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A robot end effector exchange mechanism for space applicationsEfficient robot operation requires the use of specialized end effectors or tools for tasks. In spacecraft applications, the microgravity environment precludes the use of gravitational forces to retain the tools in holding fixture. As a result of this, a retention mechanism which forms a part of the tool storage container is required. A unique approach to this problem has resulted in the development of an end effector exchange mechanism that meets the requirements for spaceflight applications while avoiding the complexity usually involved. This mechanism uses multiple latching cams both on the manipulator and in the tool storage container, combined with a system of catch rings to provide retention in both locations and the required failure tolerance. Because of the cam configuration the mechanism operates passively, requiring no electrical commands except those needed to move the manipulator into position. Similarly, it inherently provides interlocks to prevent the release of one cam before its opposite number is engaged.
Document ID
19900012772
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gorin, Barney F.
(Fairchild Space Co. Germantown, MD, United States)
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
Mechanical Engineering
Accession Number
90N22088
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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