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.
Environmental Design Implications for Deep Space SmallSats
67th International Astronautical Congress (IAC) ; 2016 ; Guadalajara, Mexico
26.09.2016
Aufsatz (Konferenz)
Keine Angabe
Englisch
Environmental design implications for two deep space SmallSats
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|SmallSats Supporting Deep Space Human Exploration
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|Space Launch System: Deep-Space Deployment for SmallSats
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