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作 者:江伟辉[1] 周健儿[1] 胡行方[2] 吴国庭[3]
机构地区:[1]景德镇陶瓷学院材料工程系,景德镇333001 [2]中国科学院上海硅酸盐研究所,上海200050 [3]北京空间飞行器总体设计部,北京100086
出 处:《无机材料学报》2002年第6期1233-1238,共6页Journal of Inorganic Materials
摘 要:研究了二种烧蚀防热材料的显微结构.研究表明:烧蚀材料1#中的高硅氧玻璃纤维在模拟烧蚀后仍保持其纤维形态不变,并且大、中、小纤维以适当的配比结合,使得纤维堆积密度增大,从而能提高材料的机械强度;烧蚀材料2#具有蜂窝夹心结构,在蜂窝中填充的低密度材料是由50~100μm的空心玻璃球所组成的,这赋予它密度低、隔热性能好的特点.The microstructures of two ablative materials Were studied. The results show that the silica fiber glass in No.1 ablative material remains unchanged after the simulative ablation, and proper combination of the fiber glass with different diameters leads to increase in packing density, which not only makes the ablative material possess high mechanic strength, but also improves its thermal insulation at high temperature. No.2 ablative material has the honeycomb structure. The honeycomb is filled with hollow glass pellets of 50similar to100 mum in diameter. Due to this special structure, No.2 ablative material is characterized by low density and high thermal insulation.
分 类 号:TQ171.77[化学工程—玻璃工业] TQ3[化学工程—硅酸盐工业]
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