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A Mirror Transport Mechanism for Use at Cryogenic TemperaturesThis report describes the Mirror Transport Mechanism (MTM), which supports a pair of dihedral mirrors and moves them in a very smooth and uniform scanning motion normal to a beamsplitter. Each scan is followed by a quick flyback and repeat. Included in the report will be material selection, design, and testing of all major components of the MTM in order to meet the stringent performance requirements under cryogenic conditions and survive the launch environment of the shuttle. Areas to be discussed in detail will be those in which failures or performance anomalies occurred and their solutions. Typically, this will include (but not to be limited to) flex pivot failures during vibration testing, excessive dihedral platform sag under one "g" operation, electronic and fiber optic characteristics, and tolerancing considerations. As of this writing, development of the mechanism has reached the final phase of thermal and vibration qualification. Environmental testing of the complete FIRAS (Far Infrared Absolute Spectrophotometer) experiment is just beginning.
Document ID
20020073827
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Stark, Kenneth W.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Wilson, Meredith
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
August 20, 2013
Publication Date
May 1, 1986
Publication Information
Publication: 20th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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