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A cryogenic scan mechanism for use in Fourier transform spectrometersThis paper describes the requirements, design, assembly and testing of the linear Scan Mechanism (SM) of the Composite Infrared Spectrometer (CIRS) Instrument. The mechanism consists of an over constrained flexible structure, an innovative moving magnet actuator, passive eddy current dampers, a Differential Eddy Current (DEC) sensor, Optical Limit Sensors (OLS), and a launch lock. Although all the components of the mechanism are discussed, the flexible structure and the magnetic components are the primary focus. Several problems encountered and solutions implemented during the development of the scan mechanism are also described.
Document ID
19950020867
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hakun, Claef F.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Blumenstock, Kenneth A.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1995
Publication Information
Publication: NASA. Johnson Space Center, The 29th Aerospace Mechanisms Symposium
Subject Category
Instrumentation And Photography
Accession Number
95N27287
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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