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Author

Title The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles [electronic resource] / A.T. Nettles, A.J. Hodge, 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/gpo10728/20110008313_2011008132.pdf
Connect to https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20110008313.pdf

Location	Call No.	OPAC Message	Status
Axe Federal Documents Online	NAS 1.60:2011-216457	---	Available

Description	1 online resource (vii, 23 p.) : ill.
Series	NASA/TP ; 2011-216457
	NASA technical paper ; 216457.
Note	Title from title screen (viewed on Aug. 2, 2011).
	"February 2011."
Bibliography	Includes bibliographical references (p. 22-23).
Subject	Damage assessment.
	Launch vehicles.
	Thermal protection.
	Sandwich structures.
	Residual strength.
	Ares 1 launch vehicle.
	Composite structures.
	Composite materials.
	Impact damage.
Added Author	Hodge, A. J.
	Jackson, J. R.
	George C. Marshall Space Flight Center.
Gpo Item No.	0830-H-15 (online)
Sudoc No.	NAS 1.60:2011-216457