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Feasibility study of a 110 watt per kilogram lightweight solar array systemAn investigation of the feasibility of a solar array panel subsystem which will produce 10,000 watts of electrical output at 1 A.U. with an overall beginning-of-life power-to-weight ratio of at least 110 watt/kg is reported. A description of the current baseline configuration which meets these requirements is presented. A parametric analysis of the single boom, two blanket planar solar array system was performed to arrive at the optimum system aspect ratio. A novel concept for the stiffening of a lightweight solar array by canting the solar cell blankets at a small angle to take advantage of the inherent in-plane stiffness to increase the symmetric out-of-plane frequency is introduced along with a preliminary analysis of the stiffening effect. A comparison of welded and soldered solar cell interconnections leads to the conclusion that welding is required on this ultralightweight solar array. The use of a boron/aluminum composite material in a BI-STEM type deployable boom is investigated as a possible advancement in the state-of-the-art.
Document ID
19730006352
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Shepard, N. F.
(General Electric Co. Philadelphia, PA, United States)
Stahle, C. V.
(General Electric Co. Philadelphia, PA, United States)
Schneider, A.
(General Electric Co. Philadelphia, PA, United States)
Hanson, K. L.
(General Electric Co. Philadelphia, PA, United States)
Date Acquired
September 2, 2013
Publication Date
November 15, 1972
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-CR-130287
QR-2
DOC-72SD4249
Report Number: NASA-CR-130287
Report Number: QR-2
Report Number: DOC-72SD4249
Accession Number
73N15079
Funding Number(s)
CONTRACT_GRANT: NAS7-100
CONTRACT_GRANT: JPL-953387
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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