| タイトル | Hydrocarbon-fuel/combustion-chamber-liner materials compatibility |
| 本文（外部サイト） | http://hdl.handle.net/2060/19910011994 |
| 著者（英） | Homer, G. David |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1991-04-01 |
| 言語 | eng |
| 内容記述 | The 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. |
| NASA分類 | NONMETALLIC MATERIALS |
| レポートNO | 91N21307
KBQ-FR-2
NAS 1.26:187104
AD-A235644
NASA-CR-187104 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/133206 |
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