Abstract
Some features of investigations of the temperature dependence of the integrated and spectral emissivity of erosion-resistant coatings on a low-thermal conductivity fibrous heat insulation are discussed. Results are provided for the standard ‘black’ and ‘white’ coatings. A study is made of the influence of repeated attacks of the high-temperature dissociated air on the integrated emissivity of the ‘black’ coating. Data are obtained on the radiation characteristics of this coating after full-scale tests during the Buran orbital spacecraft flight.
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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 73, No. 1, pp. 26–30, January–February, 2000.
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Dozhdikov, V.S., Petrov, V.A. Radiation characteristics of heat protective materials of the buran orbital spacecraft. J Eng Phys Thermophys 73, 25–28 (2000). https://doi.org/10.1007/BF02681672
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DOI: https://doi.org/10.1007/BF02681672