Research Catalog

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

Title
A quantitative damage tolerance comparison of high strength and high modulus carbon fiber sandwich structure / A.T. Nettles, W.E. Guin, and C.C. Wolfe.
Author
Nettles, A. T. (Alan T.)
Publication
Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, January 2022.

Available Online

https://purl.fdlp.gov/GPO/gpo174309

Details

Additional Authors
  • Guin, W. E.
  • Wolfe, C. C.
  • George C. Marshall Space Flight Center, issuing body.
Description
1 online resource (approximately 30 pages) : illustrations (some color).
Series Statement
NASA/TM ; 20210026811
Uniform Title
NASA technical memorandum ; 20210026811.
Subject
  • Composite materials
  • Sandwich structures
  • Carbon fibers
Note
  • "January 2022."
Bibliography (note)
  • Includes bibliographical references (page 17).
Type of Report (note)
  • Technical memorandum.
Source of Description (note)
  • Description based on online resource, PDF version; title from title page (NASA, viewed on Jan. 26, 2022).
Call Number
GPO Internet NAS 1.15:20210026811
OCLC
marcive1293754032
Author
Nettles, A. T. (Alan T.), author.
Title
A quantitative damage tolerance comparison of high strength and high modulus carbon fiber sandwich structure / A.T. Nettles, W.E. Guin, and C.C. Wolfe.
Publisher
Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, January 2022.
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA/TM ; 20210026811
NASA technical memorandum ; 20210026811.
Bibliography
Includes bibliographical references (page 17).
Type Of Report
Technical memorandum.
Connect to:
https://purl.fdlp.gov/GPO/gpo174309
Added Author
Guin, W. E., author.
Wolfe, C. C., author.
George C. Marshall Space Flight Center, issuing body.
Gpo Item No.
0830-D (online)
Sudoc No.
NAS 1.15:20210026811
View in Legacy Catalog