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INCLUSION OF GRADIENT STRUCTURES IN TRADITIONAL THERMAL PROTECTIVE COATINGS TO REDUCE TEMPERATURE ON THE HULL OF DESCENT SPACECRAFTS

Annotation

The problem of creation of thermal protection of space vehicles (spacecrafts) entering the atmosphere of planets is considered. The problem is regarded as an urgent one because the thermal protection is designed to provide thermal regimes and reliability of spacecraft instruments and systems. Results of a study on the possible improvement of the thermal protection of space vehicles by developing a technology for creating thermal protective coatings of a gradient structure of various compositions for integration into a thermal protection package to reduce the temperature on the spacecraft body are presented.

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