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Shell-NASA Vibration-Based Damage CharacterizationThis article describes collaborative research between Shell International Exploration and Production (IE&P) scientists and ISAG personnel to investigate the feasibility of ultrasonic-based characterization of spacecraft tile damage for in-space inspection applications. The approach was proposed by Shell personnel in a Shell-NASA "speed-matching" session in early 2011 after ISAG personnel described challenges inherent in the inspection of MMOD damage deep within spacecraft thermal protection system (TPS) tiles. The approach leveraged Shell's relevant sensor and analytical expertise. The research addressed the difficulties associated with producing 3D models of MMOD damage cavities under the surface of a TPS tile, given that simple image-based sensing is constrained by line of sight through entry holes that have diameters considerably smaller than the underlying damage cavities. Damage cavity characterization is needed as part of a vehicle inspection and risk reduction capability for long-duration, human-flown space missions. It was hoped that cavity characterization could be accomplished through the use of ultrasonic techniques that allow for signal penetration through solid material.
Document ID
20150003816
Acquisition Source
Johnson Space Center
Document Type
Other
Authors
Rollins, John M.
(Jacobs Technology, Inc. Houston, TX, United States)
Date Acquired
March 27, 2015
Publication Date
January 1, 2014
Publication Information
Publication: ARES Biennial Report 2012 Final
Subject Category
Quality Assurance And Reliability
Space Transportation And Safety
Distribution Limits
Public
Copyright
Public Use Permitted.
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