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Very low frequency suspension systems for dynamic testingSpecifications for a Space Station suspension system which can provide rigid-body translation frequencies on the order of 0.1-0.2 Hz for a 50-foot payload weighing about 3400 lb and having a number of highly flexible appendages are discussed. Two suspension devices are considered, an all-mechanical passive device based on coil springs and a device using a combination of a passive pneumatic system and an active electromagnetic system. Test results show that both devices meet the initial requirements.
Document ID
19890043313
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kienholz, David A.
(CSA Engineering, Inc. Palo Alto, CA, United States)
Crawley, Edward F.
(MIT Cambridge, MA, United States)
Harvey, T. Jeffrey
(AEC-Able Engineering, Inc. Goleta, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 89-1194
Meeting Information
Meeting: AIAA, ASME, ASCE, AHS, and ASC, Structures, Structural Dynamics and Materials Conference
Location: Mobile, AL
Country: United States
Start Date: April 3, 1989
End Date: April 5, 1989
Accession Number
89A30684
Distribution Limits
Public
Copyright
Other

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