An Advanced D-Strut™

Item

Title
An Advanced D-Strut™
Report Number
WL-TR-91-3078 Volume III, p. IAC-1 thru IAC-17
Creator
Davis, L. Porter
Ginter, Steven D.
Corporate Author
Honeywell Inc., Satellite Systems Operation
Date
1991
Date Issued
1991-08
Extent
17
Identifier
ADA241313
Format
1 online resource
Abstract
A viscous-damping technique offering high damping for spacecraft truss structures has been under development since 1986. The technique, known as the D-Strut™, uses a small mechanical viscous damper configured in an inner-outer tube-strut configuration, and replaces the nominal-type strut. The viscous-damped D-Strut has been employed in more compliant isolation systems for space applications, including the Hubble Space Telescope. The United States Air Force and Jet Propulsion Laboratory have investigated D-Struts for use in high specific-stiffness truss structures. This technique is an attractive means of attaining significant damping levels in space structures.
Description
A viscous-damping technique offering high damping for spacecraft truss structures has been under development since 1986. The technique, known as the D-Strut™, uses a small mechanical viscous damper configured in an inner-outer tube-strut configuration, and replaces the nominal-type strut. The viscous-damped D-Strut has been employed in more compliant isolation systems for space applications, including the Hubble Space Telescope. The United States Air Force and Jet Propulsion Laboratory have investigated D-Struts for use in high specific-stiffness truss structures. This technique is an attractive means of attaining significant damping levels in space structures.
Distribution Classification
1
Distribution Conflict
No
DTIC Record Exists
No
Illinois Tech Related
No
Photo Quality
Not Needed
Report Availability
Full text available
Type
article
Media
artcileIAC

Linked resources


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Items with "Has Part: An Advanced D-Strut™"
Title Class
Proceedings of Damping '91: 13-15 February 1991 San Diego, California (GCA-1 through JCB-17)