Wind-tunnel investigation at Mach numbers of 1.5 and 2.0 of a canard missile configuration

Richard J. Spahr, Robert A. Robinson
naca-rm-a51c08
May 1951


Wind-tunnel tests were performed at Mach numbers of 1.5 and 2.0 to investigate the force, moment, and control characteristics of a canard missile configuration (Grumman XSSM-N-6) and its components in both pitch and sideslip.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1951/naca-rm-a51c08.pdf