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Design of a unidirectional composite momentum wheel rimA preliminary study comparing twelve unidirectional-fiber composite systems to five metal materials conventionally used in momentum wheels is presented. Six different fibers are considered in the study: E-Glass, S-Glass, Boron, AS, T300, and Kevlar. Because of the possibility of high momentum requirements, and thus high stresses, only two matrix materials are considered: a high-modulus (HM) and a intermediate-modulus-high-strength (IMHS) matrix. Each of the six fibers are coupled with each of the two matrix materials. In an effort to optimize the composite system, each composite is considered while varying the fiber volume ratio from 0.0 to 0.7 in increments of 0.1. For fiber volume ratios above 0.2, all twelve unidirectional-fiber composite systems meet the study's requirements with higher factors of safety and less mass than the five conventional isotropic (metal) materials. For example, at a fiber volume ratio of 0.6, the Kevlar/IMHS composite system has a safety factor 4.5 times greater than that of a steel (maraging) system and an approximately 10 percent reduction in weight.
Document ID
19950021340
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Shogrin, Bradley
(Case Western Reserve Univ. Cleveland, OH., United States)
Jones, William R., Jr.
(NASA Lewis Research Center Cleveland, OH, United States)
Prahl, Joseph M.
(Case Western Reserve Univ. Cleveland, OH., United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1995
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-106911
E-9613
NAS 1.15:106911
Report Number: NASA-TM-106911
Report Number: E-9613
Report Number: NAS 1.15:106911
Accession Number
95N27761
Funding Number(s)
PROJECT: RTOP 274-00-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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