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Entry and Landing Probe for TitanResults of a recent study of entry and landing probes for the exploration of Titan are presented. The probes considered were based on a wide range of exploration mission possibilities. They included: an atmospheric science probe, an intermediate atmospheric and limited surface science probe, and a larger atmospheric and expanded surface science probe. Because of lower gravity on Titan and its atmospheric characteristics, the entry environment is less severe than that of Mars. However, the large uncertainties in the current definition of the atmosphere and the uncertainties in Titan's surface characteristics have required tradeoffs of various combinations of entry and descent shapes and hard lander configurations. Results show that all probe classes are feasible without major developments.
Document ID
19980033937
Acquisition Source
Ames Research Center
Document Type
Reprint (Version printed in journal)
Authors
Murphy, J. P.
(NASA Ames Research Center Moffett Field, CA United States)
Cuzzi, J. N.
(NASA Ames Research Center Moffett Field, CA United States)
Butts, A. J.
(Martin Marietta Aerospace Denver, CO United States)
Carroll, P. C.
(Martin Marietta Aerospace Denver, CO United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1981
Publication Information
Publication: Journal of Spacecraft and Rockets
Publisher: American Inst. of Aeronautics and Astronautics
Volume: 18
Issue: 2
Subject Category
Administration And Management
Report/Patent Number
NASA/TM-81-207535
NAS 1.15:207535
AIAA Paper 80-0117
Report Number: NASA/TM-81-207535
Report Number: NAS 1.15:207535
Report Number: AIAA Paper 80-0117
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Pasadena, CA
Country: United States
Start Date: January 14, 1980
End Date: January 16, 1980
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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