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NASA NTRS ยท 19830016622

Cannon launched electromechanical control actuation system development

Abstract

The 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.

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BibTeXRIS

Johnston, J. G.. 1983-05-01. Cannon launched electromechanical control actuation system development. https://ntrs.nasa.gov/citations/19830016622

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