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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 ( 100 micron diameter) of low vapor pressure liquids 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 rejectioon are discussed and solutions are suggested.
Document ID
19850005591
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mattick, A. T.
(Washington Univ. Seattle, WA, United States)
Hertzberg, A.
(Washington Univ. Seattle, WA, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1984
Publication Information
Publication: NASA. Lewis Research Center Space Power
Subject Category
Spacecraft Propulsion And Power
Accession Number
85N13900
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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