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Centerline latch tool for contingency orbiter door closureThe centerline latch tool was designed and developed as an EVA manual backup device for latching the Space Shuttle Orbiter's payload bay doors for reentry in case of a failure of the existing centerline latches to operate properly. The tool was designed to satisfy a wide variety of structural, mechanical, and EVA requirements. It provides a load path for forces on the payload bay doors during reentry. Since the tool would be used by an EVA crewmember, control, handgrips, operating forces, and procedures must be within the capabilities of a partially restrained, suited crewmember in a zero-gravity environment. The centerline latch tool described was designed, developed, and tested to meet these requirements.
Document ID
19820015474
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Trevino, R. C.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
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
82N23348
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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