{"id":2637,"date":"2021-07-09T19:45:02","date_gmt":"2021-07-09T10:45:02","guid":{"rendered":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/?page_id=2637"},"modified":"2023-11-14T13:42:02","modified_gmt":"2023-11-14T04:42:02","slug":"about-us","status":"publish","type":"page","link":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/en\/about-us.html","title":{"rendered":"About STL"},"content":{"rendered":"

Research
\n<\/span><\/strong><\/span>Space Transportation System Laboratory (STL) has investigated the issues that occur in spacecraft during atmospheric entry. Various phenomena occur during the entry, descent, and landing (EDL) phases. One of the most critical stages in space missions is characterized by the fact that the spacecraft enters the atmosphere with a high velocity and is decelerated by aerodynamic forces.<\/p>\n

Targets
\n<\/span><\/strong><\/span>During the EDL phase, the flow field around a spacecraft varies widely. For example, the following phenomena and problems occur in spacecraft:<\/p>\n