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Vehicle charging on STS-3 MissionIn the Vehicle Charging and Potential experiment on the STS-3 mission, a pulsed electron gun was used to eject known charges and currents from the Shuttle Orbiter, and the resulting perturbations of the surface charge and current densities were studied with appropriate instruments. An ejected current of 100 mA, if maintained for a time sufficiently long for equilibrium to be established, could change the vehicle potential by 50 V or more when the ambient plasma density was low. In general, the observed perturbations could be ordered qualitatively in terms of the plasma density and of the attitude of the shuttle relative to its orbital velocity vector.
Document ID
19850014162
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Williamson, P. R.
(Stanford Univ. CA, United States)
Banks, P. M.
(Stanford Univ. CA, United States)
Storey, L. R. O.
(Stanford Univ. CA, United States)
Raitt, W. J.
(Utah State Univ. Logan, United States)
Date Acquired
August 12, 2013
Publication Date
March 1, 1985
Publication Information
Publication: NASA. Lewis Research Center Spacecraft Environ. Interactions. Technol., 1983
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
85N22473
Funding Number(s)
CONTRACT_GRANT: NAS5-24455
CONTRACT_GRANT: NAGW-235
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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