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NASA Experience with the Shuttle External TankThis report is a presentation reviewing the external tanks which are used to provide the propellants for the space shuttle engines. The design of the external tank, and its lift capability improvements are reviewed. The configuration, materials, and key technologies of the super lightweight tank (SLWT) are also described. Among the key technologies which allow the SLWT project to succeed, are the successful development of an appropriate alloy. The reasons for choosing the alloy, Aluminum-Lithium 2195, and issues involved in welding are reviewed. Tests of the weld procedures, and pictures of the test results are shown. The External Tank Project has successfully made the transition from the LWT design to the SLWT design. The SLWT Provides two thirds of the weight savings required to place the Space Station in a 51.6 Degree Orbit.
Document ID
19990047392
Acquisition Source
Marshall Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Bickley, Fred
(NASA Marshall Space Flight Center Huntsville, AL United States)
Schwinghamer, Robert J.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
March 17, 1999
Subject Category
Space Transportation
Meeting Information
Meeting: National Manufacturing Week
Location: Chicago, IL
Country: United States
Start Date: March 15, 1999
End Date: March 18, 1999
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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