In this paper, the Micro chemical Thruster's structure was designed and loading method of propellant and test method of thrust were investigated.
该文设计了化学微推力器的结构，研究了微推力器的装药方法和推力的测试方法。
It was showed that PPT was a kind of advanced propeller with small thrust, which was suitable to orbit transfer, attitude control, station keeping and formation flying for small and micro satellite.
分析认为PPT是一种先进的小推力动力装置，特别适合于微小卫星的轨道转移、姿态控制、位置保持以及星座编队飞行。
The focused effect of laser is very important in laser micro-thrust measurement.
激光器的聚焦情况对于激光微推力测量过程中的实验结果有着重要影响。
Eventually given a 40 kg thrust class, low-pressurized than 3.0 single-turbofan engine micro-impeller rich data and characteristic curves.
最终给出了一台40公斤推力级、低增压比为3.0的单叶轮微涡扇发动机的丰富数据和特性曲线。
Eventually given a 40 kg thrust class, low-pressurized than 3.0 single-turbofan engine micro-impeller rich data and characteristic curves.
最终给出了一台40公斤推力级、低增压比为3.0的单叶轮微涡扇发动机的丰富数据和特性曲线。
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