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Representation of temperature ranges of the heated elements of space vehicle in a visiblerange of lengths of waves with the account integrated factor of thermal radiation

Keywords:

D.I. Klimov – Post-graduate Student, Research engineer, Open Society «Russian space systems» FSO «Roskosmos». E-mail: mitguitar@yandex.ru
V.A. Blagodyryov – Ph. D. (Eng.), Senior Research Scientist, Chief of sector, Open Society «Russian space systems» FSO «Roskosmos». E-mail: tm016@rniikp.ru


Representation of temperature ranges of the heated up elements of designs space vehicles in a seen range of lengths of waves is offered. Subranges of lengths of waves in infra-red and ultra-violet ranges are considered and corresponding by it subranges values of temperatures are found. The algorithm of recalculation of lengths of waves from infra-red and ultra-violet ranges in a visible range of lengths of waves with the account of integrated factor of thermal radiation is resulted.
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June 24, 2020
May 29, 2020

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