适用于长时间烧蚀防热的蜂窝增强低密度材料
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航天材料及工艺研究所

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TB34

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The Low Density Materials Reinforced by Honeycombfor Long Time Ablation and Thermal Protection
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    摘要:

    针对长时间烧蚀防热对防热材料的需求,研制了两种蜂窝增强低密度烧蚀防热材料,采用电弧风
    洞加热设备对其防热性能进行了考核,并对其力学及热物理性能进行了研究。结果表明,在两种长时间(1 000
    s 左右)热环境的考核下,蜂窝增强低密度材料烧蚀后背面温度均低于200℃,表面碳层均匀、完整,无明显烧蚀
    量,显示了优异的隔热性能和良好的抗气流冲刷能力。

    Abstract:

    Two kinds of low density ablative thermal protection materials reinforced by honeycomb was developed
    according to the requirements of long time ablation and thermal protection. Arc heated wind tunnel experimental were
    applied to test their property of thermal protection. Their mechanical property and thermophysical property were researched
    also. The carbon layer of the low density materials reinforced by honeycomb on the surface was even and intact
    after ablation without erosion markedly while the back temperatures were below 200℃ under the two long time(1 000 s)
    heat environment and excellent heat-insulating property and well poperty of resisting the flush of gas flow was displayed.

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邓火英 谭 珏 谭朝元 梁 馨 孙红卫.适用于长时间烧蚀防热的蜂窝增强低密度材料[J].宇航材料工艺,2014,44(1).

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  • 在线发布日期: 2016-11-28
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