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Vacuum chamber translation/positioning mechanism and welding power supply controllerWelding in the vacuum of space represents an important and fundamental problem for space exploration. Repairs or connection of metal components on orbit or during travel to the moon or distant planets may be required. Cracks or holes in spacecraft skin or supporting structures external to the pressurized section will require some type of repair that must be permanently made to the skin or support by welding. The development of a translation/positioning system that will permit research into welding of metal samples in a small vacuum chamber located at Marshall Space Flight Center (MSFC) is addressed. The system and associated software was tested to the extent possible without the availability of the welder power supply or control computer that must be supplied by MSFC. Software has been developed for straight line welding. More extensive and varied translations are possible with simple alterations to the operating software to use the full capabilities of this three axes system. The source code 'VW.BAS' has been provided to serve as an example for further development of the vacuum welder translation system.
Document ID
19930003008
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Smith, James E., Jr.
(Alabama Univ. Huntsville, AL, United States)
Cashon, John L.
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1992
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.26:184465
NASA-CR-184465
Accession Number
93N12196
Funding Number(s)
CONTRACT_GRANT: NAS8-36955
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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