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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    Title :

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


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

    Publication date :

    2015


    Size :

    15 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English