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Film-Evaporation MEMS Tunable Array for Picosat Propulsion and Thermal ControlThe Film-Evaporation MEMS Tunable Array (FEMTA) concept for propulsion and thermal control of picosats exploits microscale surface tension effect in conjunction with temperature- dependent vapor pressure to realize compact, tunable and low-power thermal valving system. The FEMTA is intended to be a self-contained propulsion unit requiring only a low-voltage DC power source to operate. The microfabricated thermal valving and very-high-integration level enables fast high-capacity cooling and high-resolution, low-power micropropulsion for picosats that is superior to existing smallsat micropropulsion and thermal management alternatives.
Document ID
20150016069
Acquisition Source
Ames Research Center
Document Type
Other - Brief Communication/Note
Authors
Alexeenko, Alina
(Purdue Univ. Indianapolis, IN, United States)
Cardiff, Eric
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Martinez, Andres
(NASA Ames Research Center Moffett Field, CA, United States)
Petro, Andrew
(NASA Headquarters Washington, DC United States)
Date Acquired
August 18, 2015
Publication Date
August 8, 2015
Subject Category
Spacecraft Instrumentation And Astrionics
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA FS-2015-03-31-ARC
ARC-E-DAA-TN25941
Report Number: NASA FS-2015-03-31-ARC
Report Number: ARC-E-DAA-TN25941
Funding Number(s)
CONTRACT_GRANT: NNX13AR02A
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Propulsion
Thermal control
Micro scale surface tension effect
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