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The sheath structure around a negatively charged rocket payloadThe sheath structure around a rocket payload charged up to 460 V negative relative to the ambient ionospheric plasma is investigated experimentally and by computer simulations. The experimental results come from the Charge 2 sounding rocket experiment in which the payload was split into two separate sections (mother and daughter) connected with a conducting, insulated tether. In one of the experimental modes, the voltage between the payloads was increased linearly from 0 to 460 V in 2.5 s. A floating probe array was mounted on the mother with probes located 25, 50, 75, and 100 cm from the rocket surface. The internal impedance of the array was smaller than the probe/plasma impedance, which influenced the potential measurements. The measurements contain signatures, resulting from the outward expansion of the ion sheath with increasing negative mother potential. This conclusion is substantiated by computer simulations of space charge limited flow.
Document ID
19900047725
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Neubert, T.
(Stanford Univ. CA, United States)
Gilchrist, B. E.
(Stanford Univ. CA, United States)
Banks, P. M.
(Stanford University CA, United States)
Mandell, M. J.
(Maxwell Laboratories, Inc. La Jolla, CA, United States)
Sasaki, S.
(Institute for Space and Astronautical Sciences Tokyo, Japan)
Date Acquired
August 14, 2013
Publication Date
May 1, 1990
Publication Information
Publication: Journal of Geophysical Research
Volume: 95
ISSN: 0148-0227
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
90A34780
Funding Number(s)
CONTRACT_GRANT: NAS8-35350
CONTRACT_GRANT: NAG5-607
CONTRACT_GRANT: NAS3-23881
CONTRACT_GRANT: NAGW-1566
Distribution Limits
Public
Copyright
Other

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