Operating the helicon double layer thruster in a space simulation chamber

被引:14
|
作者
Charles, Christine [1 ]
Boswell, Rod [1 ]
Alexander, Peter [1 ]
Costa, Costanzo [1 ]
Sutherland, Orson [1 ]
Pfitzner, Leigh [2 ]
Franzen, Roger [2 ]
Kingwell, Jeff [3 ]
Parfitt, Andrew [3 ]
Frigot, Pierre-Etienne [4 ]
Del Amo, Jose [4 ]
Saccoccia, Georgio [4 ]
机构
[1] Australian Natl Univ, SP3 Grp, Plasma Res Lab, Res Sch Phys Sci & Engn, Canberra, ACT 0200, Australia
[2] Auspace Ltd, Mitchell, ACT 2911, Australia
[3] CRC Satellites Syst, Canberra, ACT 2601, Australia
[4] European Space Agcy, European Space Res & Technol Ctr, NL-2200 AG Noordwijk, Netherlands
关键词
acceleration; ion beams; plasma engines; propulsion;
D O I
10.1109/TPS.2008.924425
中图分类号
O35 [流体力学]; O53 [等离子体物理学];
学科分类号
070204 ; 080103 ; 080704 ;
摘要
A prototype of the helicon double layer thruster (HDLT) is designed and manufactured. Initial tests with the thruster mounted on a small vacuum chamber (pumping speed of 700 l.s(-1)) show successful operation in xenon with the formation of the double layer which generates a low divergence ion beam, which is the source of thrust. The prototype is subsequently inserted inside a much larger space simulation chamber (pumping speed of 7000 l.s(-1)). A high-density blue mode is found when increasing the RF power above 380 W, and measurements with a Langmuir probe give an estimated density of 10(12) cm(-3); in the thruster. An image of the HDLT operating in the high-density blue mode is presented.
引用
收藏
页码:1196 / 1197
页数:2
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