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Autor:
Matteo Magnifico, Davide Nicolini, Giulio Simonelli, Lorenzo Serafini, S Alta, Marco Saviozzi, Luca Ceruti
Publikováno v:
40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
This paper presents the results of the first field emission thruster performance characterization test with a flight standard power control unit designed to fulfill the stringent requirements of new scientific drag-free missions. The thruster, a 5-mm