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| 001 | 011447633 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
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| 007 | cr bn ---auaua | ||
| 008 | 050908s1961 dcu b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6392632 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)61452585 |
| 040 | ⊔ | ⊔ | ‡aAD# ‡cAD# |
| 041 | 0 | ⊔ | ‡aeng |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 086 | 0 | ⊔ | ‡aNAS 1.14:D-803 |
| 088 | ⊔ | ⊔ | ‡aNAS-TN-D-803 |
| 100 | 1 | ⊔ | ‡aGrantham, William D. |
| 245 | 0 | 0 | ‡aEffects of mass-loading variations and applied moments on motion and control of a manned rotating space vehicle. / ‡cby William D. Grantham |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Office of Technical Services, Dept. of Commerce], ‡c[1961] |
| 300 | ⊔ | ⊔ | ‡a40 p. : ‡bill. ; ‡c26 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical note ; ‡vNASA TN D-803 |
| 500 | ⊔ | ⊔ | ‡aCover title. |
| 500 | ⊔ | ⊔ | ‡a"May 1961." |
| 500 | ⊔ | ⊔ | ‡aSatellites; Stability and control. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 7 | ‡aStability and control ‡2nasat |
| 650 | ⊔ | 7 | ‡aSatellites ‡2nasat |
| 710 | 2 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a011447633 |
| DAT | 0 | ⊔ | ‡a20101103092928.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112165512.0 ‡b2023-03-14T18:29:54Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
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| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106740480 ‡y1961 ‡rpd ‡qbib ‡tUS fed doc |