碳纤维-微晶复合材料反射镜光学加工实验
DOI:
CSTR:
作者:
作者单位:

北京空间机电研究所

作者简介:

通讯作者:

中图分类号:

基金项目:


Optical Polishing Experiment of Cf -Zerodur Composites Mirror
Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    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.

    参考文献
    相似文献
    引证文献
引用本文

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).

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2016-11-28
  • 出版日期:
文章二维码