An Overview of the Results from the 30,000 Hr Life Test of Deep Space 1 Flight Spare Ion Engine
Author:
Affiliation:
1. Jet Propulsion Laboratory
2. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3608
Reference14 articles.
1. Polk, J. E., etal, "An Overview of the Results from an 8200 Hour Wear Test of the NSTAR Ion Thruster," AIAA-99-2446,June1999.
2. Polk, J.E., etal, "A1000-hourWear Testof theNASANSTARIonThruster,"AIAA-96-2717,July1996.
3. Polk, J. E., etal, "The Effect of Engine Wear on Performance in the NSTAR 8000 Hour Ion Engine Endurance Test,"AIAA-97-3387,July1997.
4. Christensen, J., etal, "Design and fabrication of a Flight Model 2.3 kW Ion Thruster for the Deep Space 1 Mission,"AIAA-98-3327,July1998.
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