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LDEF yaw and pitch angle estimatesQuantification of the LDEF yaw and pitch misorientations is crucial to the knowledge of atomic oxygen exposure of samples placed on LDEF. Video camera documentation of the LDEF spacecraft prior to grapple attachment, atomic oxygen shadows on experiment trays and longerons, and a pinhole atomic oxygen camera placed on LDEF provided sources of documentation of the yaw and pitch misorientation. Based on uncertainty-weighted averaging of data, the LDEF yaw offset was found to be 8.1 plus or minus 0.6 degrees, allowing higher atomic oxygen exposure of row 12 than initially anticipated. The LDEF pitch angle offset was found to be 0.8 plus or minus 0.4 degrees, such that the space end was tipped forward toward the direction of travel. The resulting consequences of the yaw and pitch misorientation of LDEF on the atomic oxygen fluence is a factor of 2.16 increase for samples located on row 12, and a factor of 1.18 increase for samples located on the space end compared to that which would be expected for perfect orientation.
Document ID
19930003584
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Banks, Bruce A.
(NASA Lewis Research Center Cleveland, OH, United States)
Gebauer, Linda
(Cleveland State Univ. OH., United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1992
Publication Information
Publication: NASA. Langley Research Center, LDEF Materials Workshop 1991, Part 1
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93N12772
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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