000			00428pam a2200145a 44500
082			_aNASA _bTN D-3602
100			_aMiller,Max J
245	1		_aBLADE ELEMENT PERFORMANCE OF AXIAL-FLOW PUMP ROTOR WITH BLADE TIP DIFFUSION FACTOR OF 0.66
260			_a _bNasa, Washington, D.C. _c1966
300			_a33
500			_aBound With Nasa Tn D-3601, 3603-10
700			_aSandercock,Donald M
964			_gCIRC
997			_aTR11956 C
999			_c397735 _d397735