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Comparison of On-Orbit and Ground Based Hollow Cathode OperationThe Plasma Contactor Unit (PCU) was developed by the Rocketdyne division of Boeing 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 wear tests and qualification tests. GRC is currently tracking the on-orbit data for the flight HCAs. This data will be discussed with comparison to operating parameters verified by ground based HCA tests. The flight HCAs continue to operate flawlessly. The first unit has accumulated more than 3650 hours of on-orbit operation and the second unit has accumulated over 5550 hours.
Document ID
20030093731
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
Burke, Tom
(NASA Glenn Research Center Cleveland, OH, United States)
Carpenter, Christian
(QSS Group, Inc. Cleveland, OH, United States)
Date Acquired
August 21, 2013
Publication Date
September 1, 2003
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA Paper 2003-5145
NAS 1.26:212585
E-14140
NASA/CR-2003-212585
Report Number: AIAA Paper 2003-5145
Report Number: NAS 1.26:212585
Report Number: E-14140
Report Number: NASA/CR-2003-212585
Meeting Information
Meeting: 39th Joint Propulsion Conference and Exhibit
Location: Huntsville, AL
Country: United States
Start Date: July 20, 2003
End Date: July 23, 2003
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, American Society for Electrical Engineers, Society of Automotive Engineers, Inc.
Funding Number(s)
CONTRACT_GRANT: NAS3-00145
WBS: WBS 22-755-04-11
Distribution Limits
Public
Copyright
Public Use Permitted.
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