Flight Investigation to Evaluate the Roll-Rate Stabilization System of the Naval Ordnance Test Station SIDEWINDER Missile at Mach Numbers From 0.9 to 2.3

Author:	Brown, Clarence A., Jr.
Year:	1954
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-SL54D26
Link:	https://digital.library.unt.edu/ark:/67531/metadc53266/