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Atomic oxygen erosion considerations for spacecraft materials selectionThe Long Duration Exposure Facility (LDEF) satellite carried 57 experiments that were designed to define the low-Earth orbit (LEO) space environment and to evaluate the impact of this environment on potential engineering materials and material processes. Deployed by the Shuttle Challenger in April of 1984, LDEF made over 32,000 orbits before being retrieved nearly 6 years later by the Shuttle Columbia in January of 1990. The Solar Array Passive LDEF Experiment (SAMPLE) AO171 contained approximately 300 specimens, representing numerous material classes and material processes. AO171 was located on LDEF in position A8 at a yaw of 38.1 degrees from the ram direction and was subjected to an atomic oxygen (AO) fluence of 6.93 x 10(exp 21) atoms/sq cm. LDEF AO171 data, as well as short-term shuttle data, will be discussed in this paper as it applies to engineering design applications of composites, bulk and thin film polymers, glassy ceramics, thermal control paints, and metals subjected to AO erosion.
Document ID
19940026517
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Whitaker, Ann F.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Kamenetzky, Rachel R.
(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
Nonmetallic Materials
Accession Number
94N31022
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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