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Friction Stir Welding of Large Scale Cryogenic Tanks for Aerospace ApplicationsThe Marshall Space Flight Center (MSFC) has established a facility for the joining of large-scale aluminum cryogenic propellant tanks using the friction stir welding process. Longitudinal welds, approximately five meters in length, have been made by retrofitting an existing vertical fusion weld system, designed to fabricate tank barrel sections ranging from two to ten meters in diameter. The structural design requirements of the tooling, clamping and travel system will be described in this presentation along with process controls and real-time data acquisition developed for this application. The approach to retrofitting other large welding tools at MSFC with the friction stir welding process will also be discussed.
Document ID
19990103022
Acquisition Source
Marshall Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Russell, Carolyn
(NASA Marshall Space Flight Center Huntsville, AL United States)
Ding, R. Jeffrey
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1998
Subject Category
Launch Vehicles And Space Vehicles
Meeting Information
Meeting: Aeromat 1998
Location: McLean, VA
Country: United States
Start Date: June 15, 1998
End Date: June 18, 1998
Distribution Limits
Public
Copyright
Other

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