| 摘要 |
The panel (PS) has an outer skin or wall (PE) and an inner skin or wall (PI) respectively arranged at exterior and interior of a satellite. A honeycomb shaped core (AM) comprises an integrated heat pipe (CAL) that is fixedly in contact with the outer skin. Heat exchangers are associated with a heat regulation circuit e.g. two-phase mechanically pumped heat regulation loop, that regulates heat by circulation of coolant, outside the panel, where the exchangers comprise an evaporator (EVAP) and a condenser (COND). The condenser is in contact with the heat pipe. The core comprises heat conducting or insulating material. |
