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Latch fittings for the scientific instruments on the space telescopeLatch fittings which kinematically mount the replaceable scientific instruments onto the Space Telescope must maintain precise alignment and thermal stability for on-orbit observations. Design features which are needed to meet stringent criteria include the use of ceramic isolators for thermal and electrical insulation, materials with different coefficients of thermal expansion for athermalization, precision manufacturing procedures, and extremely tight tolerances. A specific latch fitting to be discussed is a ball-and-socket design. In addition, testing, crew aids, and problems will be covered.
Document ID
19830016627
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dozier, J. D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Kaelber, E.
(Perkin-Elmer)
Date Acquired
August 11, 2013
Publication Date
May 1, 1983
Publication Information
Publication: JPL The 17th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
83N24898
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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