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Consequences of atomic oxygen interaction with silicone and silicone contamination on surfaces in low earth orbit

机译:低地球轨道表面上原子氧与有机硅和有机硅污染物相互作用的后果

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Abstract: The exposure of silicones to atomic oxygen in low Earth orbit causes oxidation of the surface, resulting in conversion of silicone to silica. This chemical conversion increases the elastic modulus of the surface and initiates the development of a tensile strain. Ultimately, with sufficient exposure, tensile strain leads to cracking of the surface enabling the underlying unexposed silicone to be converted to silica resulting in additional depth and extent of cracking. The use of silicone coatings for the protection of materials from atomic oxygen attack is limited because of the eventual exposure of underlying unprotected polymeric material due to deep tensile stress cracking of the oxidized silicone. The use of moderate to high volatility silicones in low Earth orbit has resulted in a silicone contamination arrival at surfaces which are simultaneously being bombarded with atomic oxygen, thus leading to conversion of the silicone contaminant to silica. As a result of these processes, a gradual accumulation of contamination occurs leading to deposits which at times have been up to several microns thick (as in the case of a Mir solar array after 10 years in space). The contamination species typically consists of silicon, oxygen and carbon, which in the synergistic environment of atomic oxygen and UV radiation leads to increased solar absorptance and reduced solar transmittance. A comparison of the results of atomic oxygen interaction with silicones and silicone contamination will be presented based on the LDEF, EOIM-III, Offeq-3 spacecraft and Mir solar array in-space results. The design of a contamination pin-hole camera space experiment which uses atomic oxygen to produce an image of the sources of silicone contamination will also be presented. !11
机译:摘要:低地球轨道上的有机硅暴露于原子氧会导致表面氧化,从而导致有机硅转化为二氧化硅。这种化学转化增加了表面的弹性模量并引发了拉伸应变的发展。最终,在充分暴露的情况下,拉伸应变会导致表面破裂,从而使下面未暴露的有机硅转化为二氧化硅,从而导致破裂的深度和程度增加。由于由于氧化的硅氧烷的深拉伸应力开裂而最终暴露出下面的未保护的聚合物材料,因此限制了将硅氧烷涂料用于保护材料免受原子氧侵袭的使用。在低地球轨道上使用中度至高挥发性有机硅会导致有机硅污染物到达表面,同时被原子氧轰击,从而导致有机硅污染物转化为二氧化硅。这些过程的结果是,污染物逐渐积累,导致沉积物有时高达几微米厚(如在空间中放置10年后的Mir太阳电池阵列)。污染物质通常由硅,氧和碳组成,在原子氧和紫外线辐射的协同环境中,这会导致日光吸收率增加和日光透射率降低。将基于LDEF,EOIM-III,Offeq-3航天器和Mir太阳电池阵列空间结果,对原子氧与有机硅相互作用和有机硅污染的结果进行比较。还将介绍使用原子氧产生有机硅污染源图像的针孔照相机污染空间实验的设计。 !11

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