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作 者:康会峰[1,2] 徐烨璇 梅天宇 夏广庆 鹿畅[1,2,3] KANG Huifeng;XU Yexuan;MEI Tianyu;XIA Guangqing;LU Chang(Collaborative Innovation Center of Micro&Nano Satellites of Hebei Province,North China Institute of Aerospace Technology,Langfang 065000,Hebei,China;Key Laboratory of Micro Spacecraft Technology of Hebei Province,North China Institute of Aerospace Engineering,Langfang 065000,Hebei,China;State Key Laboratory of Structural Analysis,Optimization and CAE Software for Industrial Equipment,Dalian University of Technology,Dalian 116024,Liaoning,China;School of Liberal Arts and Sciences,North China Institute of Aerospace Engineering,Langfang 065000,Hebei,China)
机构地区:[1]北华航天工业学院航空宇航学院河北省微纳卫星协同创新中心,河北廊坊065000 [2]北华航天工业学院河北省微小型航天器技术重点实验室,河北廊坊065000 [3]大连理工大学工业装备结构分析优化与CAE软件全国重点实验室,辽宁大连116024 [4]北华航天工业学院文理学院,河北廊坊065000
出 处:《上海航天(中英文)》2024年第S2期141-149,共9页Aerospace Shanghai(Chinese&English)
基 金:国家重点研发计划(2021YFE0116000);国家自然科学基金(12175032,12102082);中央高校基本科研业务费专项资金(DUT21GJ206);辽宁省重点研发计划(2020JH2/10500003);河北省省级科技计划资助(22E50445D);河北省省级科技计划资助(YCYZ202201,216Z1901G,206Z1902G);河北省科技创新项目(SJMYF2022X06);河北省高等学校科学技术研究项目资助(ZC2023144);北华航天工业学院青年基金项目(KY-2024-07)
摘 要:空间探测的快速发展,使电推进技术的应用越来越广泛,其中霍尔推力器作为技术较为成熟的电推力器,目前已广泛应用于卫星位置保持、大气阻力补偿及轨道转移等任务中。霍尔推力器的贮供系负责均衡稳定地输出流量,对推力器的性能具有直接影响。本文对霍尔推力器不同种类推进剂的国内外研究现状开展调研,总结不同推进剂贮供系统的关键技术,介绍未来可替代氙气的几种推进剂。研究结果可为提升提高霍尔推力器的性能及相关后续的研究提供新思路。The rapid development of space exploration makes the application of electric propulsion technology more and more extensive.Hall thruster,as a relatively mature electric thruster,has been widely used in satellite northsouth position maintenance,atmospheric drag compensation,orbit transfer,etc.The storage and supply system of a thruster is responsible for the balanced and stable output flow,which has a direct effect on the performance of the thruster.In this paper,the research status of different types of propellants at home and abroad is investigated,the key technologies for the storage and supply systems with different propellants are summarized,and several propellants that can replace xenon in the future are introduced.The research could provide new ideas for improving the performance of Hall thrusters and the related future research.
分 类 号:V439[航空宇航科学与技术—航空宇航推进理论与工程]
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