NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Design and fabrication of a skin stringer discrete tube actively cooled structural panelThe design optimization and practical implementation of actively cooled structural panel concepts was investigated. The desired actively cooled structural panel consisted of the cooled skin and a substructure. The primary load carrying components were fabricated from 2024-T3 aliminum alloy. The 3003-H14 coolant passage tubing was chosen because of its excellent corrosion resistance, workability needed to obtain the desired cross sectional shape, and strength. The Epon 951 adhesive was selected for its excellent structural properties and is the thinnest of available films, 0.064 mm. The Eccobond 58C silver filled epoxy was chosen because of its high thermal conductivity, and the alumina filled Epon 828 was chosen for structural and expansion characteristics.
Document ID
19790013259
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anthony, F. M. (Textron Bell Aerospace Co. Buffalo, NY, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: NASA. Langley Res. Center Recent Advan. in Structures for Hypersonic Flight, Pt. 1
Subject Category
Structural Mechanics
Accession Number
79N21430
Funding Number(s)
CONTRACT_GRANT: NAS1-12806
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19790013251Collected WorksRecent Advances in Structures for Hypersonic Flight, Part 119790013251Collected WorksRecent Advances in Structures for Hypersonic Flight, Part 1
No Preview Available