000			00533pam a2200145a 44500
082			_aNASA _bMEMO 4-23-59L
100			_aLundstrom,Reginald R
245	1		_aANALYTICAL INVESTIGATION OF A FLIKER-TYPE ROLL CONTROL FOR A MACH NUMBER 6 MISSILE WITH AERODYNAMIC CONTROLS OVER AN ALTITUDE RANGE OF 82,000 TO 282,000 FEET
260			_a _bNasa, Washington, D.C. _c1959
300			_a50
500			_aBound With Nasa Memo 4-20-59l -4-22-59l And 4-30-59l Lack No.24-29
700			_aWhitman,Ruth I
964			_gCIRC
997			_aTR7402 C
999			_c395618 _d395618