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Performance of gas fed pulsed plasma thrusters using water vapor propellant

机译：使用水蒸气推进剂的气体供给脉冲等离子体推进器的性能

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摘要

The performance of two gas-fed pulsed plasma thrusters (GFPPTs) using both argon and water vapor for propellant has been measured using the JPL microthrust stand.

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作者
Ziemer, J.; Petr, R.;
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年度 2002
页码 1-8
总页数 8
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
ARGON; MICROTHRUST; PLASMA PROPULSION; PROPELLANTS; PULSED PLASMA THRUSTERS; WATER; WATER VAPOR; pulsed plasma thruster water propellant electric propulsion;

机译：氩气微小推力;等离子体推进;推进剂; pULsED pLasma THRUsTERs;水;水蒸气;脉冲等离子推进器水推进剂电推进;

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专利

1. Impulse and Performance Measurements of Electric Solid Propellant in a Laboratory Electrothermal Ablation-Fed Pulsed Plasma Thruster [J] . Matthew S. Glascock, Joshua L. Rovey, Kurt A. Polzin Aerospace . 2020,第6期

机译：实验室电热烧蚀脉冲等离子体推进器中电固体推进剂的脉冲和性能测量
2. Characteristics of a non-volatile liquid propellant in liquid-fed ablative pulsed plasma thrusters [J] . William Yeong Liang Ling, Tony Schonherr, Hiroyuki Koizumi Journal of Applied Physics . 2017,第7期

机译：液体烧蚀脉冲等离子体推进器中非挥发性液体推进剂的特性
3. Design and performance of liquid propellant pulsed plasma thruster [J] . Kakami A, Koizumi H, Komurasaki K, Vacuum: Technology Applications & Ion Physics: The International Journal & Abstracting Service for Vacuum Science & Technology . 2004,第3a4期

机译：液体推进剂脉冲等离子推进器的设计与性能
4. Performance of Gas- Fed Pulsed Plasma Thrusters Using Water Vapor Propellant [C] . J. Ziemer, R. Petr AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit . 2002

机译：水蒸气推进剂的气体脉冲等离子推进器的性能
5. Performance scaling of gas-fed pulsed plasma thrusters. [D] . Ziemer, John Kenneth. 2001

机译：气源脉冲等离子推进器的性能缩放。
6. Investigation of Microstructure and Mechanical Performance of IN738LC Superalloy Thin Wall Produced by Pulsed Plasma Arc Additive Manufacturing [O] . Kaibo Wang, Zhe Sun, Yuxin Liu, 2020

机译：脉冲等离子弧添加剂制造产生的738LC超合金薄壁微观结构和力学性能研究
7. Performance of Gas Fed Pulsed Plasma Thrusters Using Water Vapor Propellant* [O] . John K. Ziemert, Rodney A. Pet 2014

机译：使用水蒸气推进剂的气体输送脉冲等离子推进器的性能*

Performance of gas fed pulsed plasma thrusters using water vapor propellant

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