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Ray tracing optical analysis of offset solar collector for space station solar dynamic systemOFFSET, a detailed ray tracing computer code, was developed at NASA Lewis Research Center to model the offset solar collector for the Space Station solar dynamic electric power system. This model traces rays from 50 points on the face of the Sun to 10 points on each of the 456 collector facets. The triangular facets are modeled with spherical, parabolic, or toroidal reflective surface contour and surface slope errors. The rays are then traced through the receiver aperture to the walls of the receiver. Images of the collector and of the Sun within the receiver produced by this code provide insight into the collector receiver interface. Flux distribution on the receiver walls, plotted by this code, is improved by a combination of changes to aperture location and receiver tilt angle. Power loss by spillage at the receiver aperture is computed and is considerably reduced by using toroidal facets.
Document ID
19880012696
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Jefferies, Kent S.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.15:100853
NASA-TM-100853
E-4056
Accession Number
88N22080
Funding Number(s)
PROJECT: RTOP 474-12-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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