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
- 1 Post-graduate Student, Research engineer, Open Society «Russian space systems» FSO «Roskosmos»
- 2 Ph. D. (Eng.), Senior Research Scientist, Chief of sector, Open Society «Russian space systems» FSO «Roskosmos»
Abstract
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.
How to cite
Климов Д.И., Благодырёв В.А. Представление температурных диапазонов нагретых элементов конструкций космического аппарата в видимом диапазоне длин волн с учетом интегрального коэффициента теплового излучения // Электромагнитные волны и электронные системы. 2014. № 3. С. 62–65.
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