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The liquid droplet radiator - An ultralightweight heat rejection system for efficient energy conversion in spaceA heat rejection system for space is described which uses a recirculating free stream of liquid droplets in place of a solid surface to radiate waste heat. By using sufficiently small droplets (less than about 100 micron diameter) of low vapor pressure liquids (tin, tin-lead-bismuth eutectics, vacuum oils) the radiating droplet sheet can be made many times lighter than the lightest solid surface radiators (heat pipes). The liquid droplet radiator (LDR) is less vulnerable to damage by micrometeoroids than solid surface radiators, and may be transported into space far more efficiently. Analyses are presented of LDR applications in thermal and photovoltaic energy conversion which indicate that fluid handling components (droplet generator, droplet collector, heat exchanger, and pump) may comprise most of the radiator system mass. Even the unoptimized models employed yield LDR system masses less than heat pipe radiator system masses, and significant improvement is expected using design approaches that incorporate fluid handling components more efficiently. Technical problems (e.g., spacecraft contamination and electrostatic deflection of droplets) unique to this method of heat rejection are discussed and solutions are suggested.
Document ID
19810062992
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mattick, A. T.
(Washington Univ. Seattle, WA, United States)
Hertzberg, A.
(Washington, University Seattle, WA, United States)
Date Acquired
August 11, 2013
Publication Date
September 1, 1981
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
IAF PAPER 81-185
Accession Number
81A47396
Funding Number(s)
CONTRACT_GRANT: NAG3-16
CONTRACT_GRANT: F04611-81-K-0400
Distribution Limits
Public
Copyright
Other

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