1·The thruster design requires that the total volume of the propulsion system be less than 10 percent of the CubeSat.
这个推进器设计规定了推进器系统的总体积不超过立方体卫星的10%。
2·One minute later, Garriott begins a second countdown, this time to signal the end of the thruster burn.
一分钟后，加略特重新开始倒数，这次是推进器燃烧解体的信号。
3·NASA developed a similar engine for its Deep Space 1 Mission, launched in 1998, but the new thruster has advantages.
NASA在1998年所发射的“深空一号”也曾使用类似的引擎，但相较而言，这个新型的推进器有自己的优势。
4·Cantwell's rocket thruster, which was designed for use in spacecraft, can consume the excess nitrous oxide to produce heat.
Cant well的火箭推进器设计原用于宇宙飞船，现可用来燃烧大量氧化氮。
5·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。