Direct Thrust Measurement of a Permanent-Magnets Helicon Plasma Thruster for Space Propulsion

2014 ◽  
Vol 9 (0) ◽  
pp. 3406025-3406025 ◽  
Author(s):  
Daisuke KUWAHARA ◽  
Yushi KOYAMA ◽  
Shuhei OTSUKA ◽  
Takamichi ISHII ◽  
Hiroki ISHII ◽  
...  

Author(s):  
Takahiro NAKAMURA ◽  
Hiroyuki NISHIDA ◽  
Shunjiro SHINOHARA ◽  
Ikkoh FUNAKI ◽  
Takao TANIKAWA ◽  
...  

Author(s):  
Andreas Neumann

DLR operates the High Vacuum Plume Test Facility Göttingen – Electric Thrusters (STG-ET). This electric propulsion test facility has now accumulated several years of EP-thruster testing experience. Special features tailored to electric space propulsion testing like a large vacuum chamber mounted on a low vibration foundation, a beam dump target with low sputtering, and a performant pumping system characterize this facility. The vacuum chamber is 12.2m long and has a diameter of 5m. With respect to accurate thruster testing, the design focus is on accurate thrust measurement, plume diagnostics, and plume interaction with spacecraft components. Electric propulsion thrusters have to run for thousands of hours, and with this the facility is prepared for long-term experiments. This paper gives an overview of the facility, and shows some details of the vacuum chamber, pumping system, diagnostics, and experiences with these components.


2016 ◽  
Vol 8 (4) ◽  
pp. 15-27
Author(s):  
ANDREESCU Anna-Maria Theodora ◽  
◽  
TEODORESCU Maximilian-Vlad ◽  
POPESCU Jeni Alina ◽  
VILAG Valeriu-Alexandru ◽  
...  

2014 ◽  
Vol 21 (4) ◽  
pp. 043507 ◽  
Author(s):  
T. Lafleur

Author(s):  
Franco Bosi ◽  
Fabio Trezzolani ◽  
Andrea Lucca Fabris ◽  
Marco Manente ◽  
Davide Melazzi ◽  
...  

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