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    • 22. 发明授权
    • Ablator compositions
    • 消音器组成
    • US5905101A
    • 1999-05-18
    • US616518
    • 1996-03-19
    • Hironao FujikiMorio OhashiHisao Okamoto
    • Hironao FujikiMorio OhashiHisao Okamoto
    • B64G1/58C08K3/04C08K3/34C08K3/36C08K7/04C08K7/06C08K7/10C08L83/04C08L83/07
    • C08K7/06B64G1/58C08K3/36C08K7/10
    • The invention relates to an ablator composition for providing ablation protection after cure thereof. The. ablator composition includes the components of: (A) 100 parts by weight of a silicone elastomer composition which is curable to a silicone elastomer by addition reaction; (B) 50-200 parts by weight of an amorphous silica having an average diameter from 0.1 to 100 .mu.m; and (C) 1-15 parts by weight of a first fiber having an average length from 0.5 to 6 mm in a longitudinal direction thereof and an average diameter from 1 to 20 .mu.m. The first fiber is at least one of a carbon fiber and a synthetic quartz fiber. An ablating material prepared by curing the ablator composition is superior in heat insulation and substantially low in ablation rate, and thus protects a spacecraft or the like from a high temperature gas, for a long time.
    • 本发明涉及一种用于在其固化后提供消融保护的消融器组合物。 的。 消泡剂组合物包括以下组分:(A)100重量份通过加成反应可固化到硅氧烷弹性体的硅氧烷弹性体组合物; (B)50-200重量份平均直径为0.1-100μm的无定形二氧化硅; 和(C)1-15重量份的长度方向平均长度为0.5〜6mm,平均直径为1〜20μm的第一纤维。 第一纤维是碳纤维和合成石英纤维中的至少一种。 通过消融器组合物固化而形成的消融材料绝热性能优异,烧蚀速度基本较低,能长时间保护航天器等高温气体。