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Design and Fabrication of a Ring-Stiffened Graphite-Epoxy Corrugated Cylindrical ShellDesign and fabrication of supplement test panels that represent key portions of the cylinder are described, as are supporting tests of coupons, sample joints, and stiffening ring elements. The cylindrical shell is a ring-stiffened, open corrugation design that uses T300/5208 graphite-epoxy tape as the basic material for the shell wall and stiffening rings. The test cylinder is designed to withstand bending loads producing the relatively low maximum load intensity in the shell wall of 1,576 N/cm. The resulting shell wall weight, including stiffening rings and fasteners, is 0.0156 kg/m. The shell weight achieved in the graphite-epoxy cylinder represents a weight saving of approximately 23 percent, compared to a comparable aluminum shell. A unique fabrication approach was used in which the cylinder wall was built in three flat segments, which were then wrapped to the cylindrical shape. Such an approach, made possible by the flexibility of the thin corrugated wall in a radial direction, proved to be a simple approach to building the test cylinder. Based on tooling and fabrication methods in this program, the projected costs of a production run of 100 units are reported.
Document ID
19780023522
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Johnson, R., Jr.
(McDonnell-Douglas Astronautics Co. Huntington Beach, CA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1978
Subject Category
Structural Mechanics
Report/Patent Number
MDC-G7330
NASA-CR-3026
Report Number: MDC-G7330
Report Number: NASA-CR-3026
Accession Number
78N31465
Funding Number(s)
CONTRACT_GRANT: NAS1-14547
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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