STUDY OF THERMAL REGIME OF RADIATION TRANSMITTER OF SPACE VEHICLE UNDER EXPOSURE TO STAR SHOWER
M. V. Frunze Arsenal Design Bureau, St. Petersburg; General Director
V. D. Atamasov
Mozhaisky Military Space Academy, Department of Space Vehicles Design, St. Petersburg; Professor
A. V. Belyankin
Mozhaisky Military Space Academy, Department of Space Vehicles Design, St. Petersburg;
D. Y. Mikhailov
Mozhaisky Military Space Academy, Department of Space Vehicles Design, St. Petersburg; Advanced Student
M. M. Poluyan
Mozhaisky Military Space Academy, Department of Space Vehicles Design, St. Petersburg; Advanced Student
A. V. Levandovich
Mozhaisky Military Space Academy, Department of Space Vehicles Design, St. Petersburg; Advanced Student
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Abstract. An experimental instrument is developed for study of the effects of star showers on thermal regime of transmitting devices of space vehicles. The method of experiments is considered.
Keywords:
thermal radiation element, thermal regime, intensity of thermal emission.
