A quantitative damage tolerance comparison of high strength and high modulus carbon fiber sandwich structure /

Bibliographic Details

Main Authors:	Nettles, A. T. (Alan T.) (Author), Guin, W. E. (Author), Wolfe, C. C. (Author)
Format:	Government Document eBook
Language:	English
Published:	Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, January 2022.
Series:	NASA technical memorandum ; 20210026811.
Subjects:	Composite materials. Sandwich structures. Carbon fibers.
Online Access:	https://purl.fdlp.gov/GPO/gpo174309