FIELD: armament.
SUBSTANCE: the rocket has a body, propulsion system, guidance system and a control system with fixed wings and flat aerodynamic control surfaces. The flat aerodynamic control surfaces are made differential. Precontrol surface stabilizers are fastened on the rocket body, their planes coincide with the respective planes of the flat differential aerodynamic control surfaces. The quantity of the precontrol surface stabilizers equals the quantity of the flat differential aerodynamic control surfaces. The precontrol surface stabilizers and the flat differential aerodynamic control surfaces are made with a definite relation of the dimensions.
EFFECT: enhanced maneuverability of the rocket at subsonic and transonic speeds.
5 cl, 5 dwg
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Authors
Dates
2006-09-10—Published
2005-03-17—Filed