NUMERICAL AND EXPERIMENTAL ESTIMATION OF HEAT CONDUCTIVITY FOR SPACE ANTENNA REFLECTOR MATERIAL

被引：1
|
作者：
Denisov, Oleg V. [1 ]
Kirbai, Anton A. [1 ]
Minakov, Dmitrii S. [1 ]
机构：
[1] Bauman Moscow State Tech Univ, Moscow 105005, Russia
来源：
HEAT AND MASS TRANSFER IN THE THERMAL CONTROL SYSTEM OF TECHNICAL AND TECHNOLOGICAL ENERGY EQUIPMENT | 2015年 / 23卷
关键词：
D O I：
10.1051/matecconf/20152301016
中图分类号：
O414.1 [热力学];
学科分类号：
摘要：
This article devoted for experimental method of contact heating thin carbon plates. Thermal tests provided non-stationary temperature field with gradient, which is co-directional plane reinforcement in sample. New plane reinforcement thermal conductivity data were obtained within temperature gap between 295 and 375 K. Modern thermal conductivity data could be applied for development projects of space precision antenna reflectors.
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页数：5
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