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Driving and latching of the Starlab pointing mirror doorsThe Starlab Experiment, a major SDIO technology initiative, is an attached payload which will be delivered into Earth orbit aboard NASA's Space Shuttle in 1991. Starlab will generate and aim an 80 cm diameter laser beam into space through a large opening in the structure which houses the pointing mirror. Two doors, each somewhat larger than a desktop, cover the opening when the laser optics system is nonoperational. Latch Mechanism Assemblies hold the doors shut during liftoff and ascent and, again, during Orbiter reentry. Each door is powered by a Door Drive System during the many open/close cycles between various experiments. The design, testing, and resultant failure modes of these mechanisms are examined.
Document ID
19900012777
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Beaven, Herbert R., Jr.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Avina, Raymond R.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1990
Publication Information
Publication: NASA, John F. Kennedy Space Center, The 24th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Accession Number
90N22093
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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