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Advanced Concepts Liquid Droplet RadiatorAn exploratory point design study was carried out on a shuttle-launchable megawatt nuclear orbit transfer vehicle (OTV) with a 5000 kg payload capacity. The system, which consists of a fixed bed reactor, a Brayton cycle power conversion system, and a liquid droplet radiator (LDR) to reject heat, is deployable from a small package. The methods and technologies of this design are discussed, as well as critical design problems. While this is a preliminary study, it indicates that a space-nuclear reactor, combined with the LDR, make possible a continuous 10 MW(e) power station on orbit with a single shuttle launch.
Document ID
19850005590
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
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
85N13899
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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