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Compact sensitive piezoelectric mass balance for measurement of unconsolidated materials in space

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dc.contributor.author Sherrit, Stewart
dc.contributor.author Trebi-Ollennu, Ashitey
dc.contributor.author Bonitz, Robert
dc.contributor.author Bar-Cohen, Yoseph
dc.contributor.author Yen, Jesse T.
dc.date.accessioned 2014-09-26T21:41:32Z
dc.date.available 2014-09-26T21:41:32Z
dc.date.issued 2010-03-07
dc.identifier.citation 12th SPIE Conference - Electroactive Polymer Actuators and Devices(EAPAD), San Diego, California, March 7-11, 2010 en_US
dc.identifier.clearanceno 10-0505
dc.identifier.uri http://hdl.handle.net/2014/44788
dc.description.abstract In many in-situ instruments information about the mass of the sample could aid in the interpretation of the data and portioning instruments might require an accurate sizing of the sample mass before dispensing the sample. In addition, on potential sample return missions a method to directly assess the captured sample size would be required to determine if the sampler could return or needs to continue attempting to acquire sample. In an effort to meet these requirements piezoelectric balances were developed using flextensional actuators which are capable of monitoring the mass using two methods. A piezoelectric balance could be used to measure mass directly by monitoring the voltage developed across the piezoelectric which is linear with force, or it could be used in resonance to produce a frequency change proportional to the mass change. In this case of the latter, the piezoelectric actuator/balance would be swept in frequency through its fundamental resonance. If a mass is added to the balance the resonance frequency would shift down proportionally to the mass. By monitoring the frequency shift the mass could be determined. This design would allow for two independent measurements of the mass. In microgravity environments spacecraft thrusters could be used to provide acceleration in order to produce the required force for the first technique or to bring the mass into contact with the balance in the second approach. In addition, the measuring actuators, if driven at higher voltages, could be used to fluidize the powder to aid sample movement. In this paper, we outline some of our design considerations and present the results of a few prototype balances that we have developed. en_US
dc.description.sponsorship NASA/JPL en_US
dc.language.iso en_US en_US
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2010 en_US
dc.subject resonance en_US
dc.subject flextensional actuators en_US
dc.title Compact sensitive piezoelectric mass balance for measurement of unconsolidated materials in space en_US
dc.type Preprint en_US


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