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The mechanical design of an imaging photopolarimeter for the Jupiter missions (Pioneer 10 and 11)The mechanical design and fabrication are discussed of the imaging photopolarimeter (IPP), a multifunction space-qualified instrument used on the Jupiter Pioneer missions. The extreme environmental requirements for the structural design, optical system, and mechanisms are described with detailed discussion of some of the design and fabrication problems encountered.
Document ID
19760012099
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kodak, J. C.
(Santa Barbara Research Center Goleta, CA, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Publication Information
Publication: NASA. Kennedy Space Center 9th Aerospace Mech. Symp.
Subject Category
Spacecraft Instrumentation
Accession Number
76N19187
Funding Number(s)
CONTRACT_GRANT: NAS2-5605
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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