| LDR | 01265cam a2200301Ia 4500 | ||
| 001 | 011446207 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 050215s1965 dcua b 000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6404124 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)57663529 |
| 040 | ⊔ | ⊔ | ‡aegm ‡cEGM ‡dOCLCQ |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 100 | 1 | ⊔ | ‡aSzuch, John R. |
| 245 | 1 | 0 | ‡aInvestigation of the starting characteristics of the M-1 rocket engine using the analog computer / ‡cJohn R. Szuch, Leon M. Wenzel, and Robert J. Baumbick. |
| 246 | 3 | ⊔ | ‡aNASA TN D-3136 |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], ‡c1965. |
| 300 | ⊔ | ⊔ | ‡a43 p. : ‡bill. ; ‡c27 cm. |
| 490 | ⊔ | 0 | ‡aNASA technical note ; ‡vD-3136 |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 43). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aAnalog computer simulation. |
| 650 | ⊔ | 0 | ‡aThrust chambers. |
| 650 | ⊔ | 0 | ‡aRocket engines ‡xCombustion. |
| 650 | ⊔ | 0 | ‡aLiquid propellant rockets ‡xCombustion. |
| 700 | 1 | ⊔ | ‡aBaumbick, Robert J. |
| 700 | 1 | ⊔ | ‡aWenzel, Leon M. |
| 710 | 2 | ⊔ | ‡aLewis Research Center. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a011446207 |
| DAT | 0 | ⊔ | ‡a20101110154503.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112165512.0 ‡b2024-01-26T18:53:08Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6404124 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106598326 ‡sUIU ‡16404124 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20240126 ‡sgoogle ‡uuiug.30112106598326 ‡y1965 ‡ric ‡qbib ‡tUS bib date1 >= 1930 |