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SPOT 4 space magnetic recorder mechanismsThe design of the SPOT 4 satellite will be quite different from the previous ones. The design of the new magnetic tape recorder, which was derived from industrial knowledge and mission requirements; the main technical characteristics of the recorder; and the mechanical subsystems of the recorder and their locations and contributions to the final performance are all discussed. The philosophy of the development program, required to achieve the desired performance and reliability for each flight model, is described, and information on the schedule and current development is presented. The components of the tape plate system, (the transmission belts, tape rollers of the recorders, and reel hub ball bearings) which are subjected to heavy mechanical operation, fatigue, and wear in the thermal environment of the mission, are discussed. For each of the components, a description of its function in the recorder is given, as well as the mechanical stress imposed during the various operational phases. The quality testing program, which was used to verify the design safety margins, is described. Finally, the first test results of a functioning model of the flight system are presented.
Document ID
19900012766
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Borrien, A.
(Centre National d'Etudes Spatiales Toulouse (France)., United States)
Vialatoux, E.
(Centre National d'Etudes Spatiales Toulouse (France)., United States)
Lhermet, J. L.
(Schlumberger Industries Velizy (France)., United States)
Didier, A.
(Schlumberger Industries Velizy, France)
Date Acquired
September 6, 2013
Publication Date
April 1, 1990
Publication Information
Publication: NASA, John F. Kennedy Space Center, The 24th Aerospace Mechanisms Symposium
Subject Category
Instrumentation And Photography
Accession Number
90N22082
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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