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Buoyant station mission comcepts for titan explorationAn advanced mission to this unique satellite of Saturn appropriate to the turn-of-the-century time period is described. The mission concept evolves about one or more buoyant stations (balloons and/or airship) operating at varying altitudes in Titan's atmosphere. An orbiter of Titan provides communications link support and accomplishes remote sensing science objectives. Use of buoyant stations are favored over a fixed site lander for two reasons: (1) adaptable to several possible surface physical states and topographies; and (2) capable of exploring both the atmosphere and surface with regional and possibly global mobility. Auxiliary payload concepts investigated include tethered packages and sounding rockets deployed from the buoyant station, and haze probes and surface penetrators deployed from the orbiter. The paper describes science objectives and payloads, propulsion system/mass delivery trades, balloon design requirements and deployment/motion characteristics, and communications link geometry and data characteristics.
Document ID
19860031153
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Friedlander, A. L.
(Science Applications International Corp. Schaumburg, IL, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1985
Subject Category
Lunar And Planetary Exploration
Report/Patent Number
IAF PAPER 85-417
Accession Number
86A15891
Funding Number(s)
CONTRACT_GRANT: NASW-3622
Distribution Limits
Public
Copyright
Other

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