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Refractory Materials for Flame Deflector Protection System Corrosion Control: Flame Deflector Protection System Life Cycle Cost Analysis ReportA 20-year life cycle cost analysis was performed to compare the operational life cycle cost, processing/turnaround timelines, and operations manpower inspection/repair/refurbishment requirements for corrosion protection of the Kennedy Space Center launch pad flame deflector associated with the existing cast-in-place materials and a newer advanced refractory ceramic material. The analysis compared the estimated costs of(1) continuing to use of the current refractory material without any changes; (2) completely reconstructing the flame trench using the current refractory material; and (3) completely reconstructing the flame trench with a new high-performance refractory material. Cost estimates were based on an analysis of the amount of damage that occurs after each launch and an estimate of the average repair cost. Alternative 3 was found to save $32M compared to alternative 1 and $17M compared to alternative 2 over a 20-year life cycle.
Document ID
20130011672
Acquisition Source
Kennedy Space Center
Document Type
Technical Memorandum (TM)
Authors
Calle, Luz Marina
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Hintze, Paul E.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Parlier, Christopher R.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Coffman, Brekke E.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Kolody, Mark R.
(ASRC Aerospace Corp. Cleveland, OH, United States)
Curran, Jerome P.
(ASRC Aerospace Corp. Cleveland, OH, United States)
Trejo, David
(Texas A&M Univ. TX, United States)
Reinschmidt, Ken
(Texas A&M Univ. TX, United States)
Kim, Hyung-Jin
(Texas A&M Univ. TX, United States)
Date Acquired
August 27, 2013
Publication Date
January 1, 2009
Subject Category
Mechanical Engineering
Report/Patent Number
NASA/TM-2013-216321
Report Number: NASA/TM-2013-216321
Distribution Limits
Public
Copyright
Public Use Permitted.
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