HYPERSONIC GUIDED MISSILE Russian patent published in 2007 - IPC F42B15/00 

FIELD: armament.

SUBSTANCE: the hypersonic guided missile consists of a separating zero stage, sustainer stage containing the nose cone with the body that accommodates an air-dynamic control actuator with aerodynamic controls, heat-exchanging device, nose fairing with a nose air intake and an inner lengthwise channel made in it. The fairing is made of two parts: the nose part serving as an air intake and the main part. The fairing nose part is rigidly fastened with provision of sealing in the fairing main part, and provided inside with a multistep, through longitudinal hole for installation of the fairing nose part, heat-exchanging device and attachment to the zero stage body. The heat-exchanging device consists of a gas flow dissector with an input channel, grates, bank of straight thin-walled tubes, tightening nut.

EFFECT: provided operation of a missile with an air-dynamic control actuator in the conditions of kinetic heating of the components of the control actuator construction.

5 dwg