| タイトル | The alkali metal thermoelectric converter /AMTEC/ - A new direct energy conversion technology for aerospace power |
| 著者（英） | Bankston, C. P.; Jones, R.; Ewell, R.; Cole, T. |
| 著者所属（英） | Jet Propulsion Lab., California Inst. of Tech. |
| 発行日 | 1982-06-01 |
| 言語 | eng |
| 内容記述 | A thermally regenerative electrochemical device for the direct conversion of heat to electrical energy, the alkali metal thermoelectric converter (AMTEC), is characterized by potential efficiencies on the order of 15-40% and possesses no moving parts, making it a candidate for space power system applications. Device conversion efficiency is projected on the basis of experimental voltage vs current curves exhibiting power densities of 0.7 W/sq cm and measured electrode efficiencies of up to 40%. Preliminary radiative heat transfer measurements presented may be used in an investigation of methods for the reduction of AMTEC parasitic radiation losses. AMTEC assumes heat input and rejection temperatures of 900-1300 K and 400-800 K, respectively. The working fluid is liquid sodium, and the porous electrode employed is of molybdenum. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 82A31876
AIAA PAPER 82-0862 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/410669 |
