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Computer Tomography Analysis of Fastrac Composite Thrust Chamber AssembliesComputed tomography (CT) inspection has been integrated into the production process for NASA's Fastrac composite thrust chamber assemblies (TCAs). CT has been proven to be uniquely qualified to detect the known critical flaw for these nozzles, liner cracks that are adjacent to debonds between the liner and overwrap. CT is also being used as a process monitoring tool through analysis of low density indications in the nozzle overwraps. 3d reconstruction of CT images to produce models of flawed areas is being used to give program engineers better insight into the location and nature of nozzle flaws.
Document ID
20000068919
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Beshears, Ronald D.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 7, 2013
Publication Date
April 20, 2000
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA Paper 2000-3399
Report Number: AIAA Paper 2000-3399
Distribution Limits
Public
Copyright
Public Use Permitted.
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