弱刚性纤维增强树脂基防热材料的表面状态控制及表征研究
CSTR:
作者:
作者单位:

1.北京卫星制造厂有限公司,北京 100094;2.北京空间飞行器总体设计部,北京 100094

作者简介:

通讯作者:

中图分类号:

V19

基金项目:


Surface State Control and Evaluation of Weak Rigidity Fiber-reinforced Resin-based Thermal Protection Material
Author:
Affiliation:

1.Beijing Spacecrafts,Beijing 100094;2.Beijing Institute of Spacecraft System Engineering,Beijing 100094

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:

    针对空间探测领域返回舱热防护结构轻量化及表面功能涂层的工程应用问题,开展了基于低密度弱刚性纤维增强树脂基防热材料直接实施表面功能涂层需求的表面状态加工控制及表面状态表征研究。本研究创新地将手持式3D微观扫描仪应用到低密度弱刚性纤维增强树脂基防热材料加工表面状态表征,并验证了其可行性和适用性。研究掌握了加工参数对低密度弱刚性纤维增强树脂基防热材料表面状态的影响规律,确定了有效控制表面状态的精加工参数,即工步距参数为0.2 mm,加工转速为7 000 r/min,加工切深为0.5 mm,成功地将加工表面纤维凸起高度控制在<0.2 mm,满足后续在该类材料直接实施热控功能涂层的基材表面状态要求。该研究成果对空间飞行器热防护技术发展和应用具有重要工程价值。

    Abstract:

    Be aimed at engineering application of lightweight thermal protection structure and surface functional coatings in space exploration,research on surface state processing control and characterization of surface functional coatings based on the requirement for direct implementation of low-density weak rigid fiber-reinforced resin-based thermal protection material was conducted. The handheld 3D-Microscopic scanner was innovatively applied to evaluate the surface state, and its application and feasibility was verified in the study. The influence of precision processing parameters on the surface state of low-density weak rigid fiber-reinforced resin-based heat protection material was identified, and optimal parameters for effective control of surface state were determined as follows: step distance of 0.2 mm,rotate speed of 5000 r/min and cutting depth of 0.5 mm. The fiber raised height of machined surface was successfully controlled below 0.2 mm, meeting the surface state requirements for the subsequent direct application of thermal control functional coatings. The research results hold significant engineering value for the development and application of thermal protection technology in space vehicle.

    参考文献
    相似文献
    引证文献
引用本文

雷尧飞,马彬,孟博,张鹏飞,刘佳.弱刚性纤维增强树脂基防热材料的表面状态控制及表征研究[J].宇航材料工艺,2025,55(6):105-110.

复制
分享
相关视频

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:2024-05-09
  • 最后修改日期:2024-07-13
  • 录用日期:2024-10-29
  • 在线发布日期: 2025-12-29
  • 出版日期:
文章二维码