Deflection of multicellular inflatable tubes for redundant space structures

被引:3
|
作者
Sakamoto, H
Natori, MC
Miyazaki, Y
机构
[1] Inst Space & Astronaut Sci, Kanagawa 2298510, Japan
[2] Nihon Univ, Chiba 2748501, Japan
关键词
D O I
10.2514/2.3892
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A new concept of redundant space structures using multicellular inflatable elements is proposed, and the results of basic analyses on simple multicellular models are reported. Much effort has been devoted to methods for sufficiently hardening the inflatable elements in space to tolerate damage sustained from space debris, especially with respect to rigidization of a membrane; however, if the structures are redundant, they do not need to be as stiff and strong as those without redundancy. Deflections of two kinds of multicellular cantilever inflatable tubes are numerically investigated. First, nonrigidized tubes are analyzed by the modified Euler-Bernoulli beam theory. Second, rigidized tubes with slackening effects of the membrane are simulated using the modified nonlinear finite element method. The results show that multicellular tubes can be redundant against problems with pressurization and can be as stiff and as strong as monocellular models with less internal gas. In the multicellular rigidized inflatable tubes, maintaining a small amount of internal pressure is quite effective to prevent the deformation of the cross section, which causes a drop in stiffness and strength. Therefore, adopting a redundant system is effective both for rigidized and nonrigidized inflatable elements.
引用
收藏
页码:695 / 700
页数:6
相关论文
共 50 条
  • [31] INFLATABLE STRUCTURES
    BULSON, PS
    SCIENCE JOURNAL, 1970, 6 (07): : 69 - &
  • [33] THERMOMECHANICAL BEHAVIOR OF CFRP TUBES FOR SPACE STRUCTURES
    REIBALDI, GG
    ACTA ASTRONAUTICA, 1985, 12 (05) : 323 - 333
  • [34] INFLATABLE, SPACE-RIGIDIZED STRUCTURES OVERVIEW OF APPLICATIONS AND THEIR TECHNOLOGY IMPACT
    BERNASCONI, MC
    REIBALDI, GG
    ACTA ASTRONAUTICA, 1986, 14 : 455 - 465
  • [35] Piezoresistive nanocomposites for sensing MMOD impact damage in inflatable space structures
    Gola, Yachna
    Kim, Daewon
    Namilae, Sirish
    COMPOSITES COMMUNICATIONS, 2020, 21
  • [36] Local effects of piezopolymer patches on inflatable space-based structures
    Williams, RB
    Austin, EM
    Inman, DJ
    JOURNAL OF SPACECRAFT AND ROCKETS, 2002, 39 (02) : 299 - 305
  • [37] Advanced capabilities for the simulation of membrane and inflatable space structures using SAMCEF
    Jetteur, Philippe
    Bruyneel, Michael
    TEXTILE COMPOSITES AND INFLATABLE STRUCTURES II, 2008, 8 : 211 - 231
  • [38] INITIAL STRESS CORRECTION METHOD FOR THE MODELING OF FOLDED SPACE INFLATABLE STRUCTURES
    Zhan, Yanan
    Yu, Li
    Yang, Xue
    Cheng, Han
    AVIATION, 2014, 18 (04) : 166 - 173
  • [39] Rigidization analysis of SMA-based inflatable toroidal space structures
    Rastogi, Vikas
    Upadhyay, Sanjay H.
    Singh, Kripa Sankar
    MECHANICS BASED DESIGN OF STRUCTURES AND MACHINES, 2024, 52 (11) : 9334 - 9364
  • [40] Inflatable shape changing colonies assembling versatile smart space structures
    Sinn, Thomas
    Hilbich, Daniel
    Vasile, Massimiliano
    ACTA ASTRONAUTICA, 2014, 104 (01) : 45 - 60