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Structurally adaptive space crane concept for assembling space systems on orbitMany future human space exploration missions will probably require large vehicles that must be assembled on orbit. Thus, a device that can move, position, and assemble large and massive spacecraft components on orbit becomes essential for these missions. A concept is described for such a device: a space crane concept that uses erectable truss hardware to achieve high-stiffness and low-mass booms and uses articulating truss joints that can be assembled on orbit. The hardware has been tested and shown to have linear load-deflection response and to be structurally predictable. The hardware also permits the crane to be reconfigured into different geometries to satisfy future assembly requirements. A number of articulating and rotary joint concepts have been sized and analyzed, and the results are discussed. Two strategies were proposed to suppress motion-induced vibration: placing viscous dampers in selected truss struts and preshaping motion commands. Preliminary analyses indicate that these techniques have the potential to greatly enhance structural damping.
Document ID
19930006179
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Dorsey, John T.
(NASA Langley Research Center Hampton, VA, United States)
Sutter, Thomas R.
(NASA Langley Research Center Hampton, VA, United States)
Wu, K. Chauncey
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1992
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
L-17175
NAS 1.15:3307
NASA-TP-3307
Accession Number
93N15368
Funding Number(s)
PROJECT: RTOP 506-43-41-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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