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Lockheed design of a wind satellite (WINDSAT) experimentWINDSAT is a proposed space based global wind measuring system. A Shuttleborne experiment is proposed as a proof of principle demonstration before development of a full operational system. WINDSAT goals are to measure wind speed and direction to + or - 1 m/s and 10 deg accuracy over the entire earth from 0 to 20 km altitude with 1 km altitude resolution. The wind measuring instrument is a coherent lidar incorporating a pulsed CO2 TEA laser transmitter and a continuously scanning 1.25 m diameter optical system. The wind speed is measured by heterodyne detecting the backscattered return laser radiation and measuring this frequency shift.
Document ID
19930072885
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Osmundson, John S.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Martin, Stephen C.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1985
Publication Information
Publication: NASA. Goddard Space Flight Center, Proceedings of the NASA Symposium on Global Wind Measurements
Subject Category
Meteorology And Climatology
Accession Number
93N70332
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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