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Cannon launched electromechanical control actuation system developmentThe evolution of an electromechanical control actuation system from trade study results through breadboard test and high-g launch demonstration tests is summarized. Primary emphasis is on design, development, integration and test of the gear reduction system.
Document ID
19830016622
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Johnston, J. G. (Martin Marietta Aerospace Orlando, FL, United States)
Date Acquired
August 11, 2013
Publication Date
May 1, 1983
Publication Information
Publication: JPL The 17th Aerospace Mech. Symp.
Subject Category
Structural Mechanics
Accession Number
83N24893
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19830016610Collected WorksThe 17th Aerospace Mechanisms Symposium
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