(1) InnoSat technology
* propultion (propulsion to keep constellation)
=> technologically possible and implementation depends on budget/priority
 -  if possible can thruster be as small as about 1N/msec?
 - how about atmospheric drag? => yes

* local time (solar panel) => battery costs weight, but technologically possible

* radiation (appoge)
=> less investigated, and investigation depends no priority
   So far changing component (costs budget) or shielding (cost weight)

* GPS (timing+location is importation for constellation with wave instrument)
=> yes they have

* possible boom (KTH/Nickoly said 1 m)
=> ask Nickolay

* will mass really 50 kg + payload?  What would be payload mass with propulsion?
=> Japanese side should give limit

* Will 2025-2026 better?
=> better than 2023

* Next proposal
=> Yama (with FACTORS) and Nickolay (without FACTORS, just for EISCAT_3D)

(2) ESCAPE
* no particular agenda

(3) Japanese missions
* Three mission for two spot

(4) Space weather
* magnetometer situation (what should I be prepared as magnetometer PI?)
=> need to discuss with Herman but RS does not know the development
* L5 and other (D3S) situation
=> Johan with forward info to Futaana and Stas
* SSA advisery?
=> ask Lars


-------------------
宇宙研のESAアレルギー

３つに選ばれた時

光学実験の可能な欧州CoIが欲しい＝
Latmos + Sauer の組み合わせか Sauer + Urban の組み合わせ

WG は2019年3月までに立ち上げる

SPICA と同等を宣伝文句

6月11日〜15日