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Composite reinforced propellant tanksDesign studies involving weight and cost were carried out for several structural concepts applicable to space shuttle disposable tankage. An effective design, a honeycomb stabilized pressure vessel, was chosen. A test model was designed and fabricated.
Document ID
19750013268
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Brown, L. D. (Grumman Aerospace Corp. Bethpage, NY, United States)
Martin, M. J. (Grumman Aerospace Corp. Bethpage, NY, United States)
Aleck, B. J. (Grumman Aerospace Corp. Bethpage, NY, United States)
Landes, R. (Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-134726
Report Number: NASA-CR-134726
Accession Number
75N21340
Funding Number(s)
CONTRACT_GRANT: NAS3-14368
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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