| LDR | 01158nam a2200301Ia 4500 | ||
| 001 | 100233740 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 100127s1959 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6357737 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)502141669 |
| 040 | ⊔ | ⊔ | ‡aCSL ‡cTEF |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 050 | ⊔ | 4 | ‡aTL574.S7 ‡bF67 1959 |
| 100 | 1 | ⊔ | ‡aFoster, Gerald V. |
| 245 | 1 | 0 | ‡aStatic stability characteristics of a series of hypersonic boost-glide configurations at mach numbers of 1.41 and 2.01 / ‡cby Gerald V. Foster. |
| 260 | ⊔ | ⊔ | ‡aWashington [D.C.] : ‡bNational Aeronautics and Space Administration, ‡c[1959] |
| 300 | ⊔ | ⊔ | ‡a85 p. : ‡b36 ill. ; ‡c27 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical memorandum ; ‡vX-167 |
| 500 | ⊔ | ⊔ | ‡a"November 1959." |
| 500 | ⊔ | ⊔ | ‡aCover title. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 12). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aGliders (Aeronautics) |
| 650 | ⊔ | 0 | ‡aHypersonic planes. |
| 650 | ⊔ | 0 | ‡aStability of airplanes, Lateral. |
| 650 | ⊔ | 0 | ‡aStability of airplanes, Longitudinal. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a100233740 |
| DAT | 0 | ⊔ | ‡a20101001124318.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112165512.0 ‡b2024-01-26T18:54:00Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6357737 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106713461 ‡sUIU ‡16357737 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20240126 ‡sgoogle ‡uuiug.30112106713461 ‡y1959 ‡rpd ‡qbib ‡tUS fed doc |