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Analysis of the Gas Particle Radiator (GPR)The theoretical performance of a new space radiator concept, the gas particle radiator (GPR), is calculated. The GPR uses a gas containing emitting, submicron particles as the radiating media. A transparent window contains the gas particle mixture around the solid radiator emitting surface. A major advantage of the GPR is that large emissivity (e sub T is greater than or = 0.8) is achieved without the use of emissive coatings. A radiation heat transfer analysis shows that for a modest volume fraction (approx. 10(-4)) of submicron particles and gas thickness (approx. 1 cm) the emissivity, e sub T, is limited by the window transmittance. Besides determining the emissivity, the window is the critical element for making it possible for the GPR to have lower mass than a tube type radiator. The window acts as a bumper to provide meteoroid protection for the radiator wall. The GPR was compared to a proposed titanium wall, potassium heat pipe radiator. For both radiators operating at a power level of 1.01 MW at 775 K it was calculated that the GPR mass was 31 percent lower than the heat pipe radiator.
Document ID
19860022180
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Chubb, D. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1986
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-2639-1
NAS 1.15:88786
NASA-TM-88786
Report Number: E-2639-1
Report Number: NAS 1.15:88786
Report Number: NASA-TM-88786
Accession Number
86N31652
Funding Number(s)
PROJECT: RTOP 506-41-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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