| タイトル | Thermionic technology infrastructure for space power |
| 著者（英） | Huffman, F.; Reagan, P.; Merrill, O.; Miskolczy, G. |
| 著者所属（英） | Thermo Electron Corp. |
| 発行日 | 1982-01-01 |
| 言語 | eng |
| 内容記述 | An assessment is made of the potential effectiveness, designs, and technological difficulties involved in the construction of space nuclear reactors coupled to thermionic energy converters (TEC). The TECs can be positioned either inside or outside of the reactor core. The out-of-core design lowers the reactor shielding requirements, as well as removing the need for mechanically pumped coolant for the reactor. R&D is still needed for the heat pipes for the reactor and the collectors, electrical insulation, and to reduce the potential losses in the interelectrode space. A cylindrical converter for the out-of-core configuration consists of a tungsten emitter heated by a tungsten-lithium heat pipe. The collector is a layer of tungsten oxide deposited on a Nb-1%Zr alloy, and has been tested at emitter temperatures of 1300-1850 K and a collector temperature range of 700-850 K. A design of a superheated thermionic converter is described, noting that a prototype has been operated at 1730 K for 12,000 hr. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 83A27298 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/404909 |
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