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On the Operational Status of the ISS Plasma Contactor Hollow CathodesThe Plasma Contactor Unit (PCU) was developed by the Rocketdyne division of The Boeing Company to control charging of the International Space Station (ISS). Each PCU contains a Hollow Cathode Assembly (HCA), which emits the charge control electrons. The HCAs were designed and fabricated at NASA s Glenn Research Center (GRC). GRC's HCA development program included manufacture of engineering, qualification, and flight model HCAs as well as qualification and wear tests. GRC tracks the on-orbit data for the flight HCAs in order to ascertain their overall health. As of April 5, 2004, 43 ignitions and over 6000 hours have been accumulated on a single unit. The flight HCAs continue to operate flawlessly. This paper will discuss the operation of the HCAs during ground tests and on-orbit operation from initial startup to April 30, 2004.
Document ID
20040110836
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Burke, Thomas P.
(NASA Glenn Research Center Cleveland, OH, United States)
Carpenter, Christian B.
(QSS Group, Inc. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2004
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA/CR-2004-213184
AIAA Paper 2004-3425
E-14680
Meeting Information
Meeting: 40th Joint Propulsion Conference and Exhibit
Location: Fort Lauderdale, FL
Country: United States
Start Date: July 11, 2004
End Date: July 14, 2004
Sponsors: Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers, American Society of Mechanical Engineers
Funding Number(s)
WBS: WBS 22-982-10-02
CONTRACT_GRANT: NAS3-00145
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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