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Evaluation of scanning earth sensor mechanism on engineering test satellite 4The results of the analysis and the evaluation of flight data obtained from the horizon sensor test project are described. The rotary mechanism of the scanning earth sensor composed of direct drive motor and bearings using solid lubricant is operated satisfactorily. The transmitted flight data from Engineering Test Satellite IV was evaluated in comparison with the design value.
Document ID
19830016619
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ikeuchi, M. (National Space Development Agency Ibaraki, Japan)
Wakabayashi, Y. (National Space Development Agency Ibaraki, Japan)
Ohkami, Y. (National Aerospace Lab.)
Kida, T. (National Aerospace Lab.)
Ishigaki, T. (Matsushita Research Inst.)
Matsumoto, M. (Matsushita Research Inst.)
Date Acquired
August 11, 2013
Publication Date
May 1, 1983
Publication Information
Publication: JPL The 17th Aerospace Mech. Symp.
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
83N24890
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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