000			00436pam a2200145a 44500
082			_aNASA _bTR R-220
100			_aHowell,John R,Strite,Mary K
245	1		_aANALYSIS OF HEAT-TRANSFER EFFECTS IN ROCKET NOZZLES OPERATING WITH VERY HIGH-TEMPERATURE HYDROGEN.
260			_a _bNasa, Washington, D.C. _c
300			_a32
500			_aBound With Nasa Tr R-211-219
700			_aRenkel,Harold E
964			_gCIRC
997			_aTR11759 C
999			_c397569 _d397569