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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Cryocooler Coldfinger Heat Interceptor


    Contributors:

    Publication date :

    1994-06-01


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English




    Cryocooler Coldfinger Heat Interceptor

    Johnson, D. / Ross, R., Jr. | NTRS | 1994


    Cryocooler Coldfinger Heat Interceptor

    Johnson, D. L. / Ross, R. G. | British Library Conference Proceedings | 1995


    Cryocooler Heat Interceptor Test for the SMTS Program

    Gilman, D. C. | British Library Conference Proceedings | 1997


    Ford Interceptor

    Stevens,D. / Ford Motor,US | Automotive engineering | 2007


    Interceptor vehicles

    Johnson, A.F. | Engineering Index Backfile | 1960