1.State Key Laboratory of Extreme Photonics and Instrumentation, College of Optical Science and Engineering, Zhejiang University, Hangzhou 310027, China
2.Key Laboratory of 3D Micro/Nano Fabrication and Characterization of Zhejiang Province, School of Engineering, Westlake University, Hangzhou 310024, China
Qiang Li (qiangli@zju.edu.cn)
收稿日期:2024-10-09,
修回日期:2025-02-20,
录用日期:2025-03-04,
网络出版日期:2025-03-26,
纸质出版日期:2025-05-31
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Space-to-ground infrared camouflage with radiative heat dissipation[J]. LSA, 2025,14(5):1410-1419.
Qin, B. et al. Space-to-ground infrared camouflage with radiative heat dissipation. Light: Science & Applications, 14, 1410-1419 (2025).
Space-to-ground infrared camouflage with radiative heat dissipation[J]. LSA, 2025,14(5):1410-1419. DOI: 10.1038/s41377-025-01824-y.
Qin, B. et al. Space-to-ground infrared camouflage with radiative heat dissipation. Light: Science & Applications, 14, 1410-1419 (2025). DOI: 10.1038/s41377-025-01824-y.
With the development of space exploration and exploitation
it is imperative to address the potential threats posed to space objects
particularly ground-based infrared observation. However
in the extreme space environment
achieving infrared camouflage across different bands with simultaneous thermal management is challenging and has so far slipped out of concern. Here
we propose the space-to-ground infrared camouflage strategy
compatible with radiative heat dissipation. Camouflage in the H
K
mid-wave-infrared (MWIR)
and long-wave-infrared (LWIR) bands is achieved through a multilayer structure
with radiative heat dissipation in the very-long-wave-infrared (VLWIR) band. High absorptivity (0.839/0.633) in the H/K bands minimizes the reflected signal of solar radiation and low emissivity (0.132/0.142) in the MWIR/LWIR bands suppresses the thermal radiation signal. Additionally
high emissivity (0
.798) in the VLWIR band ensures efficient thermal management
resulting in a temperature decrement of 39.8 ℃ to the metal reference in the simulated space environment (with 1200 W m
−2
thermal input). This work inspires sophisticated spectral manipulation in extreme environments and guides the development of camouflage and radiative heat dissipation techniques for space objects.
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