搜索历史记录选项已关闭,请开启搜索历史记录选项。
作者: J.L. Power
DOI: 10.1109/22.141350
关键词:
摘要: The microwave electrothermal thruster (MET) is attractive for medium- or high-power spacecraft propulsion. A propellant gas heated by passing it through a plasma discharge created in resonant cavity tuning either the TM
High Density Plasma Sources#R##N#Design, Physics and Performance,1995, 引用: 5
,2000, 引用: 1
international conference on recent advances in space technologies,2015, 引用: 1
IEEE Transactions on Plasma Science,2015, 引用: 0
international conference on plasma science,2001, 引用: 5
29th Joint Propulsion Conference and Exhibit,1993, 引用: 8
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,2005, 引用: 5
Plasma Sources Science and Technology,1994, 引用: 265
Journal of Physics D,1996, 引用: 5
Plasma Science and Technology,2005, 引用: 4