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Analytical determination of space station response to crew motion and design of suspension system for microgravity experimentsThe objective of this investigation is to make analytical determination of the acceleration produced by crew motion in an orbiting space station and define design parameters for the suspension system of microgravity experiments. A simple structural model for simulation of the IOC space station is proposed. Mathematical formulation of this model provides the engineers a simple and direct tool for designing an effective suspension system.
Document ID
19870013319
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Liu, Frank C.
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1987
Publication Information
Publication: NASA. Marshall Space Flight Center Structural Dynamics and Control Interaction of Flexible Structures
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N22752
Funding Number(s)
CONTRACT_GRANT: NGT-01-008-021
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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