000			00592pam a2200145a 44500
082			_aNASA _bTM X-519
100			_aRobinson,Ross B
245	1		_aEFFECT OF VERTICLE-TAIL MODIFICATIONS ON THE STATIC STABILITY CHARACTERISTICS AT A MACH NUMBER OF 2.2 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS
260			_a _bNasa, Washington, D.C. _c1961
300			_a17
500			_aBound With Nasa Tm X-507-18,522-81, Lack No.509-13,515-17,519-21,523-29,531-39,541-46,548-65,567-68,572-80
700			_aSpearman,M Leroy
964			_gCIRC
997			_aTR14307 C
999			_c398695 _d398695