Radiative Cooling in Outer Space: Fundamentals, Advances in Materials and Applications, and Perspectives

Y Yurong Fan (State Key Laboratory of Radiation Medicine and Protection, School of Radiation Medicine and Protection, Collaborative Innovation Centre of Radiological Medicine of Jiangsu Higher Education Institutions) H Hao Chen X Xiaochuan Liu (Institute of Plasma Physics, Hefei Institutes of Physical Science, Chinese Academy of Sciences 2 , Hefei 230031, Anhui,) Y Yong Zhao (Key Lab for Special Functional Materials of Ministry of Education, School of Nano Science and Materials Engineering) Y Yong Huang (National Laboratory of Solid State Microstructures, School of Physics) J Jingchong Liu (School of Chemistry and Biological Engineering, University of Science and Technology Beijing 2 , Beijing 100083,) C Cunhai Wang (School of Energy and Environmental Engineering, University of Science and Technology Beijing 1 , Beijing 100083,)

Abstract

Abstract Effective thermal control is critical for the safe operation of spacecraft in the harsh environment of outer space. Radiative cooling (RC), an advanced passive thermal management technology, enables spontaneous heat dissipation via infrared radiation into the ultracold cosmic background. It offers an energy‐efficient solution for maintaining temperature stability without power input. While RC materials have demonstrated promising potential in space applications, a systematic review focusing specifically on their performance and adaptability in space environments remains lacking. To fill this gap, this review first clarifies the fundamental and material‐requirement differences between terrestrial and space‐based RC. Next, it focuses on the space environmental effects on RC materials and their protection strategies, including extreme temperature fluctuations, space dust deposition, vacuum ultraviolet (VUV) radiation, and atomic oxygen (AO) erosion. Finally, key challenges and future research directions are discussed to guide the development of next‐generation RC materials for integrated spacecraft thermal control. This work provides valuable insights into advancing RC technologies, with implications for improving energy efficiency, extending mission lifespans, and enhancing system reliability in future space exploration.

Article Details

Volume / Issue Vol. 37, Issue 43
Published October 01, 2025
ISSN 0935-9648
Publisher Unknown Publisher

Journal Info

Advanced Materials

Unknown Publisher

ISSN: 0935-9648 Physical Sciences

Authors (7)

Y

Yurong Fan

State Key Laboratory of Radiation Medicine and Protection, School of Radiation Medicine and Protection, Collaborative Innovation Centre of Radiological Medicine of Jiangsu Higher Education Institutions

H

Hao Chen

X

Xiaochuan Liu

Institute of Plasma Physics, Hefei Institutes of Physical Science, Chinese Academy of Sciences 2 , Hefei 230031, Anhui,

Y

Yong Zhao

Key Lab for Special Functional Materials of Ministry of Education, School of Nano Science and Materials Engineering

Y

Yong Huang

National Laboratory of Solid State Microstructures, School of Physics

J

Jingchong Liu

School of Chemistry and Biological Engineering, University of Science and Technology Beijing 2 , Beijing 100083,

C

Cunhai Wang

School of Energy and Environmental Engineering, University of Science and Technology Beijing 1 , Beijing 100083,