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003 OCoLC;

005 20120622101917.0;

006 m d f ;

007 cr m||||||||||;

008 120622s2011 alua obt f000 0 eng c;

040 a| GPOc| GPOd| MvI;

042 a| pcc;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:2011-216477;

100 1 a| Nettles, A. T.q| (Alan T.)=| ^A573713;

245 12 a| A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications /c| A.T. Nettles.;

260 a| Huntsville, Ala. :b| National Aeronautics and Space Administration, Marshall Space Flight Center,c| [2011];

300 a| 1 online resource (vii, 39 p.) :b| ill. (some col.);

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA/TM ;v| 2011-216477;

500 a| Title from title screen (viewed on June 22, 2012).;

500 a| "December 2011.";

500 a| GPO Cataloging Record Distribution Program (CRDP).;

504 a| Includes bibliographical references (p. 39).;

536 a| Sponsored by National Aeronautics and Space Administrationd| M-1326;

650 7 a| Compressive strength.2| nasat;

650 7 a| Impact strength.2| nasat;

650 7 a| Honeycomb structures.2| nasat;

650 7 a| Launch vehicles.2| nasat;

650 7 a| Damage.2| nasat;

650 7 a| Tolerances (mechanics).2| nasat;

650 7 a| Residual strength.2| nasat;

710 2 a| George C. Marshall Space Flight Center.=| ^A77995;

830 0 a| NASA technical memorandumv| 2011-216477.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo24323;

949 a| Click on web addressw| asish| joyner94;

596 a| 1;

998 a| 3089470;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 3089470-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 8/7/2012x| EDOCUMENTz| JERESOURCE;

A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications / A.T. Nettles.

Author/creator	Nettles, A. T.
Other author	George C. Marshall Space Flight Center.
Format	Electronic
Publication Info	Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]
Description	1 online resource (vii, 39 p.) : ill. (some col.)
Supplemental Content	https://purl.fdlp.gov/GPO/gpo24323

Series	NASA/TM ; 2011-216477 NASA technical memorandum 2011-216477. ^A467613
General note	Title from title screen (viewed on June 22, 2012).
General note	"December 2011."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 39).
Funding information	Sponsored by National Aeronautics and Space Administration M-1326
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:2011-216477

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A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications / A.T. Nettles.

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