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