小、迷你、微型卫星轨道校正系统用低功率空心推进器

T. Maksymenko, A. Loyan, N. Koshelev
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引用次数: 1

摘要

本文讨论了低功率SPT的发展现状。对这类推进器的主要要求作了说明。研制低功率霍尔推进器的几种方法及其优缺点。介绍了新型律功率推力器实验室模型SPT-20M的试验结果和主要参数。对比了SPT模型和由世界领先专家开发的法律功率空心推进器的特点。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The low power hollow thruster for orbit correction system for small, mini and micro satellites
In this article problem of low-power SPT development actualite is considered. The main requirements for this thruster class are represented. Some methods of low-power Hall thruster developing and their advantages and disadvantage. The test results and main parameters of new law-power thruster laboratory model SPT-20M are represented. Comparative characteristics of SPT model and law power hollow thrusters developed by leading world specialists is shown.
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