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Thruster endurance testA test system was built and several short term tests were completed. The test system included, in addition to the 30-cm ion thruster, a console for powering the thruster and monitoring performance, a vacuum facility for simulating a space environment, and a storage and feed system for the thruster propellant. This system was used to perform three short term tests (one 100-hour and two 500-hour tests), an 1108-hour endurance test which was aborted by a vacuum facility failure, and finally the 10,000-hour endurance test. In addition to the two 400 series thrusters which were used in the short term and 1100-hour tests, four more 400 series thrusters were fabricated, checked out, and delivered to NASA. Three consoles similar to the one used in the test program were also fabricated and delivered.
Document ID
19760016267
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Collett, C.
(Hughes Research Labs. Malibu, CA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1976
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-135011
Report Number: NASA-CR-135011
Accession Number
76N23355
Funding Number(s)
CONTRACT_GRANT: NAS3-15523
CONTRACT_GRANT: NAS3-17803
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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