION FOR LIQUID PROPELLANT ROCKET ENGINE[J];JOURNAL OF PROPULSION TECHNOLOGY;1999-04
7 Zhang Guozhou Tong Xiaoyan Liang Guozhu Ma Bin Cheng Xianchen (Beijing university of Aeronautics and Astronautics,Beijing 100083)[WT5”HZ];INVESTIGATION ON GAS DYNAMIC RESONANCE IGNITION TECHNOLOGY FOR LIQUID PROPELLANT ROCKET ENGINE[J];Journal of Astronautics;2001-04
【Secondary References】
Chinese Journal Full-text Database 9 Hits
1 Guo Hongjie Liang Guozhu Ma Bin Zhang Zhenpen g(School of Astronautics, Beijing University of Aeronautics and As tronautics, Beijing 100083, China);Preliminary investigation on detonation wave ignition technique[J];Journal of Beijing University of Aeronautics and Astronautics;2005-04
2 Yu Nanjia Zhang Guozhou Song Yana(School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China) Cheng Shengqing(Beijing Aerospace Propulsion Institute, Beijing 100074, China);Research on synchronistic multi-ignitions of hydrogen-oxygen resonance ignitor[J];Journal of Beijing University of Aeronautics and Astronautics;2005-06
3 Song Yana Zhang Guozhou (School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China) Zhou Wenlu Huang Xiang (Beijing Aerospace Propulsion Institute, Beijing 100076, China);Investigation on head of novel chemical thruster for orbit maneuver[J];Journal of Beijing University of Aeronautics and Astronautics;2005-08
4 YU Nan-jia,ZHANG Guo-zhou,SONG Ya-na(School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing100083,China);Experimental Investigation of Gas-Dynamic Resonance Heating[J];Journal of Aerospace Power;2005-02
5 SONG Ya-na~1,YU Nan-Jia~1,MA Bin~1,ZHOU Wen-lu~2,HUANG Xiang~2(1.School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing100083,China;2.Beijing Aerospace Propulsion Institute,Beijing100076,China);Ground Ignition Test of an Orbit Maneuver H_2/O_2 Thruster Based on Gas Dynamic Resonance Igniter[J];Journal of Aerospace Power;2005-03
6 SONG Ya-na1, YU Nan-jia1, ZHANG Guo-zhou1, MA Bin1, ZHOU Wen-lu2, HUANG Xiang2 (1.School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China) (2.Beijing Aerospace Propulsion Institute, Beijing 100076, China);Investigation of Novel Hydrogen/Oxygen Thruster for Orbital Maneuver in Space Station[J];中国航空学报(英文版);2005-04
7 YU Nan-jia~1, ZHANG Guo-zhou~1, LIU Hong-jun~2, L Qi-wei~2, HE Wei-feng~1, MA Bin~1(1.School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China; 2.Shaanxi Engine Design Inst., Xi'an 710100, China);Investigation of helium resonance ignitor and kerosene/oxygen ignitor[J];Journal of Propulsion Technology;2003-06
8 YU Nan-jia,ZHANG Guo-zhou,SONG Ya-na,MA Bin,TONG Xiao-yan(School of Astronautics,Beijing Univ. of Aeronautics and Astronautics,Beijing 100083,China);Experimental investigation for coaxial hydrogen/oxygen resonance ignitor[J];Journal of Propulsion Technology;2004-03
9 YU Nan-jia,ZHANG Guo-zhou,MA Bin,CAI Guo-biao,(School of Astronautics,Beijing Univ. of Aeronautics and Astronautics,Beijing 100191,China);Experimental investigation for hydrogen/oxygen engine using gas dynamic resonance ignition technique[J];Journal of Propulsion Technology;2010-02
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