The Hipparcos payload thermal control is presented. It ensures the active and passive thermal control with a temperature stability better than 0.05C over short periods, and about 2C over the entire mission duration. The payload structure, manufactured from carbon fiber reinforced plastic, is described. The principles of the active thermal control system are indicated, and its characteristics are listed.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Payload Thermal Control


    Contributors:
    E. Jaekel (author)

    Publication date :

    1989


    Size :

    3 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    ISS Payload Thermal Environments

    Carrillo L. / Farner D. / Preston C. | NTIS | 2015


    Planck Payload Thermal Design

    Cornut, M. / Riti, J.-B. / Hauser, A. et al. | British Library Conference Proceedings | 2000


    ISS Payload Thermal Environments

    Carrillo, Laurie / Farner, David / Preston, Caryn | NTRS | 2015


    Planck Payload Thermal Design

    Hauser, Armin / Collaudin, Bernard / Riti, Jean-Bernard et al. | SAE Technical Papers | 2000


    Polar Platform Payload Equipment Bay Thermal Control Aspects

    Cataloglu, A. / Pieper, B. / Argles, P. | SAE Technical Papers | 1994