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Author

Title Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage [electronic resource] / A.J. Hodge, A.T. Nettles, and J.R. Jackson.

Imprint

[Huntsville], Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]

Connect to
Connect to https://permanent.fdlp.gov/gpo11790/201100086412011009079.pdf
Connect to https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20110008641.pdf

Copies

Location	Call No.	OPAC Message	Status
Axe Federal Documents Online	NAS 1.60:2011-216460	---	Available

Description	1 online resource (viii, 23 p.) : ill. (some col.)
Series	NASA/TP ; 2011-216460
	NASA technical paper ; 216460.
Note	Title from title screen (viewed on Aug. 22, 2011).
	"March 2011."
Bibliography	Includes bibliographical references (p. 22-23).
Subject	Compressive strength.
	Sandwich structures.
	Carbon fibers.
	Impact strength.
	Damage.
	Epoxy matrix composites.
	Laminates.
	Fiber composites.
Added Author	Nettles, A. T. (Alan T.)
	Jackson, J. R.
	George C. Marshall Space Flight Center.
Gpo Item No.	0830-H-15 (online)
Sudoc No.	NAS 1.60:2011-216460