| LDR | 01111nam a2200289Ia 4500 | ||
| 001 | 100233619 | ||
| 003 | MiAaHDL | ||
| 005 | 20140825000000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 891108s1989 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6346560 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)20612928 |
| 040 | ⊔ | ⊔ | ‡aABC ‡cABC |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 090 | ⊔ | ⊔ | ‡aTL521.3 ‡b.N18 no. 2950 |
| 100 | 1 | ⊔ | ‡aFunk, Joan G. |
| 245 | 1 | 4 | ‡aThe interlaminar fracture toughness of woven graphite/epoxy composites / ‡cJoan G. Funk and Jerry W. Deaton. |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1989. |
| 300 | ⊔ | ⊔ | ‡a26 p. : ‡bill. ; ‡c28 cm. |
| 490 | ⊔ | 0 | ‡aNASA technical paper ; ‡v2950 |
| 500 | ⊔ | ⊔ | ‡aResearch performed at Langley Research Center. |
| 504 | ⊔ | ⊔ | ‡aBibliography: p. 6. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aGraphite fibers. |
| 650 | ⊔ | 0 | ‡aEpoxy resins. |
| 650 | ⊔ | 0 | ‡aFibrous composites ‡xTesting. |
| 650 | ⊔ | 0 | ‡aFibrous composites ‡xFracture. |
| 700 | 1 | ⊔ | ‡aDeaton, Jerry W. |
| 710 | 2 | ⊔ | ‡aLangley Research Center. |
| CID | ⊔ | ⊔ | ‡a100233619 |
| DAT | 0 | ⊔ | ‡a20100928155159.0 ‡b20140825000000.0 |
| DAT | 1 | ⊔ | ‡a20180312191600.0 ‡b2024-03-01T18:46:30Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lprepare.pl-004-007 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6346560 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106607820 ‡sUIU ‡16346560 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20240301 ‡sgoogle ‡uuiug.30112106607820 ‡y1989 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2018 |