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Boron/aluminum for space applicationsSeveral experimental boron/aluminum structures have been built for aircraft and space vehicle applications. The success of these structures has led to the decision to use boron/aluminum tubular struts on the mid-fuselage section of the Space Shuttle Orbiter. The suitability of boron/aluminum for this application has been demonstrated in a program that involved fabricating 100 tubes and performing static, fatigue, corrosion, thermal/mechanical fatigue, and damage tolerance tests on them. Other potential applications for boron/aluminum on the Space Shuttle include the wing carry-through panels and side panels for the mid-fuselage, and the landing gear struts. These applications result in significant weight savings over conventional non-composite designs at moderate costs. Boron/aluminum can now be considered a production material that, in many cases, is competitive on a weight and/or cost basis with an all-metal or resin composite system.
Document ID
19750028976
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Robertson, A. R.
Miller, M. F.
(General Dynamics Corp. Convair Aerospace Div., San Diego, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1974
Subject Category
Composite Materials
Meeting Information
Meeting: Materials on the move; Sixth National Technical Conference
Location: Dayton, OH
Start Date: October 8, 1974
End Date: October 10, 1974
Accession Number
75A13048
Funding Number(s)
CONTRACT_GRANT: F33615-72-C-1460
CONTRACT_GRANT: NAS8-27738
CONTRACT_GRANT: F33615-74-C-5151
Distribution Limits
Public
Copyright
Other

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