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Further observations of Space Shuttle plasma-electrodynamic effects from OSS-1/STS-3Recent analyses of ion measurements obtained from the Differential Ion Flux Probe (DIFP) on the deployed Plasma Diagnostics Package (PDP) during the OSS-1/STS-3 mission have provided an additional insight into the plasma-electrodynamics of the Space Shuttle Orbiter: (1) Measured ion flow directions and energies suggest that the disturbance created in the ionospheric plasma by the Shuttle Orbiter may be confined to an interaction region that extends on the order of 10 m in the forward direction and has a boundary thickness of about 2 m. (2) A correlation between the DIFP and pressure gauge measurements indicates a direct, local proportionality between the neutral gas and ion densities. (3) Preliminary results from a theoretical model of the possible interaction between measured secondary, high inclination ion streams and the ambient plasma indicate the generation of broad-band electrostatic noise such as that observed by wave instruments on the PDP.
Document ID
19860047269
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Stone, N. H.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hwang, K. S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Wright, K. H., Jr.
(Alabama, University Huntsville, United States)
Samir, U.
(Tel Aviv University Israel; Michigan, University, Ann Arbor, United States)
Murphy, G. B.
(Iowa, University Iowa City, United States)
Shawhan, S. D.
(NASA Headquarters Washington, DC United States)
Date Acquired
August 12, 2013
Publication Date
March 1, 1986
Publication Information
Publication: Geophysical Research Letters
Volume: 13
ISSN: 0094-8276
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
86A32007
Funding Number(s)
CONTRACT_GRANT: NGR-23-005-320
CONTRACT_GRANT: NAS8-33982
Distribution Limits
Public
Copyright
Other

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