航天器单相热控系统的数学建模

2014 12th International Conference on Actual Problems of Electronics Instrument Engineering (APEIE) Pub Date : 2014-10-01 DOI:10.1109/APEIE.2014.7040754

A. Delcov, A. Hodenkov, D. A. Zhuikov

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引用次数: 0

摘要

本文讨论了初等型相热控制系统的传热建模问题。给出了表征电路的计算关系式。给出了计算结果。对航天器热控制系统数学建模存在的问题和前景进行了评价。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Mathematical modeling of single-phase thermal control system of the spacecraft

This article discusses the modeling of heat transfer in elementary contour-phase thermal control system. Calculated relations to characterize the circuit are given. Results of calculation are described. Problems and prospects of mathematical modeling of systems of spacecraft thermal control are evaluated.

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2014 12th International Conference on Actual Problems of Electronics Instrument Engineering (APEIE)

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