One embodiment includes a contamination limiter for a spacecraft. The contamination limiter includes a body (101) having an interior. An inlet (104) is fluidly coupled to the interior of the body. A collector plate (120) is positioned within the interior of the body. A UV light source (110) is directed at a surface of the collector plate (120). An exterior vent (102) is fluidly coupled to the interior of the body. A volatile condensable material from the spacecraft is photofixed by the UV light exposure to the collector plate prior to venting through an exterior vent to an exterior of the spacecraft.


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    Titel :

    CONTAMINATION LIMITER FOR REDUCING OUTGASSED VOLATILE CONDENSABLE MATERIALS FROM EXTERNAL SENSITIVE OPTICAL AND THERMAL SURFACES OF A SPACECRAFT


    Weitere Titelangaben:

    KONTAMINATIONSBEGRENZER ZUR VERRINGERUNG VON AUSGEGASTEN FLÜCHTIGEN KONDENSIERBAREN STOFFEN AUS EXTERNEN EMPFINDLICHEN OPTISCHEN UND THERMISCHEN OBERFLÄCHEN EINES RAUMFAHRZEUGES
    LIMITEUR DE CONTAMINATION POUR RÉDUIRE DES MATÉRIAUX CONDENSABLES VOLATILS DÉGAZÉS À PARTIR DE SURFACES OPTIQUES ET THERMIQUES SENSIBLES EXTERNES D'UN ENGIN SPATIAL


    Beteiligte:
    PANG ANTHONY (Autor:in) / XIE JULIE (Autor:in) / LONTOC ELEAZAR P (Autor:in)

    Erscheinungsdatum :

    2024-03-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F24F Klimatisierung , AIR-CONDITIONING



    Contamination limiter for reducing outgassed volatile condensable materials from spacecraft

    PANG ANTHONY / XIE JULIE / LONTOC ELEAZAR P | Europäisches Patentamt | 2020

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