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NASA Lewis steady-state heat pipe code users manualThe NASA Lewis heat pipe code was developed to predict the performance of heat pipes in the steady state. The code can be used as a design tool on a personal computer or with a suitable calling routine, as a subroutine for a mainframe radiator code. A variety of wick structures, including a user input option, can be used. Heat pipes with multiple evaporators, condensers, and adiabatic sections in series and with wick structures that differ among sections can be modeled. Several working fluids can be chosen, including potassium, sodium, and lithium, for which monomer-dimer equilibrium is considered. The code incorporates a vapor flow algorithm that treats compressibility and axially varying heat input. This code facilitates the determination of heat pipe operating temperatures and heat pipe limits that may be encountered at the specified heat input and environment temperature. Data are input to the computer through a user-interactive input subroutine. Output, such as liquid and vapor pressures and temperatures, is printed at equally spaced axial positions along the pipe as determined by the user.
Document ID
19920019439
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Tower, Leonard K.
(Sverdrup Technology, Inc., Brook Park OH., United States)
Baker, Karl W.
(NASA Lewis Research Center Cleveland, OH, United States)
Marks, Timothy S.
(Oregon State Univ. Corvallis., United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.15:105161
NASA-TM-105161
E-6450
Report Number: NAS 1.15:105161
Report Number: NASA-TM-105161
Report Number: E-6450
Accession Number
92N28682
Funding Number(s)
PROJECT: RTOP 590-13-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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