MULTISALT-CARBON CHEMICAL COOLER FOR SPACE APPLICATIONS

L. Vasil'ev , D. Nikanpour, A. Antukh , K. Snelson ,
L. Vasil'ev , Jr., and A. Lebru

UDC 621.577

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 ejection 
into 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.

JEPTER74920199913
JEPTER7492013