| LDR | 01197cam a2200289Ii 4500 | ||
| 001 | 011444119 | ||
| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 780808s1977 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6392382 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)4119160 |
| 040 | ⊔ | ⊔ | ‡aGPO ‡cGPO ‡dOCL ‡dABC ‡dOCLCQ |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 050 | ⊔ | 4 | ‡aTL521 ‡b.A3525 no. 8454 |
| 086 | 0 | ⊔ | ‡aNAS 1.14:D-8454 |
| 245 | 0 | 0 | ‡aExperimental investigation of a swept-strut fuel-injector concept for scramjet application / ‡cGriffin Y Anderson ... [et al.] ; Langley Research Center. |
| 260 | ⊔ | ⊔ | ‡aWashington : ‡bNational Aeronautics and Space Administration ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service,?, ‡c1977. |
| 300 | ⊔ | ⊔ | ‡a63 p. : ‡bill. ; ‡c27 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical note ; ‡vNASA TN D-8454 |
| 500 | ⊔ | ⊔ | ‡aIssued Aug. 1977. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aAerodynamics, Hypersonic. |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xScramjet engines. |
| 650 | ⊔ | 0 | ‡aFuel pumps. |
| 710 | 2 | ⊔ | ‡aLangley Research Center. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a011444119 |
| DAT | 0 | ⊔ | ‡a20101103081358.0 ‡b20141009010000.0 |
| DAT | 1 | ⊔ | ‡a20141112165512.0 ‡b2023-03-14T18:37:02Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6392382 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106911644 ‡sUIU ‡16392382 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106911644 ‡y1977 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2018 |