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.
Автор:  Vasiliev L., Nikanpour D., Antuh A., Snelson K., Vasiliev L. Jr., Lebru A.
Стр:  595-600