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研究了拟在美国航天飞机搭载的G-435、G-434搭载桶实验内容选定、硬件总体布置、热设计、电源设计、运行方案设计及可靠性问题。提出了具有高度集成性的总体设计方案和搭载试验运行方案。模拟运行试验表明该方案可行可靠。
The experiment contents of G-435 and G-434 carrying barrels to be mounted on the U.S. space shuttle were studied. The hardware layout, thermal design, power supply design, operation scheme design and reliability were studied. Proposed a highly integrated design of the overall program and equipped with trial operation program. Simulation test shows that the scheme is feasible and reliable.