GUIDED ANTI-AIRCRAFT MISSILE Russian patent published in 2003 - IPC

FIELD: rocketry, applicable in tests of guided anti-aircraft missiles in the stage of their development. SUBSTANCE: a telemetry unit with a radio transmitter and a matching device is installed in the missile sustainer stage in the place of arrangement of the warhead. The body of the sustainer stage in the place of arrangement of the telemetry unit is divided by ring insulator into the head and tail sections, with the relation of the lengths of the head and tail sections of the sustainer stage being as 1/3. The output of the radio transmitter of the telemetry unit is connected by the radio transmitter of the telemetry unit is connected by the central conductor of the coaxial cable to the body of the head section of the sustainer stage that is connected to the tail section of the sustainer stage by the central conductor of the second coaxial cable, whose length equals half the length of the wave of the radiated signal. The outer shells of the sheathes of the coaxial cables are shorted out. The second coaxial cable is positioned in the telemetry unit and laid helically in the aria of the ring insulator. EFFECT: provided development of a new design. 3 dwg