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:

    Conference:

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


    Publication date :

    2015-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English