Spacecraft instruments requiring cryocoolers in their design struggle to keep overall power requirements in line with feasible solar array dimensions and launch vehicle lift capacities. Intermediate temperature (150 K to 200 K) radiators to cool radiation shields or optics on spacecraft instruments provide an as yet untapped resource for reducing the cryocooler power requirments.


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    Titel :

    Cryocooler Coldfinger Heat Interceptor


    Beteiligte:
    Johnson, D. L. (Autor:in) / Ross, R. G., Jr. (Autor:in)

    Erscheinungsdatum :

    1994-06-01


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch




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