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Spherically Actuated MotorA three degree of freedom (DOF) spherical actuator is proposed that will replace functions requiring three single DOF actuators in robotic manipulators providing space and weight savings while reducing the overall failure rate. Exploration satellites, Space Station payload manipulators, and rovers requiring pan, tilt, and rotate movements need an actuator for each function. Not only does each actuator introduce additional failure modes and require bulky mechanical gimbals, each contains many moving parts, decreasing mean time to failure. A conventional robotic manipulator is shown in figure 1. Spherical motors perform all three actuation functions, i.e., three DOF, with only one moving part. Given a standard three actuator system whose actuators have a given failure rate compared to a spherical motor with an equal failure rate, the three actuator system is three times as likely to fail over the latter. The Jet Propulsion Laboratory reliability studies of NASA robotic spacecraft have shown that mechanical hardware/mechanism failures are more frequent and more likely to significantly affect mission success than are electronic failures. Unfortunately, previously designed spherical motors have been unable to provide the performance needed by space missions. This inadequacy is also why they are unavailable commercially. An improved patentable spherically actuated motor (SAM) is proposed to provide the performance and versatility required by NASA missions.
Document ID
20160008046
Acquisition Source
Marshall Space Flight Center
Document Type
Other
Authors
Peeples, Steven
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
June 29, 2016
Publication Date
January 1, 2015
Publication Information
Publication: George C. Marshall Space Flight Center Research and Technology Report 2014
Subject Category
General
Launch Vehicles And Launch Operations
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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