FIELD: anti-aircraft ammunition. SUBSTANCE: radio- controlled anti-aircraft missile has a booster engine, sustainer stage with functional units, transmitter with an antenna and a radio sensor with an antenna device. The booster engine is made with a separation mechanism, and the transmitter antenna in the form of a dielectric rod is positioned in the end face of the sustainer stage aft part and connected to the transmitter in the form of a waveguide tee, whose two other arms of the same length are connected to the dielectric rod antennas via polarizer, the antennas are positioned diametrically relative to the missile longitudinal axis. The antennas are installed on the separation mechanism over the front part of the engine and faired. EFFECT: enhanced reliability of missile control in the launching and sustainer legs of the flight. 4 dwg
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Authors
Dates
2002-06-27—Published
2001-02-21—Filed