000 00477 a2200241 4500
001 293646
020 _a
041 _aeng
080 _aLNASA TN D-4491 : 1968
245 _aConsiderations of turbine cooling systems for mach 3 flight
250 _a
260 _aWashington, D.C.
260 _bNASA
260 _c1968
300 _a41 p.
300 _c
856 _uNASA
490 _aNASA TN D-4491 : 1968
700 _a
650 _a
650 _a
942 _cPP
942 _2UDC
999 _c251177
_d251177