Abstract
The problem of the influence of the rocket engine plume (REP) plasma on the radiation pattern (RP) of the onboard third stage antennas launch vehicle. The possibility of using the method of the impedance analog of the Sestroretskii electromagnetic space for solving this problem is shown. The distribution pattern of the plasma frequency in the REP is presented. The distribution patterns of the amplitude and phase of the magnetic field in the region under study are obtained. The RPs of the antenna system are presented, showing a significant shift in the direction of the main lobe and a change in its shape.
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