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.

Saved in:

Bibliographic Details
Online Access:	Online Access Online Access
Main Author:	Hodge, A. J.
Corporate Author:	George C. Marshall Space Flight Center
Other Authors:	Nettles, A. T. (Alan T.), Jackson, J. R.
Format:	Government Document Electronic eBook
Language:	English
Published:	[Huntsville], Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]
Series:	NASA technical paper ; 216460.
Subjects:	Compressive strength. Sandwich structures. Carbon fibers. Impact strength. Damage. Epoxy matrix composites. Laminates. Fiber composites.

Internet

Online Access
Online Access

Holdings details from Online
Call Number:	NAS 1.60:2011-216460
NAS 1.60:2011-216460	Available