High performances imaging systems for planetary landers

Details High performances imaging systems for planetary landers High performances imaging systems for planetary landers

Apr 2003

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2003eaeja....14343j&link_type=abstract

EGS - AGU - EUG Joint Assembly, Abstracts from the meeting held in Nice, France, 6 - 11 April 2003, abstract #14343

Computer Science

Performance

Scientific paper

Each planetary mission brings its specific needs and environmental conditions: high temperature and radiations for Mercury, shock, thermal cycles and low temperature operation for Mars, long vacuum cruise phase and very low temperature for comet nucleus. Nevertheless, all the missions share the same interests in term of low mass, low power and harsh environmental conditions. When a mission includes a lander, mass optimization is even more critical for the benefit of the overall science return. SPACE-X has developed high-performances imaging systems for Rosetta Lander and MarsExpress Lander. Future imaging systems for new exploration missions have to consider the promising micro-nano-technology developments in terms of miniaturisation, low power, wireless capabilities, etc.

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