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Self Indexing Latch SystemA self-latching jaw assembly is described which includes a pair of jaws for latching a fitting of an associated structure such as the keel fitting of a space telescope. The jaw assembly automatically locates the fitting received on a positioning pedestal and latches it in its original location on the pedestal without need of precision alignment. The first jaw is actuated and moved to the right whereupon a reciprocating plunger, extended from the nose of the jaw senses the hub of the spool. A jaw position responsive switch is then actuated to terminate the drive motor of the jaw. The astronaut will then actuate the drive motor of the jaw and the jaw will move to the left, whereupon the standoff will engage the face of the jaw in a latching position. In the latching position, the noses of the jaws will be under the flanges of the spool.
Document ID
19870011900
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Patent
External Source(s)
MFS-25956-1
Authors
John C Gibson
(Marshall Space Flight Center Redstone Arsenal, United States)
John A Calvert
(Marshall Space Flight Center Redstone Arsenal, United States)
Malcolm F Nesmith
(Marshall Space Flight Center Redstone Arsenal, United States)
Richard A Cloyd
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
August 13, 2013
Publication Date
April 15, 1986
Publication Information
Publisher: United States Patent and Trademark Office
Subject Category
Mechanical Engineering
Accession Number
87N21333
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,582,289
Patent Application
US-PATENT-APPL-SN-580397
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