TY - JOUR
T1 - Design of highly reflective film for smart radiation device
AU - Wang, Xiaoqian
AU - Yang, Junlin
AU - Li, Donglai
AU - Ye, Hui
AU - Ling, Chen
AU - Li, Jingbo
AU - Jin, Haibo
N1 - Publisher Copyright:
Copyright © 2022 Xiaoqian Wang, et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
PY - 2022/2/1
Y1 - 2022/2/1
N2 - Smart radiation device (SRD) based on the asymmetrical Fabry-Perot cavity automatically tune its IR emittance depending on the ambient temperature, making it an ideal choice for thermal control system of spacecrafts. The low solar absorption is desirable for SRD to prevent the spacecraft from overheating by sun light. In this paper, a multilayer highly reflective film with (LH)k stacking layers is designed to reduce the solar absorptance (As) of the Ag/Al2O3/VO2 structured SRD. The reflective film achieves a high reflection band in ~220 nm bandwidth from 460 nm to 680 nm, which results in a reduction of the solar absorptance by 25.56 % for SRD working at low temperature and 24.27 % at high temperature as the stacking factor k = 5. The simulation results indicate that an economic reflective film with k = 3 can achieve effective suppression of As of SRD, demonstrating the promising potential of the proposed reflective film in thermal control application of spacecrafts.
AB - Smart radiation device (SRD) based on the asymmetrical Fabry-Perot cavity automatically tune its IR emittance depending on the ambient temperature, making it an ideal choice for thermal control system of spacecrafts. The low solar absorption is desirable for SRD to prevent the spacecraft from overheating by sun light. In this paper, a multilayer highly reflective film with (LH)k stacking layers is designed to reduce the solar absorptance (As) of the Ag/Al2O3/VO2 structured SRD. The reflective film achieves a high reflection band in ~220 nm bandwidth from 460 nm to 680 nm, which results in a reduction of the solar absorptance by 25.56 % for SRD working at low temperature and 24.27 % at high temperature as the stacking factor k = 5. The simulation results indicate that an economic reflective film with k = 3 can achieve effective suppression of As of SRD, demonstrating the promising potential of the proposed reflective film in thermal control application of spacecrafts.
KW - Emittance
KW - Fabry-Perot cavity
KW - Highly reflective film
KW - Smart radiation device (SRD)
KW - Solar absorption
UR - http://www.scopus.com/inward/record.url?scp=85124660204&partnerID=8YFLogxK
U2 - 10.21595/vp.2022.22385
DO - 10.21595/vp.2022.22385
M3 - Conference article
AN - SCOPUS:85124660204
SN - 2345-0533
VL - 40
SP - 132
EP - 138
JO - Vibroengineering Procedia
JF - Vibroengineering Procedia
T2 - 54th International Conference on Vibroengineering
Y2 - 5 February 2022
ER -