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推进剂组分对电弧加热推力器性能的影响
Alternative TitleEffect of Propellant Composition on the Performance of Arcjet Thrusters
黄河激; 潘文霞; 孟显; 吴承康
Source Publication工程热物理学报
2013-05-15
Volume34Issue:5Pages:896-898
ISSN0253-231X
Abstract实验研究了以纯氮、纯氢、氨气以及不同体积比氮氢混合气、氨氢混合气作为推进剂时,千瓦级电弧加热推力器的性能。结合理论分析,获得了推进剂组分对推力器性能的影响规律。结果表明,推进剂有效分子量和比热比对推力器冷态性能影响显著。热态下,推进剂组分的热力学性质以及输运性质是影响推力器比冲和效率的关键因素。
Keyword电弧加热推力器 推进剂组分 比冲 比功率 效率
Subject Area电磁流体力学和等离子体动力学
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Indexed ByEI ; CSCD
Language中文
Funding Organization国家自然科学基金(No.50836007;No.11175226;No.10921062)
CSCD IDCSCD:4831597
DepartmentLHD应用等离子体力学(CPCR)
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Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/47283
Collection高温气体动力学国家重点实验室
Corresponding Author黄河激
Recommended Citation
GB/T 7714
黄河激,潘文霞,孟显,等. 推进剂组分对电弧加热推力器性能的影响[J]. 工程热物理学报,2013,34(5):896-898
APA 黄河激,潘文霞,孟显,&吴承康.(2013).推进剂组分对电弧加热推力器性能的影响.工程热物理学报,34(5),896-898.
MLA 黄河激,et al."推进剂组分对电弧加热推力器性能的影响".工程热物理学报 34.5(2013):896-898.
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