000 00598 a2200265 4500
001 169464
020 _a
041 _aeng
080 _aLNASA TN D-2878
245 _aFeasibility study of high-temperature synthetic-air heater for use with a mach 8 to 9 hypersonic tunnel. :
250 _a
260 _aWashington, D.C.
260 _bNASA
260 _c1965
300 _a19
300 _c
856 _uNASA
490 _aNBS : SMT : SP : 400 - 27 - 1974
100 _aLezberg, Erwin A.
700 _aZlatarich, Steven A.
700 _a
650 _a
650 _a
942 _cPP
942 _2UDC
999 _c190757
_d190757