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Analysis of a radiative heat exchanger for systems for thermal control of space vehicles

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Abstract

Starting from the solution of a two-dimensional heat conduction problem, a mathematical model of a heat pipe-based radiative heat exchanger is developed. Good agreement between the predicted and experimental results is obtained. The effect of operational and structural parameters on the characteristics of the radiative heat exchanger is analyzed.

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References

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Authors
  1. L. L. Vasil'ev
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  2. L. E. Kanonchik
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  3. V. A. Babenko
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Additional information

Academic Scientific Complex “The A. V. Luikov Heat and Mass Transfer Institute of the Academy of Sciences of Belarus,” Minsk. Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 67, Nos. 3–4, pp. 261–265, September–October, 1994.

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Vasil'ev, L.L., Kanonchik, L.E. & Babenko, V.A. Analysis of a radiative heat exchanger for systems for thermal control of space vehicles. J Eng Phys Thermophys 67, 917–921 (1994). https://doi.org/10.1007/BF00853020

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  • DOI: https://doi.org/10.1007/BF00853020

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