Fiscal year 1976 progress report on a feasibility study evaluating the use of surface penetrators for planetary exploration

Details Fiscal year 1976 progress report on a feasibility study evaluating the use of surface penetrators for planetary exploration Fiscal year 1976 progress report on a feasibility study evaluating the use of surface penetrators for planetary exploration

Nov 1976

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1976stin...7714969b&link_type=abstract

Unknown

Computer Science

Performance

Mars (Planet), Penetration, Planetary Quakes, Space Exploration, Geochemistry, Imaging Techniques, Planetary Meteorology, Seismic Energy, Water Management

Scientific paper

The feasibility of employing penetrators for exploring Mars was examined. Eight areas of interest for key scientific experiments were identified. These include: seismic activity, imaging, geochemistry, water measurement, heatflow, meteorology, magnetometry, and biochemistry. In seven of the eight potential experiment categories this year's progress included: conceptual design, instrument fabrication, instrument performance evaluation, and shock loading of important components. Most of the components survived deceleration testing with negligible performance changes. Components intended to be placed inside the penetrator forebody were tested up to 3,500 g and components intended to be placed on the afterbody were tested up to 21,000 g. A field test program was conducted using tentative Mars penetrator mission constraints. Drop tests were performed at two selected terrestrial analog sites to determine the range of penetration depths for anticipated common Martian materials. Minimum penetration occurred in basalt at Amboy, California. Three full-scale penetrators penetrated 0.4 to 0.9 m into the basalt after passing through 0.3 to 0.5 m of alluvial overburden. Maximum penetration occurred in unconsolidated sediments at McCook, Nebraska. Two full-scale penetrators penetrated 2.5 to 8.5 m of sediment. Impact occurred in two kinds of sediment: loess and layered clay. Deceleration g loads of nominally 2,000 for the forebody and 20,000 for the afterbody did not present serious design problems for potential experiments. Penetrators have successfully impacted into terrestrial analogs of the probable extremes of potential Martian sites.

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