Thermal control concepts for the square and the heliogyro solar sail designs under consideration for a Halley's Comet rendezvous mission are presented. The mission, involving a 1982 launch, navigation to a 0.25-AU cranking orbit about the sun in order to develop a retrograde orbit, and rendezvous with the comet in 1986, would subject surfaces of the sail vehicle to solar constant values ranging from 16 to 0.1. A highly reflective coating to produce propulsive force is needed for one surface of the sail, while the other surface requires a highly emittive coating. The problem of maintaining the sail wrinkle-free is discussed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Thermal control of a solar sail


    Beteiligte:
    Stimpson, L. D. (Autor:in) / Greenfield, M. L. (Autor:in) / Jaworski, W. (Autor:in) / Wolf, F. (Autor:in)

    Kongress:

    Thermophysics and Heat Transfer Conference ; 1978 ; Palo Alto, CA


    Erscheinungsdatum :

    1978-05-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Thermal control of a solar sail

    Stimpson, L.D. / Greenfield, M.L. / Jaworski, W. | Tema Archiv | 1978


    Thermal control of a solar sail

    STIMPSON, L. / GREENFIELD, M. / JAWORSKI, W. | AIAA | 1978


    Spacecraft solar sail processing method and solar sail

    REN ZHONGJING / LI CHENGYANG / XIE KECAI et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    SOLAR SAIL AND SOLAR SAIL SPACECRAFT USING THE SAME

    NAGAI MASATAKA | Europäisches Patentamt | 2016

    Freier Zugriff

    Solar Sail Propulsion

    Johnson, Les | NTRS | 2018