CEM will test two capillary evaporators, the main part of the two-phase heat transfer loops used for thermal control in spacecraft.Principal Investigator(s)
Russian Federal Space Agency (Roscosmos)Sponsoring Organization
Information PendingResearch Benefits
Information PendingISS Expedition Duration
April 2006 - September 2006Expeditions Assigned
13Previous ISS Missions
Performance of thermodynamic analysis and assessment of the technical characteristics of the capillary evaporator. Assessment of proposed technologies of evaporators for future application in space conditions.
Information PendingEarth Applications
Information PendingOperational Protocols
Capillary evaporator test performance aboard the ISS RS. The experimental equipment is a monoblock and consists of a capillary evaporator configured as a circuit (CPL1) and an electronic control unit. The capillary evaporator design uses a two-phase heat transfer loop, which is used to support satellite thermal control. The loop consists of an evaporator, cooler and reservoir connected by pipes. The heat generated in the evaporator is transferred by working fluid to the cooler section. The reservoir supports the temperature inside the loop and the required reserves of working fluid. The fans provide cooling of the capacitor. The electronic unit consists of a computer with a single-board microprocessor for data acquisition and regulation of the capillary evaporator power, as well as for setting an operating temperature in the reservoir. Water in amount of 20 ml will be used as a coolant.
Information on the capillary evaporator operation recorded on the memory map.