Clamp Band Assembly for the Beagle2 lander

Details Clamp Band Assembly for the Beagle2 lander Clamp Band Assembly for the Beagle2 lander

Sep 2003

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2003esasp.524..129h&link_type=abstract

In: Proceedings of the 10th European Space Mechanisms and Tribology Symposium, 24-26 September 2003, San Sebastián, Spain. Compi

Computer Science

Astrium, Beagle2, Clamp Band, Frangi-Bolt

Scientific paper

The Beagle2 probe was launched upon the European Space Agency's (ESA's) Mars Express spacecraft in June this year, destined for the Red Planet. Beagle2 was a particularly demanding programme due to the extremely tight constraints on mass, volume, power consumption and environmental conditions. This paper describes the solution, against these constraints, for the Clamp Band and Release mechanism. The design constraints are explained, followed by a detailed design, calibration and test description of the Clamp Band Assembly (CBA).

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