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Solar array flight experimentThis is a closed form solution for the longitudinal oscillation of the Solar Array Flight Experiment (SAFE) blanket for all phases of deployment. The frequency response shows that the blanket frequency increases shortly before full deployment. That fact causes a coupling between the mast and the blanket frequency but, because of the relatively high speed of deployment, a buildup of resonance is unlikely.
Document ID
19850019623
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Slaby, J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1985
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:86506
NASA-TM-86506
Report Number: NAS 1.15:86506
Report Number: NASA-TM-86506
Accession Number
85N27935
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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