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Nonintrusive inertial vibration isolation technology for microgravity space experimentsThe dynamic acceleration environment observed on Space Shuttle flights to date and predicted for the Space Station has complicated the analysis of prior microgravity experiments and prompted concern for the viability of proposed space experiments requiring long-term, microgravity environments. Isolation systems capable of providing significant improvements to this environment exist, but at present have not been demonstrated in flight configurations. A summary of the theoretical evaluation for two one degree-of-freedom (DOF) active magnetic isolators and their predicted response to both direct and base excitations is presented. These isolators can be used independently or in concert to isolate acceleration-sensitive microgravity space experiments, dependent on the isolation capability required for specific experimenter needs.
Document ID
19900002585
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Grodsinsky, Carlos M.
(NASA Lewis Research Center Cleveland, OH, United States)
Brown, Gerald V.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1989
Subject Category
Engineering (General)
Report/Patent Number
AIAA PAPER 90-0741
NAS 1.15:102386
NASA-TM-102386
E-5127
Report Number: AIAA PAPER 90-0741
Report Number: NAS 1.15:102386
Report Number: NASA-TM-102386
Report Number: E-5127
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Reno, NV
Country: United States
Start Date: January 8, 1990
End Date: January 11, 1990
Sponsors: AIAA
Accession Number
90N11901
Funding Number(s)
PROJECT: RTOP 694-03-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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