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Effect of Nozzle Temperature on the Performance of a 1 kW H2-N2 Arcjet Thruster
  • ISSN号：1009-0630
  • 期刊名称：《等离子体科学与技术：英文版》
  • 时间：0
  • 分类：O561.5[理学—原子与分子物理;理学—物理] V439[航空宇航科学与技术—航空宇航推进理论与工程;航空宇航科学技术]
  • 作者机构：[1]Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China
  • 相关基金：supported by National Natural Science Foundation of China （Nos. 50836007, 10775164 and 10921062）
作者： 潘文霞[1], 黄河激[1], 吴承康[1]
关键词： 电弧喷射推力器, 千瓦级, 温度, 喷嘴, H2, 性能, N2, 宾夕法尼亚州, arcjet thruster, nozzle temperature, energy conversion, experimental measurement
中文摘要：

E-mail address of PAN Wenxia： wxpan@imech.ac.cn

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期刊信息
  • 《等离子体科学与技术：英文版》
  • 主管单位:中国科学院 中国科协
  • 主办单位:中国科学院等离子体物理研究所 中国力学学会
  • 主编：万元熙、谢纪康
  • 地址：合肥市1126信箱
  • 邮编：230031
  • 邮箱：pst@ipp.ac.cn
  • 电话：0551-5591617 5591388
  • 国际标准刊号：ISSN：1009-0630
  • 国内统一刊号：ISSN：34-1187/TL
  • 邮发代号:
  • 获奖情况:
  • 国内外数据库收录:
  • 美国化学文摘（网络版）,荷兰文摘与引文数据库,美国工程索引,美国剑桥科学文摘,美国科学引文索引（扩展库）,英国科学文摘数据库
  • 被引量:89