000			00461pam a2200145a 44500
082			_aNASA _bTN D-5597
100			_aNiedzwiecki,Richard W
245	1		_aPERFORMANCE OF A 48-MODULE SWIRL-CAN TURBOJET COMBUSTOR SEGMENT AT HIGH TEMPERATURES USING ASTM-A1 FUEL.
260			_a _bNasa, Washington, D.C. _c1969
300			_a38
500			_aBound With Nasa Tn D-5590-96, 5598-99 Lack No.5594
700			_aMoyer,Harry M
964			_gCIRC
997			_aTR12671 C
999			_c397091 _d397091