000			00522pam a2200133a 44500
082			_aNASA _bTM X-288
100			_aSpencer,Bernard
245	1		_aAN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4(DEGRE) TO 100(DEGRE) OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELS
260			_a _bNasa,Washington, D.C. _c1960
300			_a28
500			_aBound With Nasa Tm X-281-283,289-299,Lack No. 282,84-87,90,93,95,96,98
964			_gCIRC
997			_aTR13674 C
999			_c397315 _d397315