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Structures and Design Phase I Summary for the NASA Composite Cryotank Technology Demonstration ProjectA description of the Phase I structures and design work of the Composite Cryotank Technology Demonstration (CCTD) Project is in this paper. The goal of the CCTD Project in the Game Changing Development (GCD) Program is to design and build a composite liquid-hydrogen cryogenic tank that can save 30% in weight and 25% in cost compared to state-of-the-art aluminum metallic cryogenic tank technology when the wetted composite skin wall is at an allowable strain of 5000 in/in. Three Industry teams developed composite cryogenic tank concepts that are compared for weight to an aluminum-lithium (Al-Li) cryogenic tank designed by NASA in Phase I of the CCTD Project. The requirements used to design all of the cryogenic tanks in Phase I will be discussed and the resulting designs, analyses, and weight of the concepts developed by NASA and Industry will be reviewed and compared.
Document ID
20130013009
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Johnson, Ted
(NASA Langley Research Center Hampton, VA, United States)
Sleight, David W.
(NASA Langley Research Center Hampton, VA, United States)
Martin, Robert A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 27, 2013
Publication Date
April 8, 2013
Subject Category
Composite Materials
Report/Patent Number
AIAA Paper 2013-1825
NF1676L-15319
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 Society of Mechanical Engineers, American Inst. of Aeronautics and Astronautics, American Society for Composites, American Helicopter Society, Inc., American Society of Civil Engineers
Funding Number(s)
WBS: WBS 813188.01.07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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