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Magnetic end effectors for space operationsThe Magnetic End Effector (MEE) to be flown as part of the Dexterous End Effector (DEE) flight experiment was designed to operate with the Shuttle Remote Manipulator System (SRMS). Grappling or attachment of payloads is accomplished magnetically with two fault tolerant operations. The small magnetic grapple plate weighs far less than the standard grapple fixture; allows stacking and close spacing of payloads; and eliminates secondary release mechanisms. In addition to specifics regarding the MEE, the DEE project, Magnetic Attachment Tool (MAT), RMS-Force Torque Sensor (RMS-FTS), and Targeting and Reflective Alignment Concept (TRAC) are discussed.
Document ID
19930013102
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Monford, Leo
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Carter, Edward L.
(Lockheed Engineering and Sciences Co. Houston, TX., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NASA, Washington, NASA Automated Rendezvous and Capture Review. A Compilation of the Abstracts
Subject Category
Spacecraft Instrumentation
Accession Number
93N22291
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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