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Penetrator mission concepts for exploration of the Galilean satellitesPenetrators are elongated missile-shaped objects designed to implant scientific instrumentation to depths of 1 to 15 meters in a wide variety of soil. A typical penetrator weighs 35 kg and impacts the surface at 150 m/sec oriented as close as possible to vertical. A spacecraft bus carries the penetrators to the target body, controls their deployment, and serves as a data communications relay. The analysis addresses the question of basic feasibility and covers such topics as trajectory requirements and delivered mass capability, deployment modes and penetrator retro sizing, impact site accessibility, guidance and control, and penetrator/bus communications. We conclude that such missions, while difficult in many respects, appear to be technically feasible in the context of Jovian system exploration in the post-1985 time period.
Document ID
19760060111
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Friedlander, A. L.
(Planetary Science Inst. Tucson, AZ, United States)
Niehoff, J. C.
(Science Applications, Inc. Rolling Meadows, Ill., United States)
Davis, D. R.
(Planetary Science Institute Tucson, Ariz., United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1976
Subject Category
Astronautics (General)
Report/Patent Number
AIAA PAPER 76-800
Meeting Information
Meeting: Astrodynamics Conference
Location: San Diego, CA
Start Date: August 18, 1976
End Date: August 20, 1976
Sponsors: American Institute of Aeronautics and Astronautics and American Astronautical Society
Accession Number
76A43077
Funding Number(s)
CONTRACT_GRANT: NASW-2783
Distribution Limits
Public
Copyright
Other

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