Mechanisms for the Beagle2 lander

Details Mechanisms for the Beagle2 lander Mechanisms for the Beagle2 lander

Sep 2001

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2001esasp.480...25p&link_type=abstract

In: Proceedings of the 9th European Space Mechanisms and Tribology Symposium, 19-21 September 2001, Liège, Belgium. Compiled by

Computer Science

Astrium, Beagle2, Mechanisms

Scientific paper

The Beagle2 program is particularly demanding due to the extremely tight constraints on mass, volume, power consumption and environmental conditions. This paper describes the solutions, against these constraints, for three of the key mechanisms within the lander. These are the instrument arm, the main hinge mechanism and the solar array hinge mechanisms. The design constraints for each are explained, followed by a detailed description for each of the mechanism types.

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