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    Influence of Buffer Substance on Separation Mechanism of CFRP-Based Separation Devices with Shaped Charges

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 004::page 04022037
    Author:
    Fei Weng
    ,
    Jing Sun
    ,
    Lina Feng
    ,
    Zhongwei Zhang
    ,
    Jie Li
    ,
    Yong Cao
    DOI: 10.1061/(ASCE)AS.1943-5525.0001434
    Publisher: ASCE
    Abstract: Metal materials still dominate the separation shell of pyrotechnic separation devices in space launch vehicles. Moreover, research on carbon-fiber–reinforced polymer (CFRP) composites as a separation shell material has mainly focused on the exploration and test stages. Based on safety and environmental adaptability, the buffer substance in separation devices has a great influence on the cutting results of laminates. In this study, compared with the traditional separation device, a new separation device with a shaped charge and buffer substance was designed by finite-element analysis (FEA), and a test was carried out. The predesigned cutting strategies were divided into three categories: no buffer, expansion–deformation energy-absorbing (EDEA) material buffer, and low-density energy-absorbing (LDEA) material buffer as the control group. Based on the separation time of the laminate, delamination of the laminate, deformation of the protective cover, and environmental applicability of the device, the results show that the proposed separation device with LDEA as a buffer is the best, and the trend of delamination is consistent in FEA and the test. The LDEA buffer can effectively reduce the secondary damage of detonation products to the laminate by crushing and absorbing energy to improve the separation effect of the separation shell, providing guidance for the design of CFRP-based separation devices with shaped charges.
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      Influence of Buffer Substance on Separation Mechanism of CFRP-Based Separation Devices with Shaped Charges

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4281794
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    contributor authorFei Weng
    contributor authorJing Sun
    contributor authorLina Feng
    contributor authorZhongwei Zhang
    contributor authorJie Li
    contributor authorYong Cao
    date accessioned2022-05-07T19:53:50Z
    date available2022-05-07T19:53:50Z
    date issued2022-03-25
    identifier other(ASCE)AS.1943-5525.0001434.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4281794
    description abstractMetal materials still dominate the separation shell of pyrotechnic separation devices in space launch vehicles. Moreover, research on carbon-fiber–reinforced polymer (CFRP) composites as a separation shell material has mainly focused on the exploration and test stages. Based on safety and environmental adaptability, the buffer substance in separation devices has a great influence on the cutting results of laminates. In this study, compared with the traditional separation device, a new separation device with a shaped charge and buffer substance was designed by finite-element analysis (FEA), and a test was carried out. The predesigned cutting strategies were divided into three categories: no buffer, expansion–deformation energy-absorbing (EDEA) material buffer, and low-density energy-absorbing (LDEA) material buffer as the control group. Based on the separation time of the laminate, delamination of the laminate, deformation of the protective cover, and environmental applicability of the device, the results show that the proposed separation device with LDEA as a buffer is the best, and the trend of delamination is consistent in FEA and the test. The LDEA buffer can effectively reduce the secondary damage of detonation products to the laminate by crushing and absorbing energy to improve the separation effect of the separation shell, providing guidance for the design of CFRP-based separation devices with shaped charges.
    publisherASCE
    titleInfluence of Buffer Substance on Separation Mechanism of CFRP-Based Separation Devices with Shaped Charges
    typeJournal Paper
    journal volume35
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001434
    journal fristpage04022037
    journal lastpage04022037-10
    page10
    treeJournal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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