充气式月球基地防护结构技术综述  

Review of Protection Structure Technology for Inflatable Lunar Habitats

作　　者：徐彦[1] 郑耀[1] 关富玲[2] 

机构地区：[1]浙江大学航空航天学院,浙江杭州310027 [2]浙江大学建筑工程学院,浙江杭州310058

出　　处：《载人航天》2014年第4期359-366,共8页Manned Spaceflight

基　　金：中央高校基本科研业务费(2012FZA4026);浙江省自然科学基金(LQ14A020003)

摘　　要：综述了充气式月球基地防护结构技术,包括总体设计要求和关键设计要点、柔性热防护结构的服役环境、功能需求、设计方法、材料选用等。并从结构冲击定位和强度分析、破坏响应分析、系统组成分析和自修复材料等方面,指出了对结构进行健康监测的必要性。介绍了现有的地面测试技术,包括热防护材料性能测试、展开动力学性能测试和太空环境模拟技术等,最后对防护结构技术的发展方向进行了展望。For the inflatable lunar habitats , studies on protective structure technologies were re-viewed in this paper .Structure design technology , including the system design requirement and key design points , was investigated for the inflatable lunar habitats .The service environment , functional requirements , design method , and material selection of flexible thermal protection structure were an-alyzed .To ensure the safety of the astronauts , it is necessary to adopt structural health monitoring technology for monitoring the major service behaviors of the inflatable habitats in real time .From the perspective of impact location and strength analysis , the structure damage response analysis , and system analysis and self-healing materials , an appropriate structural health monitoring system was quite necessary .The ground testing techniques were summarized , including thermal protection mate-rial performance test, the deployment test, space environment simulation technology , and etc.And finally the development directions of this technology were forecasted .

关 键 词：充气式月球基地 防护结构 结构健康监测技术 地面测试技术 

分 类 号：V476.3[航空宇航科学与技术—飞行器设计]