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Modeling of LDEF contamination environmentThe Long Duration Exposure Facility (LDEF) satellite was unique in many ways. It was a large structure that was in space for an extended period of time and was stable in orientation relative to the velocity vector. There are obvious and well documented effects of contamination and space environment effects on the LDEF satellite. In order to examine the interaction of LDEF with its environment and the resulting effect on the satellite, the Integrated Spacecraft Environments Model (ISEM) was used to model the LDEF-induced neutral environment at several different times and altitudes during the mission.
Document ID
19940026514
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Carruth, M. Ralph, Jr.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Rantanen, Ray
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Gordon, Tim
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1993
Publication Information
Publication: LDEF Materials Results for Spacecraft Applications
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
94N31019
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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