小型航天器用氨电热微发动机的研究

V. Blinov, V. V. Kositsin, V. I. Ruban, V. V. Shalay
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引用次数: 2

摘要

考虑了多用途机动小航天器氨校正推进系统电热微发动机的设计和构造概念问题。定义了ETME的结构设计,给出了实验研究的结果和进一步改进的方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The research of ammonia electrothermal microengines for small spacecrafts
Issues of design and construction concept of electrothermal microengines (ETME) for ammonia correcting propulsion systems (CPS) of maneuvering small spacecrafts (SS) using multi-purpose approach are considered. ETME structural designs are defined, results of experimental studies and ways of further improvement of ETME are presented.
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