| LDR | 01376cam a2200301Ii 4500 | ||
| 001 | 011426196 | ||
| 003 | MiAaHDL | ||
| 005 | 20141013010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 790521s1979 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6364072 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)4985363 |
| 037 | ⊔ | ⊔ | ‡b22161 |
| 040 | ⊔ | ⊔ | ‡aGPO ‡cGPO ‡dOCL ‡dOCLCQ |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 074 | ⊔ | ⊔ | ‡a830-H-15 (microfiche) |
| 086 | 0 | ⊔ | ‡aNAS 1.60:1353 |
| 100 | 1 | ⊔ | ‡aBlair, A. B. |
| 245 | 1 | 3 | ‡aAn experimental wind-tunnel investigation of a ram-air-spoiler roll-control device on a forward-control missile at supersonic speeds / ‡cA.B. Blair, Jr., Langley Research Center. |
| 260 | ⊔ | ⊔ | ‡a[Washington] : ‡bNational Aeronautics and Space Administration, Scientific and Technical Information Office ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1978 i.e. 1979. |
| 300 | ⊔ | ⊔ | ‡a188 p. : ‡bill. ; ‡c27 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical paper ; ‡v1353 |
| 500 | ⊔ | ⊔ | ‡aDec. 1978. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aAerodynamics. |
| 650 | ⊔ | 0 | ‡aGuided missiles ‡xControl systems. |
| 710 | 2 | ⊔ | ‡aLangley Research Center. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Office. |
| CID | ⊔ | ⊔ | ‡a011426196 |
| DAT | 0 | ⊔ | ‡a20101007083419.0 ‡b20141013010000.0 |
| DAT | 1 | ⊔ | ‡a20141112173021.0 ‡b2025-01-02T19:02:05Z |
| DAT | 2 | ⊔ | ‡a2025-01-02T18:30:02Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6364072 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106663161 ‡sUIU ‡16364072 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20250102 ‡sgoogle ‡uuiug.30112106663161 ‡y1979 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2019 |