低密度双基体烧蚀防热材料
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航天材料及工艺研究所,先进功能复合材料技术重点实验室

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Low Density Bi鄄Matrix Ablative Composites
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    摘要:

    采用硅基针刺毡作为增强体、先后浸渍无机和有机树脂基体的两次复合工艺,可制成密度<1. 20
    g/ cm3的双基体烧蚀防热材料。通过马弗炉烘烤、石英灯静态隔热、电弧风洞加热三种方式考核材料的剩余强
    度、抗变形能力、隔热性能和抗冲刷能力。结果表明:该材料在有氧条件下,经马弗炉1 100益、3 000 s 烘烤,剩
    余基体还有20wt%,材料仍具有一定强度;石英灯加热至1 200益,总时长1 200 s 的条件下,25 mm 厚的试样最
    终背温<120益;电弧风洞考核显示,材料抗冲刷能力强,880 s 时,25 mm 厚材料背温仅有71益。

    Abstract:

    Using the processing technology of impregnating silica鄄based needle felt with inorganic and organic
    resin matrix composites successively, bi鄄matix ablative comoposites with density less than 1. 20 g/ cm3 can be ob鄄
    tained. Residual strength, non鄄deformability, heat insulation performance and anti鄄erosion properties of this bi鄄matrix
    ablative composites are assessed through three methods, including muffle furnace baking, quartz lamp static heat insula鄄
    tion and arc air tunnel heating. The results show that after muffle furnace baking at 1 100益for 3 000 s under aerobic
    conditions, the matrix remains 20% and still has sufficient strength. While quartz lamp heating for 1 200 s with 1 200益
    peak temperature, the back temperature of 25 mm thick specimens is lower than 120益. Arc air tunnel heating results
    show that the bi鄄matrix ablative composites have outstanding anti鄄erosion properties and the back temperature of 25
    mm thick spicemens is 71益merely.

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华小玲.低密度双基体烧蚀防热材料[J].宇航材料工艺,2013,43(2).

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  • 在线发布日期: 2016-11-28
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