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Analysis of requirements for GEOS-C laser cube-corner reflector panelsA mathematical analysis of the tradeoffs and requirements was performed to develop an improved array design which will give stronger returns at lower elevation angles and reduce pulse spread in the return. It was determined that a zenith angle of 75deg can be obtained with an array with an area of 0.28 sq m, if the array is shaped on the surface of a 45 deg cone whose axis is coincident to the satellite axis. The total weight of the truncated pyramid array with 270 cube corners is calculated to be not more than 50% greater than the GEOS 2 array, while the efficiency is increased 275%.
Document ID
19720014240
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Minott, P. O.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-65862
X-524-72-33
Report Number: NASA-TM-X-65862
Report Number: X-524-72-33
Accession Number
72N21890
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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