Conceptual Design of Flexible Thermal Protect Structure for Deployable Lunar Habitats

XU Yan1, ZHENG Yao1, KUANG Songsong1, ZHOU Sheng2

PDF(10027 KB)
PDF(10027 KB)
Journal of Deep Space Exploration ›› 2016, Vol. 3 ›› Issue (2) : 168-174. DOI: 10.15982/j.issn.2095-7777.2016.02.012
Article

Conceptual Design of Flexible Thermal Protect Structure for Deployable Lunar Habitats

  • XU Yan1, ZHENG Yao1, KUANG Songsong1, ZHOU Sheng2
Author information +
History +

Abstract

Constructing lunar habitats is the first and the most important step to explore, exploit and colonize the outer space. A novel deployable lunar habitat concept is designed in the paper. The habitat structures consists of the spatial deployable truss and the flexible thermal protection laminated membrane. The structural design schemes were analyzed and compared. Nine topological schemes of the spatial deployable truss and seven designing schemes of the laminated membrane are presented. The optimal scheme was determined after strength analysis, stiffness analysis and steady thermal analysis were performed. Structural performances of the optimal design scheme for deployable lunar habitats were analyzed including static analysis, modal analysis and steady thermal analysis of three load cases. The analysis results indicates that structural performances and thermal protect performances of deployable lunar habitats are perfect. Then the technology support for scheme selection, structural design and TPS design was provided.

Keywords

deployable lunar habitats / deployable truss structures / FTPS / structural performance analysis

Cite this article

Download citation ▾
XU Yan, ZHENG Yao, KUANG Songsong, ZHOU Sheng. Conceptual Design of Flexible Thermal Protect Structure for Deployable Lunar Habitats. Journal of Deep Space Exploration, 2016, 3(2): 168‒174 https://doi.org/10.15982/j.issn.2095-7777.2016.02.012

References

[1] 叶培建,肖福根.月球探测工程中的月球环境问题[J]. 航天器环境工程,2006,23(1):1-11.Ye P J,Xiao F G. Issues about lunar environment in lunar exploration project[J]. Spacecraft Environment Engineering,2006,23(1):1-11.
[2] 关富玲,徐彦,郑耀.充气可展开结构技术在空间探索领域中的应用[J]. 载人航天,2009(4):40-48.Guan F L,Xu Y,Zheng Y. Applications of inflatable structure technology for space exploration[J]. Manned Spaceflight,2009(4):40-48.
[3] Walter E B,Nathaniel J M,Paul G F,et al. Aerothermal ground testing of flexible thermal protection systems for hypersonic inflatable aerodynamic decelerators[C]//The 9th International Planetary Probe Workshop,16-22 June 2012. Toulouse,France:[s. n.],2012.
[4] Smith B P,Glark I G,Braun R D. Thermal,structural,and inflation modeling of anisotensoid supersonic inflatable aerodynamic decelerator[C]//IEEE AC paper #1312,Version 4.[S. l.]:IEEE,2011:1-16.
[5] Hinkle J,Lin J K H,Watson J. Deployment testing of an expandable lunar habitat[C]//AIAA SPACE 2009 Conference & Exposition. California:AIAA,2009:1-9.
[6] 于登云,葛之江,王乃东,等.月球基地结构形式设想[J]. 宇航学报,2012,33(12):1840-1844.Yu D Y,Ge Z J,Wang N D,et al. Supposal for structure form of lunar base[J]. Journal of Astronautics,2012,33(12):1840-1844.
[7] 徐彦,郑耀,关富玲.充气式月球基地防护结构技术综述[J]. 载人航天,2014,20(4):359-366.Xu Y,Zheng Y,Guan F L. Review of protection structure technology for inflatable lunar habitats[J]. Manned Spaceflight,2014,20(4):359-366.
[8] 张鹏飞,梁龙,陶积柏,等. 深空环境下热防护材料的研究及应用进展[J]. 深空探测学报,2016,3(1):77-82.Zhang P F,Liang L,Tao J B,et al. Research and development of thermal protection materials applied in deep space exploration[J]. Journal of Deep Space Exploration,2016,3(1):77-82.
[9] Del Corso J A,Bruce W E,Liles K A,et al. Thermal analysis and testing of candidate materials for PAIDAE inflatable aeroshell[R]. USA:AIAA,2009.
PDF(10027 KB)

Accesses

Citations

Detail

Sections
Recommended

/