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:
    Genova, Anthony L. (Autor:in) / Yang Yang, Fan (Autor:in) / Perez, Andres Dono (Autor:in) / Galal, Ken F. (Autor:in) / Faber, Nicolas T. (Autor:in) / Mitchell, Scott (Autor:in) / Landin, Brett (Autor:in) / Burns, Jack O. (Autor:in)

    Kongress:

    AAS/AIAA Space Flight Mechanics Meeting ; 2015 ; Williamsburg, VA, United States


    Erscheinungsdatum :

    01.01.2015


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch