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| Contact |
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Bidaux Jacques-Eric |
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| Title |
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Development and testing of a Bi-stable Actuator based on a High Transition Temperatures Shape Memory Alloy |
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Paciotti G., Bidaux J.-E., Girard H., Rottmeier F., Blecha L. |
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| References |
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Proc. of the 43rd Aerospace Mechanisms Symposium, NASA Ames Research Center, Santa Clara, CA, May 4-6, 2016, pp. 453-464 |
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| Abstract |
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Pyrovalves i.e. valves actuated by a pyrotechnical device are very often used in space propulsion systems for their fast response, high reliability, low mass and low cost. However they are hazardous and single use items. Their operation induces shocks and can generate contaminants. In case a slower actuation is required or possible, shape memory based actuators allow to avoid the generation of shocks and contaminants while being fully resettable and non hazardous devices.
The goal of this project was to develop a bi-stable Shape Memory Alloy (SMA) actuator for a specific Slow Acting Latch Valve, with long life capability. The benefits of this actuator makes it interesting not only for valves actuation but also for any device that has to be actuated in a smooth and reliable way.
This paper presents the development of a bi-stable actuator based on high temperature shape memory alloys. |
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