000			00496pam a2200133a 44500
082			_aNASA _bTN D-205
100			_aSchult,Eugene D
245	1		_aFREE-FLIGHT INVESTIGATION AT MACH NUMBERS BETWEEN 0.5 AND 1.7 OF THE ZERO-LIFT ROLLING EFFECTIVENESS AND DRAG OF VARIOUS SURFACE, SPOILER, AND JET CONTROLS ON AN 80(DEGRE) DELTA-WING MISSILE
260			_a _bNasa, Washington, D.C. _c1960
300			_a47
500			_aBound With Nasa Tn D-201-204,206-210
964			_gCIRC
997			_aTR14834 C
999			_c399620 _d399620