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PULSE PLASMA THRUSTER AND SPACECRAFT USING THIS THRUSTER

机译:脉冲等离子推进器和使用该推进器的航天飞机

摘要

PROBLEM TO BE SOLVED: To provide a highly reliable pulse plasma thruster and a spacecraft using this thruster with a simple constitution for finely adjusting propulsion while lengthening the service life by increasing a generating impulse by effectively using a propellant.;SOLUTION: This pulse plasma thruster is formed by arranging discharge chambers 2a and 2b for forming its part of the propellant 8, a cathode 3, anodes 4a and 4b and an igniter 6 in a thruster unit 1, and is characterized by arranging the discharge chambers 2a and 2b in a plurality, and arranging an induction passage 7 for communicating with at least two or more among the discharge chambers 2a and 2b.;COPYRIGHT: (C)2007,JPO&INPIT
机译:解决的问题:提供一种高度可靠的脉冲等离子推进器和一种使用该推进器的航天器,其结构简单,可通过有效地使用推进剂来增加发电脉冲,从而在提高推进力的同时细调推进力。通过在推进器单元1中布置用于形成推进剂8的一部分的排放室2a和2b,阴极3,阳极4a和4b以及点火器6而形成,并且其特征在于,将排放室2a和2b布置为多个;并布置了一个感应通道7,用于与放电室2a和2b中的至少两个或更多个连通。;版权所有:(C)2007,JPO&INPIT

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