000			00428pam a2200133a 44500
082			_aNASA _bCR-649 -
100			_aMurphy,J D
245	1		_aFLIGHT TEST AERODYNAMIC HEATING DATA FOR THE AFTERBODY OF THE PROJECT MERCURY SPACECRAFT WITH COMPARISONS TO AVAILABLE PREDICTION METHODS
260			_a _bNasa, Washington, D.C. _c1966
300			_a127
500			_aBound With Nasa Cr-646-50
964			_gCIRC
997			_aTR10226 C
999			_c394418 _d394418