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Satellite thermal modeling using the illuminographic cameraThe application is discussed of illuminographic camera techniques to the measurement of radiative form factors for satellite modeling applications. The equation for the illuminographic mirror is derived, and the advantages of the method are discussed. Proximity error for the illuminographic mirror is defined, and estimates of this error as a function of the scale factor of the model are given, together with a method for halving this error. Designs for illuminographic mirrors are presented: the first provides a further threefold reduction in proximity error; the second permits the estimation of thermal radiation transfer coefficients to interior regions of otherwise inaccessible volumes. Finally, reflex Polaroid camera techniques appropriate to the relatively small size of the illuminographic mirror are described.
Document ID
19760004055
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wiesner, S. J.
(Stanford Univ. Palo Alto, CA, United States)
Howland, B.
(MIT)
Nathanson, D. M.
(MIT)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: NASA. Goddard Space Flight Center 8th Conf. on Space Simulation
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
PAPER-31
Accession Number
76N11143
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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