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喷管是激光推力器的重要组成部分。
The nozzle is one of the most important parts a laser thruster .
研究结果对于吸气式激光推力器的喷管构形设计具有指导意义。
The results are very useful to design nozzle structure of laser thruster that works in air-breathing mode.
实验结果表明，该系统可以捕获激光推力器脉冲推力加载特征。
Experimental results indicate that this test system can capture the characteristics of thrust loading and it is valuable for investigating laser thrusters and pulse detonation engines.
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