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A Comparison of Platforms for the Aerial Exploration of TitanExploration of Titan, envisioned as a follow-on to the highly successful Cassini-Huygens mission, is described in this paper. A mission blending measurements from a dedicated orbiter and an in-situ aerial explorer is discussed. Summary description of the science rationale and the mission architecture, including the orbiter, is provided. The mission has been sized to ensure it can be accommodated on an existing expendable heavy-lift launch vehicle. A launch to Titan in 2018 with a 6-year time of flight to Titan using a combination of Solar Electric Propulsion and aeroassist (direct entry and aerocapture) forms the basic mission architecture. A detailed assessment of different platforms for aerial exploration of Titan has been performed. A rationale for the selection of the airship as the baseline platform is provided. Detailed description of the airship, its subsystems, and its operational strategies are provided.
Document ID
20050237895
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Wright, Henry S.
(NASA Langley Research Center Hampton, VA, United States)
Gasbarre, Joseph F.
(NASA Langley Research Center Hampton, VA, United States)
Levine, Joel S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
AIAA Paper 2005-7155
Report Number: AIAA Paper 2005-7155
Funding Number(s)
OTHER: 23-732-50-20
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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