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Surface penetrators for planetary exploration: Science rationale and development programWork on penetrators for planetary exploration is summarized. In particular, potential missions, including those to Mars, Mercury, the Galilean satellites, comets, and asteroids are described. A baseline penetrator design for the Mars mission is included, as well as potential instruments and their status in development. Penetration tests in soft soil and basalt to study material eroded from the penetrator; changes in the structure, composition, and physical properties of the impacted soil; seismic coupling; and penetrator deflection caused by impacting rocks, are described. Results of subsystem studies and tests are given for design of entry decelerators, high-g components, thermal control, data acquisition, and umbilical cable deployment.
Document ID
19810012471
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Murphy, J. P.
(NASA Ames Research Center Moffett Field, CA, United States)
Reynolds, R. T.
(NASA Ames Research Center Moffett Field, CA, United States)
Blanchard, M. B.
(NASA Ames Research Center Moffett Field, CA, United States)
Clanton, U. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1981
Subject Category
Lunar And Planetary Exploration
Report/Patent Number
NASA-TM-81251
A-8412
Accession Number
81N21000
Funding Number(s)
PROJECT: RTOP 186-68-76-07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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