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载人航天器系统重量控制方法研究 被引量:5
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作者 李兴乾 白明生 +1 位作者 苟仲秋 张伟 《航天器环境工程》 2012年第2期201-204,共4页
系统的重量设计和控制贯穿于载人航天器研制的全过程,在型号研制中占有非常重要的地位。文章结合载人航天器型号研制实践,描述了载人航天器系统重量构成、重量控制流程、不同研制阶段的重量控制要点、系统重量控制体会以及轻量化设计措... 系统的重量设计和控制贯穿于载人航天器研制的全过程,在型号研制中占有非常重要的地位。文章结合载人航天器型号研制实践,描述了载人航天器系统重量构成、重量控制流程、不同研制阶段的重量控制要点、系统重量控制体会以及轻量化设计措施,为未来载人航天器型号设计和减重研究提供借鉴与参考。 展开更多
关键词 载人航天器 系统重量设计 重量控制
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Weight control in design of space nuclear reactor system 被引量:1
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作者 WANG SanBing HE ChaoHui 《Science China(Technological Sciences)》 SCIE EI CAS 2013年第10期2594-2598,共5页
Space nuclear power system is the key technology for deep space exploration missions in the future, especially for space base building-up. This paper evaluates several typical latest space nuclear reactor system (SNR... Space nuclear power system is the key technology for deep space exploration missions in the future, especially for space base building-up. This paper evaluates several typical latest space nuclear reactor system (SNRS) designs, and finds that most of their weights are heavier than necessary. From the point of weight-control, the SA4 design is the best but its design is more complex than others. A newly designed SNRS, based on the SAFE400 model, uses annular fuel and has better performance, with a fuel mass lower than that of the SAFE400 prototype by 18.75%. Meanwhile, different from former opinions, the delay neutron fractions of SNRS are not constant and change with the different SNRS designs. Therefore, designs of SNRS not to count the delayed neutron fracture or directly to consider it as 0.00677 are not appropriate. 展开更多
关键词 RTG SNRs power density SAFE400 MCNPX
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