This paper describes a VO2-based smart structure with an emittance that increases with the temperature. A large tunability of the spectral emittance, which can be as high as 0.90, was achieved. The transition of the total emittance with the temperature was fully reversible according to a hysteresis cycle, with a transition temperature of 66.5 degrees C. The total emittance of the device was found to be 0.22 and 0.71 at 25 degrees C and 100 degrees C, respectively. This emittance performance and the structure simplicity are promising for the next generation of energy-efficient cost-effective passive thermal control systems of spacecrafts. (C) 2013 American Institute of Physics. [http://dx.doi.org/10.1063/1.4792277]
机构:
Institute for Theoretical and Applied Electromagnetics, Russian Academy of Sciences, MoscowInstitute for Theoretical and Applied Electromagnetics, Russian Academy of Sciences, Moscow
Lelyuk D.P.
Mishin A.D.
论文数: 0引用数: 0
h-index: 0
机构:
Institute for Theoretical and Applied Electromagnetics, Russian Academy of Sciences, MoscowInstitute for Theoretical and Applied Electromagnetics, Russian Academy of Sciences, Moscow
Mishin A.D.
Maklakov S.S.
论文数: 0引用数: 0
h-index: 0
机构:
Institute for Theoretical and Applied Electromagnetics, Russian Academy of Sciences, MoscowInstitute for Theoretical and Applied Electromagnetics, Russian Academy of Sciences, Moscow
Maklakov S.S.
Makarevich A.M.
论文数: 0引用数: 0
h-index: 0
机构:
Lomonosov Moscow State University, MoscowInstitute for Theoretical and Applied Electromagnetics, Russian Academy of Sciences, Moscow
Makarevich A.M.
Sharovarov D.I.
论文数: 0引用数: 0
h-index: 0
机构:
Lomonosov Moscow State University, MoscowInstitute for Theoretical and Applied Electromagnetics, Russian Academy of Sciences, Moscow