Review of Deployabletruss Masts for Space Application

doi:10.3780/j.issn.1000-758X.2011.02.005

Abstract

Abstract: Deployabletruss masts for space application are wildly used in the scope of achieving large size, high stiffness spacecraft. The configuration, mechanism and development of several typical space deployable-truss masts were discussed. The characteristics were compared among these diffenent deployable-truss masts. The trends of the deployable-truss masts were presented. The result show that the ADAM type articulated truss, adaptive to the development of large spacecraft, is the main trend of space development-truss masts. The key technologies of the ADAM type articulated truss for engineering application were analysed.

Key words: Mast, Deployable-truss, Coilable lattice truss, Articulated truss, Spacecraft

LIU Zhi-Quan, LI Biao, CHENG Gang. Review of Deployabletruss Masts for Space Application[J]. Chinese Space Science and Technology, 2011, 31(2): 32-38.

Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks

URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2011.02.005

https://journal26.magtechjournal.com/kjkxjs/EN/Y2011/V31/I2/32

References

[1] WOLFF GEORGE. Oriented flexible rolled-up solar array[C]. Los Angeles: AIAA 3rd Communications Satellite Systems Conference, 1970.

[2] ANON. Tubular spacecraft booms[R]. NASA-SP-8065, 1971.

[3] LAPP P A, SAMPELS R L. An extendible boom system for space vehicles[R]. NASA-CR-55578,1964.

[4] BECCHI P, DELLAMICO S. Design and testing of a deployable, retrievable boom for space application[R]. NASA-89-23898, 1989. 

[5] THOMSON M W. Deployable and retractable telescoping tubular structure development[C]. California: AIAA/AHS/ASEE Aerospace Design Conference, 1993.

[6] CADOGAN D, GRAHNE M, MIKULAS M. Inflatable space structures: a new paradigm for space structure design[C]. Melbourne: 49thInternational Astronautical Congress, 1998.

[7] DERBES BILLY. Case studies in inflatable rigidizable structural concepts[C]. Novada: 37th AIAA Aerospace sciences Meeting and Exhibit, 1999.

[8] GUNNA TIBERT. Deployable tensegrity structure for space application[D]. UK: Department of Mechanics, Royal Institute of Technology, Doctoral Thesis, 2002.

[9] BOWDEN M, BENTON M. Design of deployable trussmast for space station [C]. California:AIAA/AHS/ASEE Aerospace Design Conference, 1993.

[10] HAYMAN, HEDGEPETH G J, PARK J M, et al. Design freedoms of articulating Astromast and their optimization for improved performance[C]. Washington, DC:the 35thAIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference,1994.

[11] ANON. Solar array flight experiment [R ]. NASA-CR-183535, 1986.

[12] TAKAYUKI KITAMURA, OKAZAKI KAKUMA, NATORI MICHIHIRO. Development of a hingeless mast and its application[C]. Innsbruck: 37th Congress of the International Astronautical Federation,1986.

[13] KITAMURA TAKAYUKI, OKAZAKI KAKUMA, YAMASHIRO K. Developments of extendible beams for space applications[C]. California: AIAA/AHS/ASEE Aerospace Design Conference,1993.

[14] 张淑杰, 李瑞祥, 丁同才. 盘绕式杆状展开机构的设计与力学分析[J] . 力学季刊, 2006, 27(2): 341-347.

[15] 王炜. 盘压杆展开机构的研究 [D ] . 北京: 中国空间技术研究院, 2000.

[16] 刘义良, 王春洁, 孟晋辉. 基于ANSYS的盘压杆机构大变形有限元分析 [J ] . 通用机械 ,200(1): 73-75.

[17] 刘延柱, 薛纭. 弹性杆盘绕折叠的力学分析 [J ] . 力学季刊, 2008, 29(3):343-348. 

[18] 戈冬明, 陈务军, 董石麟. 盘绕式空间可伸展臂展开状态结构动力研究[C]. 浙江大学第四届海峡两岸结构与岩土工程学术研讨会文集, 杭州, 2007: 602607.

[19] DOUGLAS MARK V, CALIF SANTA BARBARA. Module for an articulated stowable and deployable mast [P]. US,5,267,424,1993.

[20] CRAWFORD R F. Strength and efficiency of deployable booms for space applications[C ]. California: AAS/AIAA Variable Geometry and Expandable Structures Conference, 1971.
[21] JONES P A, SPENCE B R. Spacecraft solar array technology trends [J ]. IEEE, 1998, 1(1):141-152.

[22] 胡其彪. 空间可伸展结构的设计及动力学分析研究[D] . 杭州: 浙江大学, 2001.

[23] 石卫华. 索杆式展开结构的设计与分析及骨架式膜结构研究[D] . 杭州: 浙江大学, 2003.

[24] 郭宏伟, 刘荣强, 邓宗全,等. 空间索杆式伸展臂展开过程力学分析与仿真[J] . 机械设计, 2008,25(7),31-35.

[25] 阎绍泽, 季林红, 吴德隆,等. 航天多铰接机械系统动力学研究[J]. 机械科学与技术, 2000,19(4):517-520.

[26] 阎绍泽, 黄铁球, 张永,等.航天多铰接机械系统动力学分析与设计[C]. 北京: 中国机械工程学会第三届全国青年学术会议,1998.