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NASA NTRS · 19960014921

Improvements In Ball-Screw Linear Actuators

Abstract

Report describes modifications of design of type of ball-screw linear actuator driven by dc motor, with linear-displacement feedback via linear variable-differential transformer (LVDT). Actuators used to position spacecraft engines to direct thrust. Modifications directed toward ensuring reliable and predictable operation during planned 12-year cruise and interval of hard use at end of cruise.

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BibTeXRIS

Iskenderian, Theodore, Joffe, Benjamin, Summers, Robert. 1996-01-01. Improvements In Ball-Screw Linear Actuators. https://ntrs.nasa.gov/citations/19960014921

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