小功率电弧加热发动机地面试验（Ⅰ）NH3推进剂试验和分析

推进技术 ›› 2006, Vol. 27 ›› Issue (4): 359-362.

小功率电弧加热发动机地面试验（Ⅰ）NH₃推进剂试验和分析

汤海滨,刘畅,马彬,肖应超,刘宇

北京航空航天大学宇航学院北京100083;北京航空航天大学宇航学院北京100083;北京航空航天大学宇航学院北京100083;北京航空航天大学宇航学院北京100083;北京航空航天大学宇航学院北京100083

发布日期:2021-08-15
基金资助:
国家自然科学基金(50086001);国防基础科研项目(K1201060711)

Ground experiment on arcjet thrusters（Ⅰ）Experiment and analysis using NH₃ as propellant

School of Astronautics,Beijing Univ.of Aeronautics and Astronautics,Beijing 100083,China;School of Astronautics,Beijing Univ.of Aeronautics and Astronautics,Beijing 100083,China;School of Astronautics,Beijing Univ.of Aeronautics and Astronautics,Beijing 100083,China;School of Astronautics,Beijing Univ.of Aeronautics and Astronautics,Beijing 100083,China;School of Astronautics,Beijing Univ.of Aeronautics and Astronautics,Beijing 100083,China

Published:2021-08-15

摘要/Abstract

摘要： 介绍了以NH3为推进剂的小功率电弧加热式发动机模拟空间环境的地面试验,测量了发动机工作性能参数。通过对工作参数优化,达到发动机高比冲的工作状态,并重点分析了推进剂流量对发动机性能的影响。研究结论为N2H4推进剂的试验提供了依据。

关键词: 电弧加热发动机~+;试验;氨

Abstract: The ground experiment on low power arcjet thrusters was introduced.NH₃ was chosen as propellant and experiments were carried out.The thruster performance parameters were measured.High thruster specific impulse can be obtained by means of optimizing working parameters.The experimental results for mass flow are given in detail.

Key words: Arcjet thrusters~+;Experiment;Ammonia

汤海滨,刘畅,马彬,肖应超,刘宇. 小功率电弧加热发动机地面试验（Ⅰ）NH₃推进剂试验和分析[J]. 推进技术, 2006, 27(4): 359-362.

小功率电弧加热发动机地面试验（Ⅰ）NH₃推进剂试验和分析

Ground experiment on arcjet thrusters（Ⅰ）Experiment and analysis using NH₃ as propellant

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