摘要
A CO2 laser was employed to ablate water droplets provided by a pulsed liquid propellant feeding system. Experimental results indicate that momentum coupling coefficient Cm is increased to 50 × 10-5 N·s·J-1, which is higher than that of air-breathing mode laser propulsion. The measurement data were compared to the results of other authors. The way to improve the performance parameters of laser propulsion with liquid propellants was discussed.
源语言 | 英语 |
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页(从-至) | 526-529 |
页数 | 4 |
期刊 | Tuijin Jishu/Journal of Propulsion Technology |
卷 | 28 |
期 | 5 |
出版状态 | 已出版 - 10月 2007 |