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A core handling device for the Mars Sample Return MissionA core handling device for use on Mars is being designed. To provide a context for the design study, it was assumed that a Mars Rover/Sample Return (MRSR) Mission would have the following characteristics: a year or more in length; visits by the rover to 50 or more sites; 100 or more meter-long cores being drilled by the rover; and the capability of returning about 5 kg of Mars regolith to Earth. These characteristics lead to the belief that in order to bring back a variegated set of samples that can address the range of scientific objetives for a MRSR mission to Mars there needs to be considerable analysis done on board the rover. Furthermore, the discrepancy between the amount of sample gathered and the amount to be returned suggests that there needs to be some method of choosing the optimal set of samples. This type of analysis will require pristine material-unaltered by the drilling process. Since the core drill thermally and mechanically alters the outer diameter (about 10 pct) of the core sample, this outer area cannot be used. The primary function of the core handling device is to extract subsamples from the core and to position these subsamples, and the core itself if needed, with respect to the various analytical instruments that can be used to perform these analyses.
Document ID
19890016981
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gwynne, Owen (Wisconsin Univ. Madison, WI, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1989
Publication Information
Publication: NASA, Ames Research Center, Exobiology and Future Mars Missions
Subject Category
Lunar And Planetary Exploration
Accession Number
89N26352
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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