Bibcode
Bueno, José Ignacio; Vázquez, Javier; Gavira, José Manuel; Migliorero, Gerard
Bibliographical reference
In: Proceedings of the 9th European Space Mechanisms and Tribology Symposium, 19-21 September 2001, Liège, Belgium. Compiled by R. A. Harris. ESA SP-480, Noordwijk, Netherlands: ESA Publications Division, ISBN 92-9092-761-5, 2001, p. 153 - 160
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9
2001
Citations
0
Refereed citations
0
Description
The definition of a cost effective deployment mechanism to deploy
180° panel like appendages in a safe way and with minimum end stroke
deployment shock has been a challenge that led the design to achieve a
low cost, light, compact, simple, flexible, modular, and low power
demanding configuration. This mechanism is composed of an active hinge,
that includes an optimised helical torsion spring with a deployment
regulator in parallel, and a passive hinge, that includes the end stop
and the monitorisation. The main functions of the mechanisms are
decoupled in order to make the mechanism as flexible as possible to be
adapted to very different needs such as different deployment torque,
deployment angle, stiffness, interfaces, monitorisation, etc. The
deployment mechanism is provided with a very compact novel deployment
regulator based on the progressive melting of a band made of a low
melting temperature metal alloy, that is cylindrically disposed. The
deployment mechanism has been subject to a qualification test campaign
including an extensive characterisation of the deployment regulator.