| LDR | 01258cam a2200313Ii 4500 | ||
| 001 | 011426195 | ||
| 003 | MiAaHDL | ||
| 005 | 20141013010000.0 | ||
| 006 | m d | ||
| 007 | cr bn ---auaua | ||
| 008 | 780629s1977 dcua b f000 0 eng d | ||
| 029 | 1 | ⊔ | ‡aGBVCP ‡b609322982 |
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6364070 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)4015797 |
| 037 | ⊔ | ⊔ | ‡b22161 |
| 040 | ⊔ | ⊔ | ‡aGPO ‡cGPO ‡dABC ‡dOCL ‡dOCLCQ ‡dOCLCG |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 050 | ⊔ | 4 | ‡aTL521.3.T4 ‡bA3 no. 3554 |
| 074 | ⊔ | ⊔ | ‡a830-D (microfiche) |
| 086 | 0 | ⊔ | ‡aNAS 1.15:X-3554 |
| 100 | 1 | ⊔ | ‡aMartin, J. A. ‡q(James A.) |
| 245 | 1 | 3 | ‡aAn evaluation of composite propulsion for single-stage-to-orbit vehicles designed for horizontal take-off / ‡cJames A. Martin. |
| 260 | ⊔ | ⊔ | ‡aWashington : ‡bNational Aeronautics and Space Administration ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1977. |
| 300 | ⊔ | ⊔ | ‡a28 p. : ‡bill. ; ‡c27 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical memorandum ; ‡vNASA TM X-3554 |
| 500 | ⊔ | ⊔ | ‡aIssued Nov. 1977. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aLaunch vehicles (Astronautics) |
| 650 | ⊔ | 0 | ‡aSpace vehicles ‡xPropulsion systems. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| CID | ⊔ | ⊔ | ‡a011426195 |
| DAT | 0 | ⊔ | ‡a20101007083324.0 ‡b20141013010000.0 |
| DAT | 1 | ⊔ | ‡a20141112173021.0 ‡b2023-03-14T18:16:18Z |
| CAT | ⊔ | ⊔ | ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020 |
| FMT | ⊔ | ⊔ | ‡aBK |
| HOL | ⊔ | ⊔ | ‡0sdr-uiuc6364070 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106566059 ‡sUIU ‡16364070 |
| 974 | ⊔ | ⊔ | ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106566059 ‡y1977 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2018 |