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Nutation Damper SystemThe Nutation Damper System is a three function mechanism designed for the Galileo Spacecraft, a spin stabilized deep-space probe to Jupiter. By damping the movement of a large deployable science boom acting as an outboard pendulum, the nutation damper rapidly stabilizes the spacecraft from dynamic irregularities. The system includes the boom deployment device and the ultra-low friction boom hinge. This paper describes the mechanism, the degree to which friction, stiction and lost motion have been eliminated, and the unique test methods that allow its performance to be measured.
Document ID
19830016624
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sevilla, D. R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 11, 2013
Publication Date
May 1, 1983
Publication Information
Publication: The 17th Aerospace Mech. Symp.
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
83N24895
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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