RADIO-CONTROLLED MISSILE Russian patent published in 2019 - IPC F42B15/00 

FIELD: rocket equipment.

SUBSTANCE: invention relates to rocket engineering and can be used in small-size rocket systems with radio command system and high-speed rockets. Radio-controlled rocket comprises body with wings and holes made on side surface and provided with plugs. There is detachable starting engine with head fairing and waveguides with external antennae. These antennas are brought out through holes in the housing by means of high-frequency connectors. Post is pivotally mounted between wings trailing edges and head fairing. It is made of two plates in contact with rear edge of wings. Head fairing comprises hollow ledges connected to the post. Wires and external antennae are arranged in said projections. In the housing under the rear wings edges there is a bushing-frame with holes coaxial to the holes in the housing. Holes in the housing can be made threaded. Said plugs can have thread with diameter larger than those made in the sleeve. High-frequency connectors are pressed to inner surface of plugs by elastically deformable element, and elastically deformable element is made in form of plate-like spring. At that, the post is pressed to the side surfaces of the wing before the rear edge with screws through the holes made in the plates. Gaskets from resilient material are installed between plates and side surfaces of wings.

EFFECT: increased level of permissible overloads and reliability of rocket operation at high flight speeds.

7 cl, 4 dwg