Space Environment Simulation Tests for Black Polyimide Film

被引:0
作者
Wang, Lei [1 ]
Cao, Yun-zhen [2 ]
机构
[1] Qian Xuesen Lab Space Technol, Beijing 100094, Peoples R China
[2] Chinese Acad Sci, Shanghai Inst Ceram, Key Lab Inorgan Coating Mat, Shanghai 200050, Peoples R China
来源
PROTECTION OF MATERIALS AND STRUCTURES FROM THE SPACE ENVIRONMENT, ICPMSE-11 | 2017年 / 47卷
关键词
Black polyimide film; Degradation; Solar absorptance; Irradiation test;
D O I
10.1007/978-3-319-19309-0_6
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Black polyimide film is electrically conductive with high solar absorptance and high infrared emittance. The material can be applied as satellite thermal control film to enhance radiative heat transfer and thereby help isothermalize the components of spacecraft. The film can be used in satellite optical devices and telescopes baffle systems to minimize reflection from stray light. In this paper the degradation of solar absorptance of black polyimide film under simulated space environment tests such as thermal cycling, ultraviolet irradiation, proton irradiation and electron irradiation are reported. The test results show that the black polyimide film has very good stability in simulated space environment.
引用
收藏
页码:53 / 59
页数:7
相关论文
共 6 条
  • [1] Feng W-q, 2007, SPACECRAFT ENV ENG, V24, P27
  • [2] Fogdall LB, 1999, 993678 AIAA, P1
  • [3] Gilmore D.G., 2002, Spacecraft Thermal Control Handbook: Fundamental Technologies, V1
  • [4] Marco J, 2003, P 9 INT S MAT SPAC E
  • [5] Min G.R., 1998, Spacecraft Thermal Control, V2nd ed.
  • [6] Structural characterization of catalytically active metal nanoclusters in poly(amide imide) films with high metal loading
    Troger, L
    Hunnefeld, H
    Nunes, S
    Oehring, M
    Fritsch, D
    [J]. JOURNAL OF PHYSICAL CHEMISTRY B, 1997, 101 (08): : 1279 - 1291