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GEOFF STURTIVANT PAPERS AND PATENTS

PAPERS

BRITISH AEROSPACE REACTION WHEELS FOR THE OLYMPUS SATELLITE
Presented at the First European Mechanisms & tribology Symposium Oct 1983, Neuchatel, Switzerland.

BRITISH AEROSPACE MECHANISMS FOR THE INTELSAT VI SATELLITE
Presented at the Second European Mechanisms & tribology Symposium Oct 1985, Meersburg, FR Germany.

RESULTS OF A 10Nms REACTION WHEEL TEST PROGRAMME
Presented at the Second European Mechanisms & tribology Symposium Oct 1985, Meersburg, FR Germany.

PATENTS

Hinge Actuator Mechanism for deployment of Satellite antennas . UK Patent Number GB2103023A (1981)

Authors
Geoffrey John Sturtivant
Karl Gallagher

Applicant
British Aerospace plc

This invention relates to damping devices in which a damping force is generated by movement of an electrically conducting member through a magnetic field which movement causes eddy currents to be induced in the member which, in turn, generate a force resisting movement of the member dependent upon its velocity. In particular, but not exclusively, this invention relates to eddy current dampers for use on spacecraft.






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