1) micro colloid thruster
微胶体推进器
2) colloid thruster
胶体推进器
1.
MEMS colloid thruster array can meet the thruster index requirements of small size and high specific impulse.
MEMS阵列式胶体推进器具有体积小,比冲高等特点,能够满足微卫星发展需求。
3) micro-thruster
微推进器
1.
Igniter is the most important part of MEMS solid propellant micro-thruster, and its igniting voltage and igniting reliability are mainly decided by the igniting resistance.
点火电路是MEMS固体化学微推进器中最重要的组成部分,其点火电压的大小及点火可靠性则主要取决于点火电阻。
2.
With the development of micro-satellite, the study of micro-thruster, including laser plasma micro-thruster, becomes urgent in recent years.
随着微卫星技术的发展,微推进器的研究已经越来越紧迫,而激光等离子体微推进器则正是其中的一种。
3.
The developments in thrust measuring techniques for the micro-thrusters are reviewed.
对近年来微推进器(Micro thruster)的推力测试技术和手段进行了较全面的综述,并对几种典型进行单脉冲冲量、平均推力等参数测量的推力测试系统和手段进行描述,分析各自的特点。
4) microthruster
微推进器
1.
A double wafer microthruster based on MEMS is designed and fabricated.
介绍了一种两层结构的MEMS冷气微推进器的设计和制作。
5) Micro thruster
微推进器
1.
MEMS based solid propellant micro thruster is a new type of micropropulsion system, which is required in microspacecraft for station keeping, attitude control, gravitation compensation and orbit adjust.
MEMS固体微推进器是一种新型的微推进系统,主要用于微型航天器的位置保持、姿态控制、引力补偿和轨道调整。
2.
Design, fabrication and test of the micro thruster were introduced in this thesis.
微推进器是一种基于MEMS技术的新型微推进系统,主要用于微小型航天器的位置保持、姿态控制、轨道调整等。
6) Gelled propellants
胶体推进剂
补充资料：固液混合火箭推进剂(见火箭推进剂)
固液混合火箭推进剂(见火箭推进剂)
solid-liguid hybrid rocket propellant
guye hunhe huoiian tui)in)i固液混合火箭推进剂(s olid一Iiguid hy-brid rocket proPellant)见火箭推讲齐，}_
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条