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Use of a chemical heat pump in a heat-emitting space system.

Utilisation d'une pompe à chaleur chimique dans un système spatial de rejet thermique.

Author(s) : VALKOV V., NIKANPOUR D., PAROLIS L. de

Summary

This article presents the results obtained when chemical heat pumps were used in a radiator-heat pump application designed for use in a lunar station. The cooling power inside the station was 2 kilowatts. The temperature of the lunar environment is -70 deg C. Various chemical heat pump design variants were considered: two reactors, a condenser and an evaporator; four reactors and two salts, requiring neither a condenser nor an evaporator; multi-effect designs.

Details

  • Original title: Utilisation d'une pompe à chaleur chimique dans un système spatial de rejet thermique.
  • Record ID : 1998-2530
  • Languages: French
  • Source: Ab-sorption 96. Towards sustainable technologies. Proceedings./ Ab-sorption 96. Vers les technologies durables. Comptes rendus.
  • Publication date: 1996/09/17
  • Document available for consultation in the library of the IIR headquarters only.

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