Publication Date:
2019-07-13
Description:
This paper summarizes the development of reservoir cathodes for the 20 kWe NEXIS ion thruster. It includes results of performance testing, thermal characterization and preliminary wear testing.
Keywords:
Spacecraft Propulsion and Power
Type:
Joint Propulsion Conference; Jul 01, 2004; Ft. Lauderdale, FL; United States
Format:
text
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