000			00423pam a2200145a 44500
082			_aNASA _bTN D-6167
100			_aNiedzwiecki,Richard W
245	1		_aPERFORMANCE OF A SHORT MODULAR TURBOJET COMBUSTOR SEGMENT USING ASTM-A1 FUEL
260			_a _bNasa, Washington, D.C. _c1971
300			_a32
500			_aBound With Nasa Tn D-6160-6166,6168-6169
700			_aMoyer,Harry M
964			_gCIRC
997			_aTR13034 C
999			_c398688 _d398688