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Design, Testing and Evaluation of Latching End EffectorThe Latching End Effector (LEE) forms part of the Space Station Remote Manipulator System (SSRMS) for which Spar Aerospace Ltd, Space Systems Division is the prime contractor. The design, testing and performance evaluation of the Latching End Effector mechanisms is the subject of this paper focusing on: (1) ambient, thermal and vibration testing; (2) snare/rigidize performance testing and interaction during payload acquisition; and (3) latch/umbilical test results and performance.
Document ID
19950020841
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
B Walker (Spar Aerospace Ltd. Brampton Ontario, Canada)
R Vandersluis (Spar Aerospace Ltd. Brampton Ontario, Canada)
Date Acquired
September 6, 2013
Publication Date
May 1, 1995
Publication Information
Publication: 29th Aerospace Mechanisms Symposium
Publisher: National Aeronautics and Space Administration
Subject Category
Mechanical Engineering
Report/Patent Number
N95-27261
NASA/CP-3293
Meeting Information
Meeting: 29th Aerospace Mechanisms Symposium
Location: League City, TX
Country: US
Start Date: May 17, 1995
End Date: May 19, 1995
Sponsors: Lockheed Missiles and Space Company (United States), National Aeronautics and Space Administration
Accession Number
95N27261
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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