NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A damage tolerance comparison of IM7/8551 and IM8G/8553 carbon/epoxy compositesA damage tolerance study of two new toughened carbon fiber/epoxy resin systems was undertaken as a continuation of ongoing work into screening new opposites for resistance to foreign object impact. This report is intended to be a supplement to NASA TP 3029 in which four new fiber/resin systems were tested for damage tolerance. Instrumented drop weight impact testing was used to inflict damage to 16-ply quasi-isotropic specimens. Instrumented output data and cross-sectional examinations of the damage zone were utilized to quantify the damage. It was found that the two fiber/resin systems tested in this study were much more impact resistant than an untoughened composite such as T300/934, but were not as impact resistant as other materials previously studied.
Document ID
19910008909
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lance, D. G.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Nettles, A. T.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1991
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-103526
NAS 1.15:103526
Report Number: NASA-TM-103526
Report Number: NAS 1.15:103526
Accession Number
91N18222
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available