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Medium Earth Orbit Scatterometer (MEOScat) Concept Phase StudyIn this report, advanced scatterometer concept options to operate in the post-SeaWinds era are examined. In order to meet the future requirements of scientific and operational users, a variety of scatterometer systems capable of producing improved wind vector products are evaluated. Special emphasis is placed on addressing concept options that operate at higher altitudes in order to improve the temporal revisit time. A preliminary set of generalized wind measurement goals designed to meet the future needs of both scientific and operational communities is put forth. Geophysically based measurement constraints (such as allowable carrier frequencies and measurement incidence angles) are identified. It was found that a potential key constraint at higher satellite altitudes is the longer time required to make all of the azimuth measurements. The revisit and coverage characteristics of a variety of platform orbits throughout the MEO range is studied in detail, and a discussion of the associated increase in radiation is presented. The "trade space" of scatterometer architectures and design options, along with associated advantages and disadvantages, is described for mission options in the MEO range. Finally, key technology studies that will enable further development of a MEO scatterometer mission are identified.
Document ID
20050185549
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
Authors
Spencer, Michael W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 7, 2013
Publication Date
April 14, 2004
Subject Category
Instrumentation And Photography
Report/Patent Number
JPL-Publ-04-7
Funding Number(s)
CONTRACT_GRANT: NAS7-03001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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