碳纤维-微晶复合材料反射镜光学加工实验
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北京空间机电研究所

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Optical Polishing Experiment of Cf -Zerodur Composites Mirror
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    摘要:

    采用环抛方法对有预埋件和无预埋件的两块碳纤维-微晶复合材料反射镜进行光学加工,之后
    进行了稳定性实验研究,采用Zygo 干涉仪实测了碳纤维-微晶复合材料反射镜面形。稳定实验后,有预埋件反
    射镜面形P-V 值为3. 013λ,RMS 值为0. 669λ;无预埋件反射镜面形P-V 值为2. 313λ,RMS 值为0. 276λ(λ =
    632. 8 nm)。实验结果证明,有预埋件的碳纤维-微晶复合材料反射镜结构优于无预埋件结构,为碳纤维-微晶
    复合材料反射镜的工程化提供参考。

    Abstract:

    The two cf-zerodur composites mirrors with and without pre-embedded parts are polished by continuous
    polishing method, and they are under stability experiment after polishing. The surface figures of the cf-zerodur
    composites mirrors are measured by a Zygo interferometer. The surface errors of the mirror without pre-embedded parts
    after the stability experiment are as follows:the P-V error is 2. 313λ,the RMS error is 0. 669λ. The surface errors of
    the mirror with pre-embedded parts after the stability experiment are as follows: the P-V error is 3. 013λ,the RMS error
    is 0. 276λ(λ =632. 8 nm). The experimental results show that the structure of cf-zerodur composites mirror with
    pre-embedded parts is better than that of without pre-embedded parts. The paper presents some references for the application
    of cf-zerodur composites mirrors.

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王慧军.碳纤维-微晶复合材料反射镜光学加工实验[J].宇航材料工艺,2013,43(4).

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  • 在线发布日期: 2016-11-28
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第十一届航天复合材料成形与加工工艺技术中心交流会 征文通知

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