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Radiation exposure and Mission Strategies
for Interplanetary Manned Missions (REMSIM) 总被引:1,自引:0,他引:1
C. Cougnet N. B. Crosby S. Eckersley C. Foullon V. Guarnieri S. Guatelli D. Heynderickx A. Holmes-Siedle C. Lobascio S. Masiello P. Nieminen G. Parisi P. Parodi M. A. Perino M. G. Pia R. Rampini P. Spillantini V. Tamburini E. Tracino 《Earth, Moon, and Planets》2004,94(3-4):279-285
Cosmic radiation is an important problem for human interplanetary missions. The “Radiation Exposure and Mission Strategies for Interplanetary Manned Missions–REMSIM” study is summarised here. They are related to current strategies and countermeasures to ensure the protection of astronauts from radiation during interplanetary missions, with specific reference to: radiation environment and its variability; radiation effects on the crew; transfer trajectories and associated fluences; vehicle and surface habitat concepts; passive and active shielding concepts; space weather monitoring and warning systems. 相似文献
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为研究充气锚杆极限承载力计算方法,在模型试验基础上,探讨充气锚杆抗拔过程中的受力特征与破坏形式,分析锚杆荷载-位移曲线变化特征。基于圆孔扩张理论,通过简化力学模型,推导充气锚杆侧阻力与端阻力计算公式,将理论公式计算值与试验成果进行比较。研究结果表明:(1) 采用球孔扩张理论可以较好地描述膨胀体端部对土体产生的弹性、塑性变形力学机制,估算端阻力值。充气膨胀压力对土体的挤压膨胀作用大大增加了锚杆的侧阻力。(2) 极限承载力理论公式计算值与抗拔试验值基本吻合,验证了极限承载理论计算公式的正确性。(3) 通过与螺旋锚杆相比,充气锚杆的承载力约为单锚片螺旋锚杆的4.3倍,约为双锚片螺旋锚杆的1.9倍,充气锚杆的承载能力优势明显。 相似文献
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