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載人航天器系統(tǒng)重量控制方法研究

The system weight control for manned spacecraft

  • 摘要: 系統(tǒng)的重量設(shè)計(jì)和控制貫穿于載人航天器研制的全過(guò)程，在型號(hào)研制中占有非常重要的地位。文章結(jié)合載人航天器型號(hào)研制實(shí)踐，描述了載人航天器系統(tǒng)重量構(gòu)成、重量控制流程、不同研制階段的重量控制要點(diǎn)、系統(tǒng)重量控制體會(huì)以及輕量化設(shè)計(jì)措施，為未來(lái)載人航天器型號(hào)設(shè)計(jì)和減重研究提供借鑒與參考。

     

    Abstract: The design and the control of the system weight are important in the development of manned spacecrafts. Based on the practices, this paper discusses the composition of the system weight of manned spacecrafts, and the rellated control processes, focusing on the key points at different development stages, the first-hand experience, and the lightweight design.

     

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