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A movable stop mechanism for the SIRE telescopeA movable stop mechanism (MSM) designed to activate flaps that change the size and shape of a telescope aperture stop on command is described. Operating at the cryogenic temperatures of the optical system, it consists primarily of a rotary solenoid that drives (activates) dual four-bar linkages in synchronism that in turn rotate the butterfly flaps into position. The design, performance characteristics, and testing of this mechanism are discussed. Specific problems that occurred during testing and the solutions that were adopted are also described.
Document ID
19820015477
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tweedt, R. E.
(Hughes Aircraft Co. El Segundo, CA, United States)
Poulsen, R. N.
(Hughes Aircraft Co. El Segundo, CA, 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
Mechanical Engineering
Accession Number
82N23351
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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