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首页> 外文期刊>Journal of Spacecraft and Rockets >Polydimethylsiloxane/Additive Systems for Thermal and Ultraviolet Stability in Geostationary Environment
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Polydimethylsiloxane/Additive Systems for Thermal and Ultraviolet Stability in Geostationary Environment

机译:聚二甲基硅氧烷/添加剂体系,在地球静止环境中具有热稳定性和紫外线稳定性

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摘要

The development of radiation resistant materials is an ongoing challenge for space industry. High-energy irradiation (ultraviolet, electrons, neutrons, protons) induce damage to materials and electronic components in spaceships. Silicone resins are often used and play a key role as coatings and adhesive materials for satellites. Polydimethylsiloxanes show material exhaustion after long-term exposure to ultraviolet irradiation. Consequently, solutions are required to increase their thermo-and photostability under solar irradiation. Three different families of additives, namely ultraviolet absorbers, hindered amine light stabilizers, and a carbazole derivative are investigated. Those ultraviolet stabilizers were mixed with polydimethylsiloxane, then a cross-linking process was run by hydrosilylation. When ultraviolet absorbers could not be used due to a miscibility problem, addition of 0.5 wt% of bis (2,2,6,6-tetramethylpiperidin-4-yl) decanedioate (hindered amine light stabilizer 1) was shown to increase the thermal stability, measured by thermogravimetric analysis, from 360 to 395 degrees C (Td(5%)). Using visible near-infrared spectroscopy and after 450 equivalent solar hours of ultraviolet irradiation, an average increase of 2.6% in the ultraviolet stability was also obtained in the wavelength range from 250 to 400 nm. A polydimethylsiloxane/dibromocarbazole 1.0 wt% did not improve the ultraviolet stability but exhibited a strong increase (about 100 degrees C) of the degradation temperature of the polydimethylsiloxane.
机译:耐辐射材料的开发是航天工业的一项持续挑战。高能辐射(紫外线,电子,中子,质子)会导致宇宙飞船的材料和电子组件损坏。硅树脂经常被使用,并在人造卫星的涂料和粘合材料中起关键作用。长期暴露于紫外线照射后,聚二甲基硅氧烷显示出材料耗尽。因此,需要解决方案以增加其在太阳辐射下的热稳定性和光稳定性。研究了三种不同的添加剂,即紫外线吸收剂,受阻胺光稳定剂和咔唑衍生物。将那些紫外线稳定剂与聚二甲基硅氧烷混合,然后通过氢化硅烷化进行交联过程。当由于混溶性问题而无法使用紫外线吸收剂时,添加0.5 wt%的双(2,2,6,6-四甲基哌啶-4-基)癸二酸酯(受阻胺类光稳定剂1)会提高热稳定性。通过热重分析在360至395摄氏度(Td(5%))范围内测量。使用可见光近红外光谱法,在450当量太阳小时的紫外线照射后,在250至400 nm的波长范围内,紫外线稳定性也平均提高了2.6%。 1.0重量%的聚二甲基硅氧烷/二溴咔唑没有改善紫外线稳定性,但是显示出聚二甲基硅氧烷的降解温度的强烈增加(约100℃)。

著录项

  • 来源
    《Journal of Spacecraft and Rockets》 |2016年第6期|1128-1133|共6页
  • 作者单位

    Univ Bordeaux, Lab Chim Polymeres Organ, Polymerizat Catalysis & Macromol Design, Bordeaux INP,CNRS,UMR5629, 16 Ave Pey Berland, F-33607 Pessac, France;

    Univ Bordeaux, Lab Chim Polymeres Organ, Polymerizat Catalysis & Macromol Design, Bordeaux INP,CNRS,UMR5629, 16 Ave Pey Berland, F-33607 Pessac, France;

    Univ Bordeaux, Lab Chim Polymeres Organ, Polymerizat Catalysis & Macromol Design, Bordeaux INP,CNRS,UMR5629, 16 Ave Pey Berland, F-33607 Pessac, France;

    Univ Bordeaux, Lab Chim Polymeres Organ, Polymerizat Catalysis & Macromol Design, Bordeaux INP,CNRS,UMR5629, 16 Ave Pey Berland, F-33607 Pessac, France;

    Off Natl Etud & Rech Aerosp, Space Environm Dept, F-31055 Toulouse, France;

    Off Natl Etud & Rech Aerosp, Space Environm Dept, F-31055 Toulouse, France;

    Ctr Natl Etud Spatiales, Thermal Control Dept, 18 Ave Edouard Belin, F-31401 Toulouse, France;

    MAP Coatings ZI, Silicone Polymers Design R&D Dept, 2 Rue Clement Ader, F-09100 Pamiers, France;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
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