The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles
By: A.T. Nettles, A.J. Hodge, and J.R. Jackson
Contributors: Hodge, A. J.; Jackson, J. R.; George C. Marshall Space Flight Center
Series: NASA/TP -- 2011-216457; NASA technical paper -- 216457.
Publisher: National Aeronautics and Space Administration, Marshall Space Flight Center
Published: 2011
Place of publication: Huntsville], Ala
Language: eng
Format: [electronic resource] /
Number of pages: 23
Subjects: Damage assessment; Launch vehicles; Thermal protection; Sandwich structures; Residual strength; Ares 1 launch vehicle; Composite structures; Composite materials; Impact damage
Notes: Title from title screen (viewed on Aug. 2, 2011).

"February 2011."

Includes bibliographical references (p. 22-23).