GUIDED MISSILE Russian patent published in 2001 - IPC

FIELD: rocketry, applicable in small-sized missile rounds, as well as in artillery. SUBSTANCE: the guided missile has a body with the warhead and control equipment units successively arranged in it, the warhead front end is attached to the body, and the control equipment units are installed in a casing attached to the rear end of the warhead, clearances are formed between the control equipment units, casing and the inner surface of the body. Shock- absorbers in the form of leaf springs are made between the casing and the inner surface of the body. EFFECT: enhanced permissible flight speed of the missile in the atmosphere due to the reduced heat transfer from the heated body to the equipment units and reduced force action on the units in flight. 2 dwg