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MISTE flight experiment status

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dc.contributor.author Barmatz, M. B. en_US
dc.contributor.author Zhong, F. en_US
dc.contributor.author Hahn, I. en_US
dc.contributor.author Weilert, M. en_US
dc.date.accessioned 2004-09-17T07:04:50Z
dc.date.available 2004-09-17T07:04:50Z
dc.date.issued 2002-05-09 en_US
dc.identifier.citation 2002 NASA/JPL Workshop for Fundamental Physics in Space en_US
dc.identifier.citation Dana Point, CA, USA en_US
dc.identifier.clearanceno 02-1707 en_US
dc.identifier.uri http://hdl.handle.net/2014/9612
dc.description.abstract The MISTE flight experiment has made significant scientific and technical progress in preparing for a future microgravity flight. We are collaborating with several theoretical modeling groups that have developed crossover (equation-of-state) models for predicting thermodynamic behavior near the liquid-gas critical point. Several of these models have already been used to test experimental measurements of the heat capacity at constant volume, isothermal susceptibility, and coexistence curve in the crossover region near the 3He liquid-gas critical point. A brief description of these models and a representative fit to experimental data will be presented. In collaboration with Mission Research Corporation, MISTE has been testing a new small pneumatic valve for use at low temperatures. The results of recent successful low temperature actuation tests will also be discussed. en_US
dc.format.extent 2944857 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other critical phenomena liquid-gas critical point en_US
dc.title MISTE flight experiment status en_US


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