| タイトル | Diode laser satellite systems for beamed power transmission |
| 本文（外部サイト） | http://hdl.handle.net/2060/19900015269 |
| 著者（英） | Walker, G. H.; Williams, M. D.; Kwon, J. H.; Humes, D. H. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1990-01-01 |
| 言語 | eng |
| 内容記述 | A power system composed of an orbiting laser satellite and a surface-based receiver/converter is described. Power is transmitted from the satellite to the receiver/converter by laser beam. The satellite components are: (1) solar collector; (2) blackbody; (3) photovoltaic cells; (4) heat radiators; (5) laser system; and (6) transmission optics. The receiver/converter components are: receiver dish; lenticular lens; photocells; and heat radiator. Although the system can be adapted to missions at many locations in the solar system, only two are examined here: powering a lunar habitat; and powering a lunar rover. Power system components are described and their masses, dimensions, operating powers, and temperatures, are estimated using known or feasible component capabilities. The critical technologies involved are discussed and other potential missions are mentioned. |
| NASA分類 | LASERS AND MASERS |
| レポートNO | 90N24585
NAS 1.60:2992
NASA-TP-2992
L-16669 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/137491 |
