| 摘要 |
The invention relates to a propulsion bay (1) intended to be transported, at least temporarily, in a space launch vehicle (2) and comprising an adapter (3) that co-operates with at least one system located, at least temporarily, on board the bay (1), said system comprising an electrical power supply. The bay is characterised in that it also comprises at least one electric space propulsion engine that can be powered by the power supply of the system. |
