| タイトル | Actively Cooled Ceramic Matrix Composite Concepts for High Heat Flux Applications |
| 本文（外部サイト） | http://hdl.handle.net/2060/20050198964 |
| 著者（英） | Jaskowiak, Martha H.; Dickens, Kevin; Eckel, Andrew J. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2004-01-01 |
| 言語 | eng |
| 内容記述 | High temperature composite heat exchangers are an enabling technology for a number of aeropropulsion applications. They offer the potential for mass reductions of greater than fifty percent over traditional metallics designs and enable vehicle and engine designs. Since they offer the ability to operate at significantly higher operating temperatures, they facilitate operation at reduced coolant flows and make possible temporary uncooled operation in temperature regimes, such as experienced during vehicle reentry, where traditional heat exchangers require coolant flow. This reduction in coolant requirements can translate into enhanced range or system payload. A brief review of the approaches, challenges and test results are presented, along with a status of recent government-funded projects. |
| NASA分類 | Composite Materials |
| レポートNO | E-14885 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/219765 |
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