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Deployable controllable geometry truss beamA study was conducted on a truss beam structural concept that can deploy and maneuver in a serpentine manner to align or position the truss beam tip. The truss beam is composed of a series of rod members connected together at joints that provide the required rotational degrees of freedom. The current study was conducted to evaluate the requirements of the joints and define a mechanical assembly that could provide both high structural stiffness and the required maneuverability. The truss beam requires two joint types; both types were fabricated and incorporated in a demonstration model. An analysis of the concept was performed to define the location and orientation of the beam tip during deployment and serpentine maneuvers.
Document ID
19850019622
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Rhodes, M. D.
(NASA Langley Research Center Hampton, VA, United States)
Mikulas, M. M., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1985
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-86366
L-15901
NAS 1.15:86366
Report Number: NASA-TM-86366
Report Number: L-15901
Report Number: NAS 1.15:86366
Accession Number
85N27934
Funding Number(s)
PROJECT: RTOP 506-53-43-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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