摘要
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.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 54-58 |
| 页数 | 5 |
| 期刊 | Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics |
| 卷 | 29 |
| 期 | 1 |
| 出版状态 | 已出版 - 1月 2003 |
指纹
探究 'Experimental studies on gas-oxygen/alcohol multi-pipe igniter' 的科研主题。它们共同构成独一无二的指纹。引用此
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