000 | 00657 a2200241 4500 | ||
---|---|---|---|
001 | 335605 | ||
020 | _a | ||
041 | _aeng | ||
080 | _aLNASA CR 2531 : 1975 | ||
245 | _aAnalytical and experimental evaluation of flowing air test conditions for selected metallics in a shuttle tps application | ||
250 | _a | ||
260 | _aWashington, D.C. | ||
260 | _bNational Aeronautics and Space Administration (NASA) | ||
260 | _c1975 | ||
300 | _a194 p. | ||
300 | _c | ||
856 | _u | ||
490 | _aNASA CR 2531 : 1975 | ||
700 | _a | ||
650 | _a | ||
650 | _aHeat shielding, TDNi-20Cr, Coated niobium, Space shuttle orbiter, Plasma jets | ||
942 | _cPP | ||
942 | _2UDC | ||
999 |
_c200613 _d200613 |