| タイトル | Graphite Fiber/Copper Matrix Composites for Space Power Heat Pipe Fin Applications |
| 著者（英） | Ellis, David L.; McDanels, David L.; Baker, Karl W. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1991-01-01
1991 |
| 言語 | eng |
| 内容記述 | High specific thermal conductivity (thermal conductivity divided by density) is a major design criterion for minimizing system mass for space power systems. For nuclear source power systems, graphite fiber reinforced copper matrix (Gr/Cu) composites offer good potential as a radiator fin material operating at service temperatures above 500 K. Specific thermal conductivity in the longitudinal direction is better than beryllium and almost twice that of copper. The high specific thermal conductivity of Gr/Cu offers the potential of reducing radiator mass by as much as 30 percent. Gr/Cu composites also offer the designer a range of available properties for various missions and applications. The properties of Gr/Cu are highly anisotropic. Longitudinal elastic modulus is comparable to beryllium and about three times that of copper. Thermal expansion in the longitudinal direction is near zero, while it exceeds that of copper in the transverse direction. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 93A13789
E-5697 |
| 権利 | Copyright |
|
