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Active vehicle charging measurements in sounding rocket and space shuttle orbiter environments at Low Earth Orbit (LEO) altitudeIt was concluded that for electron beam emission up to 100mA, vehicle charging is not a significant problem with the Space Shuttle Orbiter. Similarly, sounding rocket payloads have no serious charging problems up to this level of beam current, provided that the maximum amount of the rocket skin is available to collect ionospheric electrons from the LEO altitude range. However, sounding rockets are marginal in their collecting area capability and other effects may occur to balance the beam current when operated at lower altitudes during the night.
Document ID
19870017512
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Raitt, W. J.
(Utah State Univ. Logan, UT, United States)
Eccles, J. V.
(Utah State Univ. Logan, UT, United States)
Myers, N. B.
(Utah State Univ. Logan, UT, United States)
Thompson, D. C.
(Utah State Univ. Logan, UT, United States)
Banks, P. M.
(Utah State Univ. Logan, UT, United States)
Williamson, P. R.
(Utah State Univ. Logan, UT, United States)
Bush, R. I.
(Utah State Univ. Logan, UT, United States)
Hawkins, J.
(Utah State Univ. Logan, UT, United States)
Sasaki, S.
(Utah State Univ. Logan, UT, United States)
Oyama, K.-I.
(Tokyo Univ. Japan)
Date Acquired
September 5, 2013
Publication Date
May 1, 1987
Publication Information
Publication: AGARD, The Aerospace Environment at High Altitudes and its Implications for Spacecraft Charging and Communications
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N26945
Funding Number(s)
CONTRACT_GRANT: NAS8-36011
CONTRACT_GRANT: F19628-86-K-0015
Distribution Limits
Public
Copyright
Other
Document Inquiry

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