A Proposed On-Orbit Demonstration of an Advanced Pulsed-Plasma Thruster for Small Satellite Applications

Author(s):  
D. R. Bromaghim ◽  
G. G. Spanjers ◽  
R. A. Spores ◽  
R. L. Burton ◽  
D. Carroll
Nukleonika ◽  
2015 ◽  
Vol 60 (2) ◽  
pp. 257-261 ◽  
Author(s):  
Agnieszka Szelecka ◽  
Jacek Kurzyna ◽  
Dariusz Daniłko ◽  
Serge Barral

Abstract A new type of pulsed plasma thruster (PPT) for small satellite propulsion is investigated, of which the most innovative aspect is the use of a non-volatile liquid propellant. The thruster is based on an open capillary design. The thruster achieved a thrust-to-power ratio above 45 μN/W, which constitutes a 5-fold improvement over the water-propelled pulsed plasma thruster, and which is also slightly above the performance of a similarly sized PPT with a solid propellant.


Vacuum ◽  
2008 ◽  
Vol 83 (1) ◽  
pp. 72-76 ◽  
Author(s):  
Junichiro Aoyagi ◽  
Masayuki Mukai ◽  
Yukiya Kamishima ◽  
Tsubasa Sasaki ◽  
Kouhei Shintani ◽  
...  

2013 ◽  
Vol 91 ◽  
pp. 187-193 ◽  
Author(s):  
David Krejci ◽  
Bernhard Seifert ◽  
Carsten Scharlemann

1996 ◽  
Author(s):  
Gregory Spanjers ◽  
Keith McFall ◽  
Frank Gulczinski, III ◽  
Ronald Spores

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