| 摘要 |
This separation mechanism for a space structure (1A) is for separating a second structure (3) from a first structure (2) in outer space and comprises a first member (4) that is fixed to the first structure (2) and a second member (5) that is fixed to the second structure (3). The first member (4) and the second member (5) are both made of an insulating material having a relatively low thermal conductivity. A current-carrying layer (6) is interposed between the first member (4) and the second member (5), and the first member (4) or the second member (5) is joined to the current-carrying layer (6) by means of a joining layer (7). The current-carrying layer (6) is configured so as to destroy or melt the joining layer (7) by means of heat that is generated when a current is caused to flow in the current-carrying layer (6). |
