Tests of a 1/15-scale model of the TALOS 6cl missile were performed in the TMB 7- by 10-Foot Transonic Wind Tunnel for a Mach number range of 0.7 to 1.17, at angles of attack of -4 to 10, and roll angles of 0 and -45. The investigation included evaluation of the effects of ram-air bleed at the base of the second stage and the longitudinal stability and control effectiveness of ...
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