ARSTRACT An extensive data base (through research and system design) descrihing the unique aerodynamic self induced rolling moment coefficient of wrap around fins (WAF) on rockets has heen accumulated over the past decade hy the US Army Missile Command (MICOM). Most recent investigations have centered on tailoring the roll rate of rockets having wrap around fins by simple leading and trailing edge modifications. These results indicate the ability both t o predict r o l l performance of rockets with W A F ' S and to tailor roll rate for specific applications.
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