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Space Station Freedom solar array containment box mechanismsSpace Station Freedom will feature six large solar arrays, called solar array wings, built by Lockheed Missiles & Space Company under contract to Rockwell International, Rocketdyne Division. Solar cells are mounted on flexible substrate panels which are hinged together to form a 'blanket.' Each wing is comprised of two blankets supported by a central mast, producing approximately 32 kW of power at beginning-of-life. During launch, the blankets are fan-folded and compressed to 1.5 percent of their deployed length into containment boxes. This paper describes the main containment box mechanisms designed to protect, deploy, and retract the solar array blankets: the latch, blanket restraint, tension, and guidewire mechanisms.
Document ID
19940028786
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Johnson, Mark E.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Haugen, Bert
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Anderson, Grant
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1994
Publication Information
Publication: NASA. Lewis Research Center, The 28th Aerospace Mechanisms Symposium
Subject Category
Energy Production And Conversion
Accession Number
94N33292
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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