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An extendible structure for solar electric power in spaceThe needs of certain space experiments have required the development of a mechanism capable of extending solar array panels from a spacecraft in orbit, and of positioning the panels so they function effectively as solar collectors. Rather stringent design requirements were imposed by the power and configuration requirements of the spacecraft itself. Further, since high reliability was essential, a simple mechanism was called for.

The resulting design can be described as four "jack-in-the-box" modules, each containing a simple slider-crank device which extends and positions a solar panel in a single, continuous cycle. The modules have been fabricated and qualification tested and will be flight-tested in the near future.
Document ID
19660027427
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
Authors
D. E. Lindberg
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 3, 2013
Publication Date
May 19, 1966
Subject Category
Auxiliary Systems
Report/Patent Number
N66-36717
Meeting Information
Meeting: First Aerospace Mechanisms Symposium
Location: Santa Clara, CA
Country: US
Start Date: May 19, 1966
End Date: May 20, 1966
Sponsors: Lockheed Martin (United States), Jet Propulsion Lab
Accession Number
66N36717
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
EXPANDABLE STRUCTURE
SPACECRAFT POWER SUPPLY
SOLAR CELL
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