000			00430pam a2200133a 44500
082			_aNASA _bTN D-6614 -
100			_aPappas,C C
245	1		_aCALCULATION OF LAMINAR HEAT TRANSFER TO THE WINDWARD SURFACES OF STRAIGHT WING SHUTTLE VEHICLES AT HIGH ANGLE OF ATTACK AND WITH YAW
260			_a _bNasa, Washington, D.C. _c1972
300			_aiv,15
500			_aBound With Nasa Tn D-6610-19
964			_gCIRC
997			_aTR9709 C
999			_c395187 _d395187