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�������պ����ѧѧ�� 2003, Vol. 29 Issue (1) :54-58    DOI:
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Experimental Studies on Gas��Oxygen/Alcohol Multi��Pipe Igniter
Wang Yibai, Liu Yu, Qin Lizi, Ma Bin*
School of Astronautics, Beijing University of Aeronautics and Astronautics

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Abstract�� Multi-pipe synchronous ignition technique is one of the key techniques of aerospike engine. Design and experiments of a gas-oxygen/alcohol multi-pipe igniter were introduced. The key factors influencing multi-pipe ignition were studied, which include propellants mixture ratio, time of igniting, material and geometrical size of the pipe, methods used to cool the igniter, and oxygen supply combustion. In addition, ignition methods at high altitude were also investigated. On the above basis, parameters of the igniter were determined, multi-pipe synchronous ignition was realized.
Keywords�� ignition   test   liquid rocket engines   aerospike nozzle     
Received 2001-08-06;

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��һ��, ����, ������, ���.�����ƾ���ܵ���������о�[J]  �������պ����ѧѧ��, 2003,V29(1): 54-58
Wang Yibai, Liu Yu, Qin Lizi, Ma Bin.Experimental Studies on Gas��Oxygen/Alcohol Multi��Pipe Igniter[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2003,V29(1): 54-58
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