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European technology on composite materialsThe following advanced composite materials were evaluated for future space shuttle applications: (1) Carbon and boron fiber composites using epoxy and polyimide as resins for stringer and skin panels: (2) high pressure steel tanks where the cylindrical part is reinforced by carbon fiber; and (3) an orbiter cargo door in boron fiber and polyimide resin.
Document ID
19720023236
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fray, J. (Hawker Siddeley Dyn. Ltd. Paris, France)
Kitchenside, A. W. (Brit. Aircraft Corp.)
Cools, J. J. (Roy. Neth. Aircraft Factories Fokker)
Hanselmann, C. P. H. (Maschinenfabrik Augsburg-Nuernberg A.G.)
Jonke, R. J. (European Space Vehicle Launcher Development Organization)
Date Acquired
August 6, 2013
Publication Date
July 1, 1972
Publication Information
Publication: NASA, Washington NASA Space Shuttle Technol. Conf.
Subject Category
Materials, Nonmetallic
Accession Number
72N30886
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19720023215Collected WorksNASA Space Shuttle Technology Conference: Dynamics and Aeroelasticity; Structures and MaterialsN72-30865 21-31Collected Works
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