NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Liquid metal micro heat pipes for space radiator applicationsMicromachining is a chemical means of etching three-dimensional structures, typically in single-crystalline silicon. These techniques are leading toward what is coming to be referred to as MEMS (micro electro mechanical systems), where in addition to the ordinary two dimensional (planar) microelectronics, it is possible to build three-dimensional micromotors, electrically-actuated microvalves, hydraulic systems, and much more on the same microchip. These techniques become possible because of differential etching rates of various crystallographic planes and materials used for semiconductor microfabrication. The University of Cincinnati group in collaboration with NASA Lewis formed micro heat pipes in silicon by the above techniques. Work is ongoing at a modest level, but several essential bonding and packaging techniques have been recently developed. Currently, we have constructed and filled water/silicon micro heat pipes. Preliminary thermal tests of arrays of 125 micro heat pipes etched in a 1 inch x 1 inch x 250 micron silicon wafer have been completed. These pipes are instrumented with extremely small P-N junctions to measure their effective conductivity and their maximum operating power. A relatively simple one-dimensional model has been developed in order to predict micro heat pipes' operating characteristics. This information can be used to optimize micro heat pipe design with respect to length, hydraulic diameter, and number of pipes. Work is progressing on the fabrication of liquid-metal micro heat pipes. In order to be compatible with liquid metal (sodium or potassium), the inside of the micro heat pipes will be coated with a refractory metal (such as tungsten, molybdenum, or titanium).
Document ID
19960001642
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gerner, F. M.
(Cincinnati Univ. OH, United States)
Henderson, H. T.
(Cincinnati Univ. OH, United States)
Date Acquired
September 6, 2013
Publication Date
July 7, 1995
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-199122
NAS 1.26:199122
Report Number: NASA-CR-199122
Report Number: NAS 1.26:199122
Accession Number
96N11650
Funding Number(s)
CONTRACT_GRANT: NAG3-1392
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available