NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Filament-wound graphite/epoxy rocket motor caseThe fabrication procedures are described for a filament-wound rocket motor case, approximately 56 cm long x 71 cm diameter, utilizing high tensile strength graphite fibers. The process utilized Fiberite Hy-E-1330B prepreg tape which consists of Courtaulds HTS fibers in a temperature-sensitive epoxy matrix. This fabrication effort, with resultant design, material and process recommendations, substantiates the manufacturing feasibility of graphite/epoxy rocket motor cases in the 56 cm x 71 cm size range.
Document ID
19720025116
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Humphrey, W. D. (Brunswick Corp. Lincoln, NE, United States)
Schmidt, W. W. (Brunswick Corp. Lincoln, NE, United States)
Date Acquired
August 6, 2013
Publication Date
July 15, 1972
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-128417
BC-8845-FAB
Report Number: NASA-CR-128417
Report Number: BC-8845-FAB
Accession Number
72N32766
Funding Number(s)
CONTRACT_GRANT: JPL-953210
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available