The Thermal Control Subsystem engineers task is to maintain the temperature of all spacecraft components, subsystems, and the total flight system within specified limits for all flight modes from launch to end-of-mission. In some cases, specific stability and gradient temperature limits will be imposed on flight system elements. The Thermal Control Subsystem of "normal" flight systems, the mass, power, control, and sensing systems mass and power requirements are below 10% of the total flight system resources. In general the thermal control subsystem engineer is involved in all other flight subsystem designs.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Spacecraft Design Thermal Control Subsystem


    Beteiligte:

    Kongress:

    Presentation at University of Michigan, Ann Arbor, Michigan, January 31, 2008 ; 2008 ; Ann Arbor, MI, United States


    Erscheinungsdatum :

    2008-01-31


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Spacecraft Design Thermal Control Subsystem

    Miyake, Robert N. | NTRS | 2003


    Design of Spacecraft Thermal Control Subsystem

    Miao, Jianyin / Zhong, Qi / Zhao, Qiwei et al. | Springer Verlag | 2020


    Spacecraft active thermal control subsystem design and operation considerations

    SADUNAS, J. / LEHTINEN, A. / NGUYEN, H. et al. | AIAA | 1986


    Stochastic Approach to Spacecraft Thermal Control Subsystem

    Sepúlveda, Alejandro Torres / Herrera, Félix Lamela | SAE Technical Papers | 2000


    Spacecraft Subsystem Reliability

    Saleh, Joseph Homer / Castet, Jean‐François | Wiley | 2011