2912 JEM エアロックの設計

抄録

Japanese Experiment Module (JEM) of International Space Station (ISS), has unique Airlock. JEM Airlock will be used when the experimental equipment shall be carried out/in between Pressurised Module and Exposed Facility. JEM Airlock has cylindrical structure and two hatches. Experiment payloads are carried by the Slide Table and Capture Mechanism. This paper shows the design overview of JEM Airlock.