PROBLEM TO BE SOLVED: To provide improved thermal control systems that make a spacecraft more thermally efficient.SOLUTION: Systems, methods and apparatus for dual condenser loop heat pipes for satellites with sun-normal radiators comprise: heating a liquid in an evaporator in order to convert the liquid to a vapor; passively circulating the vapor within tubing from the evaporator to a first radiator not illuminated by the sun and to a second radiator illuminated by the sun; converting the vapor to the liquid when the vapor is within the first radiator not illuminated by the sun; and passively circulating the liquid within the tubing from the first radiator not illuminated by the sun to the evaporator.SELECTED DRAWING: Figure 3A

    【課題】宇宙船の熱効率が向上する、改良された熱制御システムを提供する。【解決手段】太陽に垂直のラジエータを有する衛星向けのデュアルコンデンサループヒートパイプのためのシステム、方法、及び装置において、蒸発器内で液体を蒸気に転化させるために、液体を加熱すること更に、蒸気を管組織内で、蒸発器から太陽に照らされない第1のラジエータへ、及び太陽に照らされる第2のラジエータへ受動的に循環させ、蒸気が太陽に照らされない第1のラジエータ内にあるときに、蒸気を液体に転化させることを含む。更に、液体を管組織内で、太陽に照らされない第1のラジエータから蒸発器へ受動的に循環させることを含む。【選択図】図3A


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    Title :

    DUAL CONDENSER LOOP HEAT PIPE FOR SATELLITES WITH SUN-NORMAL RADIATORS


    Additional title:

    太陽に垂直のラジエータを有する衛星向けのデュアルコンデンサループヒートパイプ


    Contributors:

    Publication date :

    2018-10-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F28D Wärmetauscher, soweit in keiner anderen Unterklasse vorgesehen, in denen die Wärmetauschmittel nicht in direkte Berührung miteinander kommen , HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT



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