Experimental and Numerical Studies of a Low-Power N2 Arcjet Thruster

By Keisuke Ichige; Shigeru Kuchi-ishi; Ken-ichi Abe

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Experimental and Numerical Studies of a Low-Power N2 Arcjet Thruster

机译：低功率N2 Arcjet推进器的实验和数值研究

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This paper describes the experimental and numerical studies of a laboratory model of the low-power nitrogen arc- jet thruster that developed to provide thruster performance data to validate numerical results. The arcjet thruster was operate by using a nozzle 1.0 mm in constrictor diameter. Thrust and input power were measured for various arc currents and nitrogen mass flow rates. The operation was done at power levels ranging from 156W to 540W and nitro- gen mass flow rates from 5 mg/s to 30 mg/s.

机译：本文介绍了低功率氮气电弧喷射推进器实验室模型的实验和数值研究，该模型的开发旨在提供推进器性能数据以验证数值结果。通过使用收缩器直径为1.0 mm的喷嘴操作arcjet推进器。测量了各种电弧电流和氮气质量流量的推力和输入功率。该操作在156W至540W的功率水平和5 mg / s至30 mg / s的氮气质量流率下完成。

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来源
《Transactions of the Japan society for aeronautical and space sciences》 |2001年第142期|p.208-214|共7页
作者
By Keisuke Ichige; Shigeru Kuchi-ishi; Ken-ichi Abe;
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作者单位

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类航空;
关键词
Arcjet Thruster; Electric Propulsion; Thermochemical Nonequilibrium;

机译：Arcjet推进器;电力推进;热化学非平衡;

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Experimental and Numerical Studies of a Low-Power N2 Arcjet Thruster

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