FIELD: rockets.
SUBSTANCE: invention relates to the technology of jet propulsion and can be used to create high-speed ground and air ammunition. The rocket missile consists of solid fuel stages, freely inserted one into another and sequentially separating, equipped with a mechanism for automatic transfer of combustion from one stage to another. The separating stages therein have aerodynamic elements on the surface thereof, arranged helically and used for spinning the missile after launch, and aerodynamic rudders are located on the last inseparable stage, through used to suppress the rotation in the final section of the flight and to aim accurately at the target by means of roll, course and pitch control.
EFFECT: invention provides a structural simplification and application of the jet principle of achieving hypersonic speeds for small-sized ammunition.
3 cl, 1 dwg
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