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Heat-pipe transient model for space applicationsA two-dimensional model is developed for simulating heat pipes transient performance following changes in the input/rejection power or in the evaporator/condenser temperatures. The model employs the complete form of governing equations and momentum and energy jump conditions at the liquid-vapor interface. Although the model is capable of handling both cylindrical and rectangular geometries, the results reported are for a circular heat pipe with liquid lithium as the working fluid. The model incorporates a variety of other working fluids, such as water, ammonia, potassium, sodium and mercury, and offers combinations of isothermal, isoflux, convective and radiative heating/cooling conditions in the evaporator and condenser regions of the heat pipe. Results presented are for lithium heat pipes with exponential heating of the evaporator and isothermal cooling of the condenser.
Document ID
19930029870
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tournier, Jean-Michel
(NASA Lewis Research Center Cleveland, OH, United States)
El-Genk, Mohamed S.
(New Mexico Univ. Albuquerque, United States)
Juhasz, Albert J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Publication Information
Publication: In: Space nuclear power systems; Proceedings of the 8th Symposium, Albuquerque, NM, Jan. 6-10, 1991. Pt. 2 (A93-13751 03-20)
Publisher: American Institute of Physics
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
93A13867
Funding Number(s)
CONTRACT_GRANT: NAG3-941
Distribution Limits
Public
Copyright
Other

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