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IAPS (8-cm) ion thruster cyclic endurance testAttention is given to the cyclic endurance qualification test, performed in a vacuum facility with a liquid nitrogen-cooled cryosurface and a frozen mercury target, to which a mercury-ion thruster representative of Ion Auxiliary Propulsion System (IAPS) thrusters was subjected. At the time that the endurance test was successfully concluded, upon consumption of the IAPS propellant tank's mercury, 8,471 hours of 'beam-on time' and 599 cycles had been accumulated. The system's Power Electronics Unit accumulated 10,268 hours of test time with high voltage applied to the operating thruster or dummy load.
Document ID
19850034255
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dulgeroff, C. R.
(Hughes Research Labs. Malibu, CA, United States)
Beattie, J. R.
(Hughes Research Labs. Malibu, CA, United States)
Poeschel, R. L.
(Hughes Research Labs. Malibu, CA, United States)
Hyman, J., Jr.
(Hughes Research Laboratories Malibu, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: International Electric Propulsion Conference
Location: Tokyo
Country: Japan
Start Date: May 28, 1984
End Date: May 31, 1984
Sponsors: Japan Society for Areonautical and Space Sciences, AIAA, and DGLR
Accession Number
85A16406
Funding Number(s)
CONTRACT_GRANT: NAS3-21741
Distribution Limits
Public
Copyright
Other

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