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Low cost, SPF aluminum cryogenic tank structure for ALSPast production work has shown that cryogenic tank structure for the Shuttle Booster Rockets and the Titan system have very high life cycle costs for the fuel tank structure. The tanks are machined stiffener-skin combination that are subsequently formed into the required contour after machining. The material scrap rate for these configurations are usually high, and the loss of a tank panel due to forming or heat treatment problems is very costly. The idea of reducing the amount of scrap material and scrapped structural members has prompted the introduction of built-up structure for cryogenic tanks to be explored on the ALS program. A build-up structure approach that has shown improvements in life cycle cost over the conventional built-up approach is the use of superplastically formed (SPF) stiffened panels (reducing the overall part count and weight for the tank) resistance spot welded (RSW) to outer tank skin material. The stiffeners provide for general stability of the tank, while the skin material provides hoop direction continuity for the loads.
Document ID
19930008841
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Anton, Claire E.
(Rockwell International Corp. Los Angeles, CA, United States)
Rasmussen, Perry
(Rockwell International Corp. Los Angeles, CA, United States)
Thompson, Curt
(Rockwell International Corp. Los Angeles, CA, United States)
Latham, Richard
(Rockwell International Corp. Los Angeles, CA, United States)
Hamilton, C. Howard
(Rockwell International Corp. Los Angeles, CA, United States)
Ren, Ben
(Rockwell International Corp. Los Angeles, CA, United States)
Gandhi, Chimata
(Rockwell International Corp. Los Angeles, CA, United States)
Hardwick, Dallis
(Rockwell International Corp. Los Angeles, CA, United States)
Date Acquired
September 6, 2013
Publication Date
September 22, 1992
Subject Category
Structural Mechanics
Report/Patent Number
NA-92-1097
REPT-92HP-0084-053
NASA-CR-189654
NAS 1.26:189654
Report Number: NA-92-1097
Report Number: REPT-92HP-0084-053
Report Number: NASA-CR-189654
Report Number: NAS 1.26:189654
Accession Number
93N18030
Funding Number(s)
PROJECT: RTOP 946-01-00-83
CONTRACT_GRANT: NAS1-18590
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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