当前位置: X-MOL 学术J. Propuls. Power › 论文详情
Our official English website, www.x-mol.net, welcomes your feedback! (Note: you will need to create a separate account there.)
Increased Thrust-to-Power Ratio of a Stepped-Diameter Helicon Plasma Thruster with Krypton Propellant
Journal of Propulsion and Power ( IF 1.9 ) Pub Date : 2020-09-03 , DOI: 10.2514/1.b37940
Kazunori Takahashi 1 , Yoshinori Takao 2 , Akira Ando 1
Affiliation  

Journal of Propulsion and Power, Ahead of Print.


中文翻译:

带有K推进剂的阶梯式直径Helicon等离子推进器的推力功率比提高

推进与动力杂志,预印本。
更新日期:2020-09-03
down
wechat
bug