| LDR | 01061cam a2200241Ia 4500 | ||
| 001 | 011433479 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 040806s1964 dcua b 000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6391148 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)56103523 |
| 040 | ⊔ | ⊔ | ‡aEGM ‡cEGM ‡dOCLCQ |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 100 | 1 | ⊔ | ‡aPyle, Jon S. |
| 245 | 1 | 0 | ‡aComparison of flight pressure measurements with wind-tunnel data and theory for the forward fuselage of the X-15 airplane at Mach numbers from 0.8 to 6.0 / ‡cJon S. Pyle. |
| 246 | 3 | ⊔ | ‡aNASA TN D-2241 |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Office of Technical Services, Dept. of Commerce], ‡c1964. |
| 300 | ⊔ | ⊔ | ‡a29 p. : ‡bill. ; ‡c27 cm. |
| 490 | ⊔ | 0 | ‡aNASA technical note ; ‡vD-2241 |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 7). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aX-15 (Rocket aircraft) ‡xDesign and construction. |
| 710 | 2 | ⊔ | ‡aFlight Research Center (U.S.) |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a011433479 |
| DAT | 0 | ⊔ | ‡a20101102100717.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112164151.0 ‡b2024-01-23T18:45:16Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6391148 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106866160 ‡sUIU ‡16391148 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20240123 ‡sgoogle ‡uuiug.30112106866160 ‡y1964 ‡ric ‡qbib ‡tUS bib date1 >= 1929 |