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Interactions between satellites and plasmaThe interactions of a spacecraft with the surrounding, streaming plasma were determined by the following effects: the fade out of the plasma in the wake of the probe, the emission of photoelectrons and secondary electrons, the differential charging of the surface of the probe, and a spatial potential distribution in the vicinity of the space probe. These effects and their importance are discussed and following plasma conditions are considered: (1) geostationary satellite orbits; (2) in the solar wind (HELIOS mission); and (3) in the ionosphere at an altitude of 250 km (the projected OSV on Spacelab). The fundamental models are reviewed.
Document ID
19840025380
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Isensee, U.
(NASA Headquarters Washington, DC United States)
Lehr, W.
(NASA Headquarters Washington, DC United States)
Maassberg, H.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1984
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-77476
NAS 1.15:77476
Report Number: NASA-TM-77476
Report Number: NAS 1.15:77476
Accession Number
84N33451
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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