An examination of impact damage in glass/phenolic and aluminum honeycomb core composite panels
By: A.T. Nettles, D.G. Lance, and A.J. Hodge.
Contributors: Lance, D. G.; Hodge, A. J.; George C. Marshall Space Flight Center.
Series: NASA technical paper -- 3042.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1990
Place of publication: Washington, D.C; [Springfield, VA
Language: eng
Format: Microform
Subjects: Honeycomb structures -- Testing.; Composite materials -- Testing.; Impact.; Glass.; Phenolic resins.; Aluminum.; Aluminum.; Glass fiber reinforced plastics.; Graphite-epoxy composites.; Honeycomb cores.; Impact damage.; Phenolic resins.; Sandwich structures.
Notes: Prepared at the George C. Marshall Space Flight Center.

Also available via Internet from the NASA Technical Report Server web site. Address as of 12/15/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900018560%5F1990018560.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 1 microfiche.