5kW xenon ion thruster lifetest
Author(s) -
Michael Patterson,
Timothy R. Verhey
Publication year - 1990
Publication title -
21st international electric propulsion conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1990-2543
Subject(s) - propellant , ion thruster , xenon , aerospace engineering , power (physics) , nuclear engineering , beam (structure) , propulsion , environmental science , physics , engineering , atomic physics , optics , quantum mechanics
This paper describes the results of the first lifetest of a high power ring-cusp ion thruster. A 30-cm laboratory model thruster was operated steady-state at a nominal beam power of 5kW on xenon propellant for approximately 900 hours. This test was conducted to identify life-limiting erosion mechanisms and thruster design modifications, and to demonstrate operation using simplified power processing. The results from this test are described including the conclusions derived from extensive post-test analyses of the thruster. Modifications to the thruster and ground support equipment, which have been incorporated to solve problems identified by the lifetest, are also described.
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