UDC 621.577

L. Vasiliev , D. Nikanpour , A. Antuh , K. Snelson ,
L. Vasiliev Jr. , A. Lebru

MULTISALT-CARBON CHEMICAL COOLER
FOR SPACE APPLICATIONS

Introduction. Thermal management systems for future 
large spacecraft or high power constellations of small satellites 
must be able to handle high power densities for final heat rejection 
to space. Currently passive radiators or single-phase / two-phase 
(liquid-vapor) mechanically, or capillary pumped systems have been 
developed as thermal control systems relying on heat by collection 
through evaporation and heat release by condensation via space radiators.

Academic Scientific Complex
"A. V. Luikov Heat and Mass Transfer
Institute" of the National Academy
of Sciences of Belarus, Minsk

IFZH74920199913
IFZH7492013