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Six mechanisms used on the SSM/1 radiometerFuture USAF Block 5D Defense Meteorological Satellites will carry a scanning microwave radiometer sensor (SSM/1). SSM/1 senses the emission of microwave energy and returns to earth data used to determine weather conditions, such as rainfall rates, soil moisture, and oceanic wind speed. The overall design of the SSM/1 radiometer was largely influenced by the mechanisms. The radiometer was designed to be stowed in a cavity on the existing spacecraft. The deployment of the sensor is complex due to the constraint of this cavity and the need for precision in the deployment. The radiometer will continuously rotate, instead of oscillate, creating the need for a bearing and power transfer assembly and a momentum compensation device. The six mechanisms developed for this program are described.
Document ID
19850025221
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ludwig, H. R.
(Hughes Aircraft Co. El Segundo, CA, United States)
Date Acquired
August 12, 2013
Publication Date
August 1, 1985
Publication Information
Publication: NASA. Ames Research Center 19th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
85N33534
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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