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Focus drive mechanism for the IUE scientific instrumentA compact, lightweight mechanism was developed for in-orbit adjustment of the position of the secondary mirror (focusing) of the International Ultraviolet Explored telescope. This device is a linear drive with small (.0004 in.) and highly repeatable step increments. Extremely close tolerances are also held in tilt and decentering. The unique mechanization is described with attention to the design details that contribute to positional accuracy. Lubrication, materials, thermal considerations, sealing, detenting against launch loads, and other features peculiar to flight hardware are discussed. The methods employed for mounting the low expansion quartz mirror with minimum distortion are also given.
Document ID
19790013223
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Devine, E. J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Dennis, T. B., Jr.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 9, 2013
Publication Date
April 28, 1977
Publication Information
Publication: The 11th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
79N21394
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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