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Hydrocarbon-fuel/combustion-chamber-liner materials compatibilityThe results of dynamic tests using methane and NASA-Z copper test specimen under conditions that simulate those expected in the cooling channels of a regeneratively cooled LOX/hydrocarbon booster engine operating at chamber pressures up to 3000 psi are presented. Methane with less than 0.5 ppm sulfur contamination has little or no effect on cooling channel performance. At higher sulfur concentrations, severe corrosion of the NASA-Z copper alloy occurs and the cuprous sulfide Cu2S, thus formed impedes mass flow rate and heat transfer efficiency. Therefore, it is recommended that the methane specification for this end use set the allowable sulfur content at 0.5 ppm (max). Bulk high purity liquid methane that meets this low sulfur requirement is currently available from only one producer. Pricing, availability, and quality assurance are discussed in detail. Additionally, it was found that dilute sodium cyanide solutions effectively refurbish sulfur corroded cooling channels in only 2 to 5 minutes by completely dissolving all the Cu2S. Sulfur corroded/sodium cyanide refurbished channels are highly roughened and the increased surface roughness leads to significant improvements in heat transfer efficiency with an attendant loss in mass flow rate. Both the sulfur corrosion and refurbishment effects are discussed in detail.
Document ID
19910011994
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Homer, G. David
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1991
Subject Category
Nonmetallic Materials
Report/Patent Number
NASA-CR-187104
NAS 1.26:187104
KBQ-FR-2
AD-A235644
Accession Number
91N21307
Funding Number(s)
CONTRACT_GRANT: NAS3-25070
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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