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003 OCoLC;

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007 he bmb024bbca;

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037 a| N 90-25374b| NASA;

042 a| pcc;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:102678;

100 1 a| Poe, C. C.=| ^A447973;

245 10 a| Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case /c| C.C. Poe, Jr.;

260 a| Hampton, Va. :b| National Aeronautics and Space Administration, Langley Research Center,c| [1990];

300 a| 34 p. :b| ill.;

336 a| textb| txt2| rdacontent;

337 a| microformb| h2| rdamedia;

338 a| microficheb| he2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 102678;

500 a| Cover title.;

500 a| Shipping list no.: 90-1086-M.;

500 a| "June 1990.";

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

530 a| Also available via Internet from the NASA Technical Report Server web site. Address as of 3/3/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900016058%5F1990016058.pdf; current access available via PURL.;

504 a| Includes bibliographical references (p. 17-18).;

536 h| 505-63-01-05;

650 7 a| Critical pressure.2| nasat;

650 7 a| Graphite-epoxy composites.2| nasat;

650 7 a| Impact damage.2| nasat;

650 7 a| Low speed.2| nasat;

650 7 a| Residual strength.2| nasat;

650 7 a| Rocket engine cases.2| nasat;

710 2 a| Langley Research Center.=| ^A192893;

830 0 a| NASA technical memorandumv| 102678.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS58426;

949 a| NAS 1.15:102678w| sudoch| joyner32;

596 a| 1;

998 a| 992994;

999 a| NAS 1.15:102678w| SUDOCc| 1i| MQ1753366d| 8/7/2007l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 4/8/2005x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case / C.C. Poe, Jr.

Author/creator	Poe, C. C.
Other author	Langley Research Center.
Format	Microform
Publication Info	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
Description	34 p. : ill.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS58426
Subjects	Space shuttles--Propulsion systems. --Materials. --Impact testing.

Series	NASA technical memorandum ; 102678 NASA technical memorandum 102678. ^A467613
General note	Cover title.
General note	Shipping list no.: 90-1086-M.
General note	"June 1990."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 17-18).
Other forms	Also available via Internet from the NASA Technical Report Server web site. Address as of 3/3/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900016058%5F1990016058.pdf; current access available via PURL.
Reproduction note	Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990] 1 microfiche : negative.
Funding information	505-63-01-05
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:102678
Stock number	N 90-25374 NASA

Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case / C.C. Poe, Jr.

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