NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Spacecraft-environment interaction: The environmental plasma aspectThe effects involved in the interaction between an obstacle and a space plasma can be divided into: (1) effects on the obstacle itselt (i.e., its charging); and (2) effects on the environmental plasma due to the motion of the obstacle (i.e., the creation of shocks ahead of the obstacle and complicated wakes behind the obstacle). In the wake (or antisolar direction), plasma oscillations are excited and instabilities, wave-particle interactions, turbulence, etc., are believed to take place. The effects on the obstacle and on the environmental space plasma are coupled. Hence, simultaneous solutions to the Vlasov (or Boltzmann) and Poisson equations are sought. To obtain realistic solutions of practical use, three-dimensional and time-dependent models of the interaction are needed. Achieving the latter is indeed not simple.
Document ID
19850014168
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Samir, U.
(Michigan Univ. Ann Arbor, MI, United States)
Date Acquired
August 12, 2013
Publication Date
March 1, 1985
Publication Information
Publication: NASA. Lewis Research Center Spacecraft Environ. Interactions Technol., 1983
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
85N22479
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available