FIELD: armament.
SUBSTANCE: the radio-controlled missile has a body, engine, control equipment, whose input via feeder channels is connected to the antennas. The control equipment is positioned in the axisymmetric space formed inside the engine near its front end face. The feeder channels are provided with high-frequency connectors, having a threaded joint between them. The connector bodies are made in the form of a bottom cylinder with a central axial hole. A tapered-section nut is installed on the cylinder outer surface by means of a threaded connection, it is positioned in a radial tapered hole made on the side surface of the missile body near the front end face of the engine concentrically to the connectors, whose parts located on the side of the control equipment, are fastened inside the body.
EFFECT: reduced length of the missile.
2 dwg
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Authors
Dates
2005-08-20—Published
2004-03-11—Filed