The trajectory design for the Dark Ages Radio Explorer (DARE) mission concept involves launching the DARE spacecraft into a geosynchronous transfer orbit (GTO) as a secondary payload. From GTO, the spacecraft then transfers to a lunar orbit that is stable (i.e., no station-keeping maneuvers are required with minimum perilune altitude always above 40 km) and allows for more than 1,000 cumulative hours for science measurements in the radio-quiet region located on the lunar farside.


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    Titel :

    Trajectory Design from GTO to Near-Equatorial Lunar Orbit for the Dark Ages Radio Explorer (DARE) Spacecraft


    Beteiligte:
    A. L. Genova (Autor:in) / F. Yang Yang (Autor:in) / A. D. Perez (Autor:in) / K. F. Galal (Autor:in) / N. T. Faber (Autor:in) / S. Mitchell (Autor:in) / B. Landin (Autor:in) / J. O. Burns (Autor:in)

    Erscheinungsdatum :

    2015


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch