The performance analysis of power processing unit for electrojet plasma thrusters of space crafts

Proceedings of the 6th International Scientific and Practical Conference of Students, Post-graduates and Young Scientists. Modern Techniques and Technology. MTT'2000 (Cat. No.00EX369) Pub Date : 2000-02-28 DOI:10.1109/SPCMTT.2000.896025

M. Mikhailov

引用次数: 0

Abstract

At the present time, modern spacecraft have an onboard orbit raising thrusters system (ORTS). Many ORTSs contain electrojet plasma thrusters. The power processing unit is an obligatory part of any ORTS. It ensures the required electropower modes to all stationary plasma thruster elements. Here, the author presents a method for the performance analysis of spacecraft electrojet plasma thruster power processing units.

查看原文本刊更多论文

航天器电喷等离子体推力器功率处理单元性能分析

目前，现代航天器都采用星载轨道提升推进器系统(ORTS)。许多ORTSs包含电喷射等离子体推进器。电源处理单元是任何ort的必备部件。它确保了所有固定等离子体推力器元件所需的电力模式。本文提出了一种航天器电喷等离子体推力器功率处理单元的性能分析方法。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

求助全文

约1分钟内获得全文求助全文

来源期刊

Proceedings of the 6th International Scientific and Practical Conference of Students, Post-graduates and Young Scientists. Modern Techniques and Technology. MTT'2000 (Cat. No.00EX369)

自引率

0.00%

发文量