The paper presents a methodology to estimate the onset voltage of a micro fabricated colloid thruster.
提供了一种考虑到微制造工艺实际的对微胶体推进器的起始电压进行估计的方法。
The several key technologies of laser micro-thruster are discussed as well.
讨论了激光微推力器需要解决的几个关键技术问题。
Ignition start-up model of impulse micro-thruster is established, considering two phase flow and impact heat transfer of particle on the surface of propellant.
建立了微型脉冲推力器点火启动模型，模型中考虑了两相流动和颗粒对推进剂表面的冲击传热。
Ignition start-up model of impulse micro-thruster is established, considering two phase flow and impact heat transfer of particle on the surface of propellant.
建立了微型脉冲推力器点火启动模型，模型中考虑了两相流动和颗粒对推进剂表面的冲击传热。
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