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Liquid Bipropellant Microrocket Concept Under DevelopmentFundamental research into the feasibility of microrockets for primary propulsion and attitude control for far-term micro/integrated spacecraft is being performed. These rockets would be fabricated using microelectrical and mechanical systems (MEMS) technology. The enabling technology is being developed at the Massachusetts Institute of Technology (MIT). The NASA/MIT program leverages a very large Army Research Office and Defense Advanced Research Projects Agency (DARPA) program for the development of microturbine technology. The microrocket motor is complete with regenerative cooling, turbopumps, and control valves etched onto the same chip. They would be fabricated in large numbers in parallel using semiconductor manufacturing techniques. The technology may lead to the development of microsatellites as fully integrated MEMS devices that could be mass produced at a fraction of the cost of current satellites.
Document ID
20050187015
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schneider, Steven J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 23, 2013
Publication Date
April 1, 1999
Publication Information
Publication: Research and Technology 1998
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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