Description of design principles of thermocontrol system for small subsatellites Magion- 4, 5 and thermal behavior during two years of flight exploitation are presented. Passive type of thermocontrol system is intended to support the temperature level (-10…50) °C in inner volume of equipment compartment at solar subsatellite orientation and in temporary Earth shadow. Heat energy balance of the object at required temperature range is provided by utilization of radiating surfaces with defined areas, by thermal coupling of hot and cold subsatellite parts and by adaptation of constructive subsatellite elements to solve thermal tasks. Survey of telemetric date concerns temperature state of the main major parts of satellite are under consideration as well.


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    Titel :

    Magion-4 Satellite Thermal Status -2 Years Flight Operation


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Vojta, J. (Autor:in) / Grechina, N. (Autor:in) / Zhuk, S. (Autor:in) / Baturkin, V. (Autor:in) / Khrapchenkov, V. (Autor:in) / Agafonov, Y. (Autor:in)

    Kongress:

    International Conference On Environmental Systems ; 1998



    Erscheinungsdatum :

    13.07.1998




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Magion-4 Satellite Thermal Status-2 Years Flight Operation

    Vojta, J. / Zhuk, S. / Baturkin, V. et al. | British Library Conference Proceedings | 1998


    Design and construction of the Magion satellite

    Plichta, J. | Tema Archiv | 1980


    MAGION Small Spacecraft as a Tool for Flight Dynamics Learning

    Khrapchenkov, V. / Pivovarov, M. / Eismont, N. et al. | British Library Conference Proceedings | 1996


    AOC of Magion Spacecraft as a Sub-Satellite in Interball Mission

    Eismont, N. | British Library Online Contents | 1996


    AOC of Magion Spacecraft as a Sub-Satellite in Interball Mission

    Eismont, N. / European Space Agency / German Aerospace Establishment (DLR) | British Library Conference Proceedings | 1996