Performance of a green propellant thruster with discharge plasma

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• 作者：Takahiro Shindo ; ^{shindo-takahiro@ed.tmu.ac.jp} ; Asato Wada ; Hiroshi Maeda ; Hiroki Watanabe ; Haruki Takegahara
• 关键词：Hydroxylammonium nitrate ; Green propellant ; Ignition ; Plasma ; Pulsed discharge ; Chamber pressure
• 刊名：Acta Astronautica
• 出版年：2017
• 出版时间：February 2017
• 年：2017
• 卷：131
• 期：Complete
• 页码：92-95
• 全文大小：1589 K
• 卷排序：131

文摘

Discharge plasma was employed to react hydroxylammonium nitrate based propellant. The maximum thrust of 322 mN was obtained during the 1.5 s short-firing test. Rapid combustion chamber pressure increase was observed by using pulsed discharge.