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Feasibility of remotely manipulated welding in space. A step in the development of novel joining technologiesIn order to establish permanent human presence in space technologies of constructing and repairing space stations and other space structures must be developed. Most construction jobs are performed on earth and the fabricated modules will then be delivered to space by the Space Shuttle. Only limited final assembly jobs, which are primarily mechanical fastening, will be performed on site in space. Such fabrication plans, however, limit the designs of these structures, because each module must fit inside the transport vehicle and must withstand launching stresses which are considerably high. Large-scale utilization of space necessitates more extensive construction work on site. Furthermore, continuous operations of space stations and other structures require maintenance and repairs of structural components as well as of tools and equipment on these space structures. Metal joining technologies, and especially high-quality welding, in space need developing.
Document ID
19840012789
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Masubuchi, K.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Agapakis, J. E.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Debiccari, A.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Vonalt, C.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1983
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.26:175437
NASA-CR-175437
Report Number: NAS 1.26:175437
Report Number: NASA-CR-175437
Accession Number
84N20857
Funding Number(s)
CONTRACT_GRANT: NASW-3740
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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