This paper analyzed the heat transfer and the distribution of pressure in the high-altitude simulated test module, and proposed the methods of calculation.

分析了高空模拟试验舱的传热与舱压分布，并提出了计算方法，为高模试验舱的结构设计提供了参考。

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When it's depressurized at altitude, it becomes a near-vacuum, causing the aforementioned heat-transfer problem.

ENGADGET: Art Thompson, Red Bull Stratos' technical project director, talks circuit breakers, wind shear and biomedical data