NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Damping Mechanisms for Microgravity Vibration Isolation (MSFC Center Director's Discretionary Fund Final Report, Project No. 94-07)As a research facility for microgravity science, the International Space Station (ISS) will be used for numerous investigations such as protein crystal growth, combustion, and fluid mechanics experiments which require a quiescent acceleration environment across a broad spectrum of frequencies. These experiments are most sensitive to low-frequency accelerations and can tolerate much higher accelerations at higher frequency. However, the anticipated acceleration environment on ISS significantly exceeds the required acceleration level. The ubiquity and difficulty in characterization of the disturbance sources precludes source isolation, requiring vibration isolation to attenuate the anticipated disturbances to an acceptable level. This memorandum reports the results of research in active control methods for microgravity vibration isolation.
Document ID
19980017169
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Whorton, M. S.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Eldridge, J. T.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Ferebee, R. C.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Lassiter, J. O.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Redmon, J. W., Jr.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1998
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA/TM-1998-206953
NAS 1.15:206953
M-849
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available