Mathematics – Logic
Scientific paper
Dec 1991
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991esasp.328...51b&link_type=abstract
In ESA, Radars and Lidars in Earth and Planetary Sciences p 51-58 (SEE N92-25668 16-32)
Mathematics
Logic
Electromagnetism, Geological Surveys, Mars (Planet), Phase Shift Keying, Radar Geology, Radar Measurement, Topology, Airships, Ground Tests, Mars Craters, Mars Volcanoes, Radar Detection, Radar Equipment, Systems Engineering
Scientific paper
The Mars 96 International Scientific Mission to launch an aerostat that will drift in the Martian atmosphere for ten days is described. The stabilizing element of the aerostat (guiderope) will be dragged on the Martian surface every night. A ground penetrating radar will be installed within the guiderope. Its external surface will act as a transmit and receive antenna. A full scale model was built and tested on different soils and glaciers. Further experiments will be performed to test the full specifications. Radar potential and data processing could yield a penetrating depth down to 2.5 km with 30 m resolution on Mars. The main technical features of the radar are described. Its implementation into the guiderope is discussed. Some experimental results are presented.
Barbin Y.
Elkine M.
Finkelstein M.
Glotov V.
Kofman Wlodek
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