AEROSPACE CHINA

中国航天科技集团有限公司主管

中国航天系统科学与工程研究院主办

ISSN 1671-0940

CN 11-4673/V

导航

AEROSPACE CHINA ›› 2022, Vol. 23 ›› Issue (3): 44-50.doi: 10.3969/j.issn.1671-0940.2022.03.007

• 学术研究 • 上一篇    下一篇

A Study of Low-Density Heat-Resistant Coating for New-Generation Launch Vehicle Fairings

  

  • 出版日期:2022-12-13 发布日期:2022-12-13

A Study of Low-Density Heat-Resistant Coating for New-Generation Launch Vehicle Fairings

  1. 1 Shanghai Aerospace Equipments Manufacturing Co. Ltd., Shanghai 200245
    2 Shanghai Jiao Tong University, Shanghai 200240
    3 Shanghai Aerospace System Engineering Institute, Shanghai 201109
  • Online:2022-12-13 Published:2022-12-13

Abstract: In this paper, the properties of different low-density heat-resistant coating prescriptions were compared, and a heat-resistant coating with a density of 0.65 g/cm3, a tensile strength of 2.04 MPa, and a thermal conductivity of 0.126 W/(m·K) was obtained. The thermal performance of the coating was characterized by an oxygen-acetylene ablation test, a hot radiation test using a quartz lamp and in an arc-heated wind tunnel test. The results indicated that the low-density heat-resistant coating prescription has advantages of high temperature resistance, erosion resistance, ablative resistance and excellent heat resistance, which can satisfy the heat resistance requirements of new-generation launch vehicle fairings.
The successful application of this heat-resistant coating technology resolved the problems of low efficiency and poor adhesive performance of the traditional hand-pasted cork process, and realized the rapid spray application of the thermal protection layer, effectively improved the manufacturing efficiency and production quality of the heat-resistant layer of new-generation launch vehicle fairings.

Key words: