The paper will describe the key technical drivers on the Sylph mission concept to explore a plume at Europa as a secondary free-flyer as a part of the planned Europa Mission. Sylph is a radiation-hardened smallsat concept that would utilize terrain relative navigation to fly at low altitudes through a plume, if found, and relay the mass spectra data back through the flyby spacecraft during its 24-hour mission. The second topic to be discussed will be the mission design constraints of the Near Earth Asterioid (NEA) Scout concept. NEAScout is a 6U cubesat that would utilize an 86 sq. m solar sail as propulsion to execute a flyby with a near-Earth asteroid and help retire Strategic Knowledge Gaps for future human exploration. NEAScout would cruise for 24 months to reach and characterize one Near-Earth asteroid that is representative of Human Exploration targets and telemeter that data directly back to Earth at the end of its roughly 2.5 year mission.


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    Titel :

    Environmental Design Implications for Deep Space SmallSats


    Beteiligte:
    Kahn, Peter (Autor:in) / Imken, Travis (Autor:in) / Elliott, John (Autor:in) / Sherwood, Brent (Autor:in) / Frick, Andreas (Autor:in) / Sheldon, Douglas (Autor:in) / Lunine, Jonathan (Autor:in)

    Kongress:

    67th International Astronautical Congress (IAC) ; 2016 ; Guadalajara, Mexico


    Erscheinungsdatum :

    26.09.2016


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Environmental Design Implications for Deep Space SmallSats

    Kahn, Peter / Imken, Travis / Elliott, John et al. | NTRS | 2016