| 摘要 |
<p>The invention concerns a geostationary satellite stabilised on its orbit along its three axes and comprising at least a first face (8) and at least a second face (9), such that the first face is lit by the sun when the second face is in the shade and inversely. The invention is characterised in that the satellite comprises means for thermal coupling (15, 16) between at least a first face (8) and at least a second face (9). The invention is applicable to temperature control of satellites, in particular telecommunication satellites.</p> |
