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MEMS Micro-Valve for Space ApplicationsWe report on the development of a Micro-ElectroMechanical Systems (MEMS) valve that is designed to meet the rigorous performance requirements for a variety of space applications, such as micropropulsion, in-situ chemical analysis of other planets, or micro-fluidics experiments in micro-gravity. 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. We at JPL 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.
Document ID
20000052736
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
Authors
Chakraborty, I.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Tang, W. C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Bame, D. P.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Tang, T. K.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1998
Subject Category
Mechanical Engineering
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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