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Placement of retroreflectors on the Lageos satelliteA model is presented for placing a large number of equal size holes in the surface of a spherical satellite. This problem differs from the classical mathematical problem of packing the maximum number of equal nonoverlapping circles on a sphere in that no hole can intersect the assembly joint at the satellite equator. The model was used during the design of Lageos to analyze the influence of the satellite diameter and hole size on the number of holes that could be placed on the satellite. The retroreflector placement pattern used in constructing Lageos was produced by the model.
Document ID
19760018219
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Moore, J. E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1976
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-TM-X-73302
Accession Number
76N25307
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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