Journal
SENSORS AND ACTUATORS A-PHYSICAL
Volume 83, Issue 1-3, Pages 188-193Publisher
ELSEVIER SCIENCE SA
DOI: 10.1016/S0924-4247(99)00382-9
Keywords
MEMS; valve; piezoelectric; actuator; space
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We report on the development of a micro-electro-mechanical systems (MEMS) valve that is designed to meet the rigorous performance requirements for a variety of space applications, such as micro-propulsion, in situ chemical analysis of other planets, or microbiology. These systems often require very small yet reliable silicon valves with extremely low leak rates and long shelf lives. Also, they must survive the perils of space travel, which include unstoppable radiation, monumental shock and vibration forces, as well as extreme variations in temperature. Currently, no commercial MEMS valve meets these requirements. At JPL, we are developing a piezoelectric MEMS valve that attempts to address the unique problem of space. We begin with proven configurations that may seem familiar. However, we have implemented some major design innovations that should produce a superior valve. The JPL micro-valve is expected to have an extremely low leak rate, limited susceptibility to particulates, vibration or radiation, as well as a wide operational temperature range. Published by Elsevier Science S.A. All rights reserved.
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