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Thermal-Mechanical Cyclic Test of a Composite Cryogenic Tank for Reusable Launch VehiclesThis viewgraph presentation provides an overview of thermal-mechanical cyclic tests conducted on a composite cryogenic tank designed for reusable launch vehicles. Topics covered include: a structural analysis of the composite cryogenic tank, a description of Marshall Space Flight Center's Cryogenic Structure Test Facility, cyclic test plans and accomplishments, burst test and analysis and post-testing evaluation.
Document ID
20030062263
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Messinger, Ross (Boeing Co. Huntington Beach, CA, United States)
Pulley, John (Boeing Co. Huntington Beach, CA, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2003
Subject Category
Composite Materials
Meeting Information
Meeting: 44th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics, & Material Conference
Location: Norfolk, VA
Country: United States
Start Date: April 7, 2003
End Date: April 10, 2003
Sponsors: American Society for Composites, American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, American Society of Civil Engineers
Funding Number(s)
CONTRACT_GRANT: NCC8-39
Distribution Limits
Public
Copyright
Public Use Permitted.

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