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| 001 | 011444548 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 070518s1968 dcua b 000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6401967 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)131278775 |
| 040 | ⊔ | ⊔ | ‡aEGM ‡cEGM |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 100 | 1 | ⊔ | ‡aAdelman, Howard M. |
| 245 | 1 | 0 | ‡aVibration analysis of a 1/40-scale dynamic model of Saturn V -- launch-platform -- umbilical-tower configuration / ‡cHoward M. Adelman and Earl C. Steeves. |
| 246 | 3 | ⊔ | ‡aNASA TN D-4871 |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡aSpringfield, Va. : ‡bFor sale by the Clearinghouse for Federal Scientific and Technical Information, ‡c1968. |
| 300 | ⊔ | ⊔ | ‡a58 p. : ‡bill. ; ‡c27 cm. |
| 490 | ⊔ | 0 | ‡aNASA technical note ; ‡v4871 |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 26). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aMathematical models. |
| 650 | ⊔ | 0 | ‡aFinite element method. |
| 650 | ⊔ | 0 | ‡aSaturn launch vehicles ‡xTesting. |
| 650 | ⊔ | 0 | ‡aLaunch complexes (Astronautics) ‡xVibration ‡xMeasurement. |
| 700 | 1 | ⊔ | ‡aSteeves, Earl C. |
| 710 | 2 | ⊔ | ‡aLangley Research Center. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a011444548 |
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| DAT | 1 | ⊔ | ‡a20141112165512.0 ‡b2024-01-24T18:37:43Z |
| DAT | 2 | ⊔ | ‡a2024-01-24T18:30:02Z ‡b2020-08-29T20:00:02Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
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| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20240124 ‡sgoogle ‡uuiug.30112106746388 ‡y1968 ‡rpdus ‡qgfv |