A study on grid-stiffened multi-functional composite structures with radiation spot shielding

被引:8
|
作者
Jang, T. S. [1 ]
Rhee, J. [2 ]
Hyun, B. -S. [2 ]
Seo, H. -S. [3 ]
Kim, T. Y. [4 ]
Seo, J. K. [1 ]
机构
[1] Korea Adv Inst Sci & Technol, Satellite Technol Res Ctr, 291 Daehak Ro, Taejon 305701, South Korea
[2] Korea Aerosp Res Inst, 169-84 Gwahak Ro, Daejeon 305806, South Korea
[3] Korea Aerosp Ind, 802 Yucheon Ri, Sacheon Si 664710, Gyeongsangnam D, South Korea
[4] Korea Polytech Univ, Dept Mech Engn, 237 Sangidaehak Ro, Siheung Si 429793, Gyeonggi Do, South Korea
关键词
Multi-functional structures; Grid-stiffened composite panel; Spacecraft; Radiation shielding; Lightweight composite materials; SPACECRAFT;
D O I
10.1016/j.ast.2016.05.002
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper deals with alternative multi-functional structures by using grid-stiffened composite panel with excellent bending stiffness and lightweight characteristics. The grid-stiffened multi-functional structure can provide an array of available rooms for integrating multiple electronic circuitries into structure with ease. The substrate fabrication process was proposed and the grid-stiffened multi-functional structure equipped with several electronics and interfaces was built up. In order to improve the thermal conduction capability, pitch-based carbon fibers were applied to facesheet of the multi-functional structure. The spot shielding technique was also proposed to enhance the radiation shielding at the selective region sensitive to radiation, and the lightweight radiation spot shielding plate was fabricated with multi-layered laminate of CFRP and tungsten foil. The radiation shielding effectiveness of the multi-functional structure with spot shielding plate was demonstrated by proton beam irradiation test. Through the test, it was found that the radiation spot shielding plate has comparable proton-shielding performance to aluminum but more lightweight characteristics than aluminum. Grid-stiffened MFS with radiation spot shielding can be an effective measure for accommodating lots of electronics into structure, providing dramatic mass and volume savings in spacecraft design. (C) 2016 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:330 / 339
页数:10
相关论文
共 50 条
  • [1] Study of filament wound grid-stiffened composite cylindrical structures
    Buragohain, M.
    Velmurugan, R.
    COMPOSITE STRUCTURES, 2011, 93 (02) : 1031 - 1038
  • [2] Fiber-placed composite grid-stiffened structures
    Van West, BP
    Wegner, P
    ADVANCING AFFORDABLE MATERIALS TECHNOLOGY, 2001, 33 : 782 - 791
  • [3] BUCKLING OPTIMIZATION OF STEERING STIFFENERS FOR GRID-STIFFENED COMPOSITE STRUCTURES
    Wang, Dan
    Abdalla, Mostafa M.
    20TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS, 2015,
  • [4] EFFECT OF STIFFNESS CHARACTERISTICS ON THE RESPONSE OF COMPOSITE GRID-STIFFENED STRUCTURES
    AMBUR, DR
    REHFIELD, LW
    JOURNAL OF AIRCRAFT, 1993, 30 (04): : 541 - 546
  • [5] A sizing method for cylindrical grid-stiffened structures in composite material
    Gatta, G
    Romano, F
    HIGH PERFORMANCE STRUCTURES AND MATERIALS II, 2004, : 551 - 560
  • [7] Scaling effects in the manufacture and testing of grid-stiffened composite structures
    Alantali, A.
    Alia, R. A.
    Umer, R.
    Cantwell, W. J.
    JOURNAL OF COMPOSITE MATERIALS, 2018, 52 (17) : 2351 - 2363
  • [8] Buckling optimization design of curved stiffeners for grid-stiffened composite structures
    Wang, Dan
    Abdalla, Mostafa M.
    Zhang, Weihong
    COMPOSITE STRUCTURES, 2017, 159 : 656 - 666
  • [9] Optimal Design of Filament Wound Grid-stiffened Composite Cylindrical Structures
    Buragohain, M.
    Velmurugan, R.
    DEFENCE SCIENCE JOURNAL, 2011, 61 (01) : 88 - 94
  • [10] The effects of delamination deficiencies on compressive properties of composite grid-stiffened structures
    Mo, Yihua
    Cheng, Gengdong
    Wang, Bing
    Wang, Xiaohong
    MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 2018, 25 (11) : 901 - 916