Assessment of the Technical Characteristics of a Capillary Evaporator in Microgravity (Cemex) - 07.29.14

Overview | Description | Applications | Operations | Results | Publications | Imagery
ISS Science for Everyone

Science Objectives for Everyone
CEM will test two capillary evaporators, the main part of the two-phase heat transfer loops used for thermal control in spacecraft.

Science Results for Everyone
Information Pending

This content was provided by A. V. Markov, and is maintained in a database by the ISS Program Science Office.

Experiment Details


Principal Investigator(s)

  • A. V. Markov, S.P. Korolev RSC Energia, Russia

  • Co-Investigator(s)/Collaborator(s)
    Information Pending
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    Sponsoring Space Agency
    Russian Federal Space Agency (Roscosmos)

    Sponsoring Organization
    Information Pending

    Research Benefits
    Information Pending

    ISS Expedition Duration
    April 2006 - September 2006

    Expeditions Assigned

    Previous ISS Missions
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    Experiment Description

    Research Overview
    Information Pending

    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.

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    Space Applications
    Information Pending

    Earth Applications
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    Operational Requirements
    Information Pending

    Operational 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.

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    Results/More Information
    Information on the capillary evaporator operation recorded on the memory map.

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    Related Websites
    Energia - Science Research on the ISS Russian Segment

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    image Kit with CEM equipment consisting of the CPL block and Memory map CEM* (in cover). Image courtesy of Russian Space Agency (FSA).
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