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Permeability Testing Of Composite Material And Adhesive Bonds For The Dc Xa Composite Feedline Program by Alan T. Nettles
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1NASA Technical Reports Server (NTRS) 19950017131: Permeability Testing Of Composite Material And Adhesive Bonds For The DC-XA Composite Feedline Program
By NASA Technical Reports Server (NTRS)
Hercules IM7/8552 carbon/epoxy and Hysol EA 9394 epoxy adhesive bonded between composite/titanium were tested for permeability after various numbers of thermal cycles between 100 C and liquid nitrogen (-196 C). The specimens were quenched from the 100 C temperature into liquid nitrogen to induce thermal shock into the material. Results showed that the carbon/epoxy system was practically impermeable even after 12 thermal cycles. The EA 9394 adhesive bondline was more permeable than the carbon/epoxy, but vacuum mixing minimized the permeability and kept it within allowable limits. Thermal cycling had little effect on the permeability values of the bondline specimens.
“NASA Technical Reports Server (NTRS) 19950017131: Permeability Testing Of Composite Material And Adhesive Bonds For The DC-XA Composite Feedline Program” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19950017131: Permeability Testing Of Composite Material And Adhesive Bonds For The DC-XA Composite Feedline Program
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19950017131: Permeability Testing Of Composite Material And Adhesive Bonds For The DC-XA Composite Feedline Program” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - ADHESIVE BONDING - COMPOSITE MATERIALS - EPOXY RESINS - PERMEABILITY - THERMAL CYCLING TESTS - BONDED JOINTS - LIQUID NITROGEN - THERMAL SHOCK - Nettles, A. T.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19950017131
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