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The aerodynamics of bodies in a rarefied ionized gas with applications to spacecraft environmental dynamicsThe objectives are to provide a parametric description of the electrostatic interaction of a mesosonic, collisionless plasma with conducting bodies on the order of 1 to 10 Debye lengths in size, and to extend this description to the satellite-ionospheric interaction, where possible. Experimental findings include: the wake of the geometrically complex body appears to be a linear superposition of the wakes of its simple geometric components; and vector ion flux measurements show converging ion streams at the wake axis and direct evidence of ion streams deflected from the wake axis by the positive space charge potential associated with the axial ion peak. The extension to the satellite-ionospheric interaction utilizes qualitative scaling and indicates that similar, but smaller amplitude, wake structures may be expected for small or highly charged bodies. However, for large bodies at small potentials, the structure may be diffused by the thermal ion motion and the dispersion resulting for space charge potentials.
Document ID
19820007243
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Stone, N. H.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1981
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
M-361
NASA-TP-1933
Report Number: M-361
Report Number: NASA-TP-1933
Accession Number
82N15116
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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