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Spacecraft two-phase thermal control system simulation

机译:航天器两相热控制系统仿真

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摘要

The results of computer simulation of a typical spacecraft pumped two-phase thermal control system are presented. The two-phase thermal control system transients under effect of typical disturbances are obtained. The system dynamic characteristics are analyzed and influence of design parameters on the quality of system dynamic processes are discussed.
机译:介绍了典型的航天器泵浦两相热控制系统的计算机模拟结果。获得典型干扰效果的两相热控制系统瞬变。讨论了系统动态特性,讨论了设计参数对系统动态过程质量的影响。

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