Rocket-powered flight test of a roll-stabilized supersonic missile configuration

Robert A. Gardiner, Jacob Zarovsky
naca-rm-l9k01a
Jan 1950


The results of a flight at supersonic speed of an automatically roll-stabilized rocket-powered model incorporating a gyro-actuated control system in combination with wing-tip ailerons are reported.

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http://naca.central.cranfield.ac.uk/reports/1950/naca-rm-l9k01a.pdf