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The design and development of an end effector for the shuttle remote manipulator systemThe design requirements, the design, and qualification and development test problems encountered on the Remote Manipulator End Effector are described. The constraints and interfaces with the arm, the Orbiter, and the payload are identified. The design solution to meet the requirements is a unique device that provides a soft-docking feature termed capture and a hard-docking feature termed rigidization.
Document ID
19820015473
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Daniell, R. G.
(Spar Aerospace Products Ltd. Toronto Ontario, Canada)
Sachdev, S. S.
(Spar Aerospace Products Ltd. Toronto Ontario, Canada)
Date Acquired
August 10, 2013
Publication Date
May 1, 1982
Publication Information
Publication: NASA. Kennedy Space Center The 16th Aerospace Mech. Symp.
Subject Category
Space Transportation
Accession Number
82N23347
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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