Xe ion plasma thruster XIPS-200 for orbit correction of geostationary communication satellite

被引：0

作者：

Stepanushkin, NP ^{[1
]}

Koshelev, NN ^{[1
]}

Aliyeva, MT ^{[1
]}

Loyan, AV ^{[1
]}

Ishenko, EI ^{[1
]}

机构：

[1] Natl Aerosp Univ KhAI, Kharkov, Ukraine

来源：

RAST 2005: Proceedings of the 2nd International Conference on Recent Advances in Space Technologies | 2005年

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

One of the more developed, approbate in space condition, reliable and having a big work resources electric propultions (EP) is ion plusma thruster (IPT). Probably therefore for today it is demand for solution of broad-spectrum tasks of space vehicles movement. One of them is orbit correction of weighty geostationary communication satellites [1, 2, 3].

引用

页码：355 / 357

页数：3