The TacSat‐4 micro‐satellite uses an aluminum/ammonia loop heat pipe (LHP) to transport 700 W of heat from the electronics to two radiator sections. In addition to the thermal requirements, there were additional specifications for the primary and secondary wicks, and the flow balancer between the two LHP condensers. This paper discusses the experimental test rigs designed to verify the LHP performance against these requirements. The measured LHP performance at various operating conditions including start‐up, un‐balanced condenser heat removal, transient power, high power, and shut‐down is discussed.


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    Titel :

    Loop Heat Pipe for TacSat‐4


    Beteiligte:

    Kongress:

    SPACE, PROPULSION & ENERGY SCIENCES INTERNATIONAL FORUM: SPESIF‐2009 ; 2009 ; Huntsville (Alabama)


    Erschienen in:

    AIP Conference Proceedings ; 1103 , 1 ; 91-100


    Erscheinungsdatum :

    16.03.2009


    Format / Umfang :

    10 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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