| LDR | 01341cam a2200325Ia 4500 | ||
| 001 | 011442802 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 070404s1968 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6395286 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)122352686 |
| 040 | ⊔ | ⊔ | ‡aAD# ‡cAD# ‡dEGM |
| 041 | 0 | ⊔ | ‡aeng |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 086 | 0 | ⊔ | ‡aNAS 1.14:D-4393 |
| 088 | ⊔ | ⊔ | ‡aNASA-TN-D-4393 |
| 100 | 1 | ⊔ | ‡aStabe, Roy G. |
| 245 | 1 | 0 | ‡aCold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. ‡nIV, ‡pPerformance of first stage with modified inlet feedpipe-manifold assembly / ‡cRoy G. Stabe, John F. Kline. |
| 246 | 3 | ⊔ | ‡aNASA TN D-4393 |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡aSpringfield, VA : ‡bFor sale by the Clearinghouse for Federal Scientific and Technical Information, ‡c1968. |
| 300 | ⊔ | ⊔ | ‡a21 p. : ‡bill. ; ‡c26 cm. |
| 490 | ⊔ | 0 | ‡aNASA technical note ; ‡vD-4393 |
| 500 | ⊔ | ⊔ | ‡aCover title. |
| 500 | ⊔ | ⊔ | ‡a"February 1968." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 20-21). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aTurbine pumps ‡xTesting. |
| 650 | ⊔ | 0 | ‡aRocket engines ‡xModels. |
| 700 | 1 | ⊔ | ‡aKline, John F. |
| 710 | 2 | ⊔ | ‡aLewis Research Center. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a011442802 |
| DAT | 0 | ⊔ | ‡a20101104142321.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112165512.0 ‡b2023-12-12T18:45:31Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6395286 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106871632 ‡sUIU ‡16395286 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20231212 ‡sgoogle ‡uuiug.30112106871632 ‡y1968 ‡rpd ‡qbib ‡tUS fed doc |