Abstract
Abstract
The study of interference emissions, the model of the spacecraft module in the case when the radio-absorbing material TPMV-1C is placed in the internal space of the module model is carried out. The interference emissions are created by an on-board instrument simulator located in the internal space of the spacecraft module model. A noticeable decrease in the interference emission of the spacecraft module model is demonstrated with the use of radar absorbing material. The expediency of using the TPMV-1C radar absorbing material to reduce the interference emissions of on-board instruments and devices of electrical systems of spacecraft is shown.
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5 articles.
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