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Mechanical isolation for gravity gradiometersIn principle, gravity gradiometers are immune to the effects of acceleration and vibrations. In real instruments, scale factor errors and structural compliance lead to undesired instrument outputs. Described here are the instruments and the fundamental sources of the problems, a calculation of the magnitude of the effects, a demonstration of the need for isolation in the Shuttle (indeed, almost any spacecraft), and the Jet Propulsion Laboratory eddy current isolation technique and its current development status.
Document ID
19910003099
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sonnabend, David
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1990
Publication Information
Publication: NASA, Marshall Space Flight Center, Measurement and Characterization of the Acceleration Environment on Board the Space Station
Subject Category
Spacecraft Instrumentation
Accession Number
91N12412
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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