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Evaluation of particle transport for the P80-1 spacecraftCharged and neutral particle transport from an 8-cm mercury ion thruster to the surfaces of the P80-1 spacecraft, the Teal Ruby sensor and the ECOM-501 sensor was examined. Evaluation of particle transport modes utilized both laboratory measurements and analysis. Line-of-sight particle transport considered deposition of Group II (high energy-high angle mercury charge exchange) ions and neutral mercury on solar array surfaces. Nonline-of-sight transport modes studied were recirculation/reinterception of mercury ions in magnetic fields and refraction of low energy mercury charge exchange (Group IV) ions by local electric fields.
Document ID
19800029131
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sellen, J. M., Jr.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Komatsu, G. K.
(TRW Defense and Space Systems Group Redondo Beach, Calif., United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1979
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 79-2047
Meeting Information
Meeting: International Electric Propulsion Conference
Location: Princeton, NJ
Start Date: October 30, 1979
End Date: November 1, 1979
Sponsors: Princeton University, AIAA, and DGLR,
Accession Number
80A13301
Funding Number(s)
CONTRACT_GRANT: NAS3-21047
Distribution Limits
Public
Copyright
Other

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