| LDR | 01251cam a2200313Ia 4500 | ||
| 001 | 100233701 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 091109s1963 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6365742 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)464226980 |
| 040 | ⊔ | ⊔ | ‡aCSL ‡cTEF ‡dOCL |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 050 | ⊔ | 4 | ‡aTL789.8.U6 ‡bO83 1963 |
| 100 | 1 | ⊔ | ‡aOsborne, Robert S. |
| 245 | 1 | 0 | ‡aStability and control characteristics of a 0.0667-scale model of the final version of the North American X-15 research airplane (configuration 3) at transonic speeds / ‡cby Robert S. Osborne. |
| 260 | ⊔ | ⊔ | ‡aWashington, [DC] : ‡bNational Aeronautics and Space Administration, ‡c[1963] |
| 300 | ⊔ | ⊔ | ‡a102 p. : ‡bill. ; ‡c27 cm. |
| 490 | 0 | ⊔ | ‡aNASA TM ; ‡vX-758 |
| 500 | ⊔ | ⊔ | ‡a"April 1963." |
| 500 | ⊔ | ⊔ | ‡aCover title. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 8). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aAerodynamics, Transonic. |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xHandling characteristics ‡xTesting. |
| 650 | ⊔ | 0 | ‡aStability of airplanes ‡xTesting. |
| 650 | ⊔ | 0 | ‡aX-15 (Rocket aircraft) ‡xModels ‡xTesting. |
| 700 | 1 | ⊔ | ‡aWare, George M. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a100233701 |
| DAT | 0 | ⊔ | ‡a20101008091734.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112165512.0 ‡b2024-01-24T18:37:19Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6365742 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106664813 ‡sUIU ‡16365742 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20240124 ‡sgoogle ‡uuiug.30112106664813 ‡y1963 ‡rpd ‡qbib ‡tUS fed doc |