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Structural Design and Sizing of a Metallic Cryotank ConceptThis paper presents the structural design and sizing details of a 33-foot (10 m) metallic cryotank concept used as the reference design to compare with the composite cryotank concepts developed by industry as part of NASA s Composite Cryotank Technology Development (CCTD) Project. The structural design methodology and analysis results for the metallic cryotank concept are reported in the paper. The paper describes the details of the metallic cryotank sizing assumptions for the baseline and reference tank designs. In particular, the paper discusses the details of the cryotank weld land design and analyses performed to obtain a reduced weight metallic cryotank design using current materials and manufacturing techniques. The paper also discusses advanced manufacturing techniques to spin-form the cryotank domes and compares the potential mass savings to current friction stir-welded technology.
Document ID
20130012938
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Sleight, David W.
(NASA Langley Research Center Hampton, VA, United States)
Martin, Robert A.
(NASA Langley Research Center Hampton, VA, United States)
Johnson, Theodore F.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 27, 2013
Publication Date
April 8, 2013
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-15305
Meeting Information
Meeting: 54th AIAA/ASME/ASCE/AHS/ASC, Structures, Structural Dynamics, and Materials Conference
Location: Boston, MA
Country: United States
Start Date: April 8, 2013
End Date: April 11, 2013
Sponsors: American Inst. of Aeronautics and Astronautics, American Helicopter Society, Inc., American Society of Civil Engineers, American Society for Composites, American Society of Mechanical Engineers
Funding Number(s)
WBS: WBS 813188.01.07.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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