The Thermal Canister is a proof of concept experiment flown on the third flight of the Space Shuttle (March 1982). The canister utilizes heat pipe technology to provide a closely controlled, stable temperature environment for scientific instruments negating the effects of the harsh, variable shuttle environment. Primary objectives were to demonstrate control at 15° ± 2°C in each of the four external environments experienced by the shuttle. Secondary objectives were to control different side panels of the canister simultaneously to different temperatures in the 5° to 25°C range. The canister met all flight objectives.


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    Titel :

    The Thermal Canister: An Instrument Thermal Control System


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Intersociety Conference on Environmental Systems ; 1983



    Erscheinungsdatum :

    11.07.1983




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Instrument canister thermal control

    HARWELL, W. / HASLETT, R. / OLLENDORF, S. | AIAA | 1977


    Instrument Canister Thermal Control

    Fletcher, Leroy S. | AIAA | 1978


    Thermal-control canister

    Ollendorf, S. | NTRS | 1978


    The Heat Pipe Thermal Canister

    Crosbie, A.L. | AIAA | 1981


    The heat pipe thermal canister

    HARWELL, W. / OLLENDORF, S. | AIAA | 1980