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| 003 | MiAaHDL | ||
| 005 | 20141009010000.0 | ||
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| 008 | 020828s1969 dcua b f000 0 eng d | ||
| 035 | ⊔ | ⊔ | ‡asdr-uiuc6401519 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)646012167 |
| 040 | ⊔ | ⊔ | ‡aABC ‡cSTF |
| 049 | ⊔ | ⊔ | ‡aUIUU |
| 050 | 1 | 4 | ‡aTL521 ‡b.A3525 no. 5010 |
| 086 | 0 | ⊔ | ‡aNAS 1.14:D-5010 |
| 088 | ⊔ | ⊔ | ‡aNASA-TN-D-5010 |
| 100 | 1 | ⊔ | ‡aRoyster, Dick M. |
| 245 | 1 | 0 | ‡aTensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ̊to 400 ̊F (370 ̊to 480 ̊K) ‡cby Dick M. Royster. |
| 260 | ⊔ | ⊔ | ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡aSpringfield, Va. : ‡bFor sale by the Clearinghouse for Federal Scientific and Technical Information, ‡c[1969] |
| 300 | ⊔ | ⊔ | ‡a42 p. : ‡bill. ; ‡c27 cm. |
| 490 | 0 | ⊔ | ‡aNASA technical note, ‡x0499-9339 ; ‡vNASA TN D-5010 |
| 500 | ⊔ | ⊔ | ‡aPrepared at Langley Research Center. |
| 500 | ⊔ | ⊔ | ‡a"January 1969"--Cover. |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (p. 12). |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 0 | ‡aSupersonic transport planes ‡xMaterials ‡xEnvironmental testing. |
| 650 | ⊔ | 0 | ‡aAluminum alloys ‡xCreep. |
| 650 | ⊔ | 0 | ‡aAluminum alloys ‡xDuctility. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bNational Aeronautics and Space Administration. |
| 710 | 2 | ⊔ | ‡aLangley Research Center. |
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