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Development of a ferromagnetic rotary vacuum sealed spacecraft spin fixtureA number of successful spacecraft tests were conducted on an environmental spin fixture which utilizes a ferrofluidic rotary vacuum seal. The 27 cm (10.5 inch) diameter fixture drive shaft supports and spins communications satellites during flight acceptance testing in a thermal vacuum chamber. The drive shaft rotary seal serves to maintain the canned drive system electro-mechanical components at ambient pressure within the space simulator. The ferromagnetic fluid seal was chosen over conventional mechanical sealing devices for its zero-leakage, zero-wear, and minimum friction drag characteristics, as well as its high reliability potential.
Document ID
19790010844
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Levine, M. B.
(Hughes Aircraft Co. El Segundo, CA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1977
Publication Information
Publication: NASA. Goddard Space Flight Center Ninth Conf. on Space Simulation
Subject Category
Ground Support Systems And Facilities (Space)
Accession Number
79N19015
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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