FIELD: weapons and ammunition.
SUBSTANCE: invention relates to rocketry and can be used in various antiaircraft complexes with radio control system. Proposed missile comprises detachable launching stage, sustainer stage with functional units, control hardware, radio signal receiver, antenna and power supply including separation conductor. Sustainer stage tail part incorporates onboard telemetry transmitting module. The latter consists of signal controller ADC and radio transmitter with phase-pulse modulation of carrier frequency connected, via switching device, with strip antenna of sustainer stage and, via matching device, with launching stage antenna. Note here that control input of aforesaid switching device is connected with separation conductor.
EFFECT: multi-channel data transfer, data registration at surface fire control station.
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