| 摘要 |
PROBLEM TO BE SOLVED: To provide a heat conductive interface portion for a vehicle capable of being operated in space which is highly reliable, durable, capable of being effectively and easily used, capable of enduring the harshness of satellite launch, and which also realizes economical production of a satellite. SOLUTION: Unnecessary heat is eliminated from a heat generation device 12 which is installed on a space vehicle that moves in an orbit in space by disposing a heat conductive interface portion 10 between the heat generation device and a support platform 14. The interface portion 10 is composed of rows of aluminum strips 16 aligned with each other with space in between. The rows cover a radiating surface 20 at a lower side of the device. The strip 16 becomes flat when compressed. Also, the strip 16 has such a configuration that a deformable projection such as a wavy portion which forms the heat conductive interface portion between the heat generation device 12 and the platform 14. |
