Raijin-2 (Rising-2) is a Japanese micro-
satellite launched in 2014. The satellite is built around a 10 cm diameter, 1m focal length
Cassegrain telescope and features the following instruments:
HPT - main telescope with 5m resolution at nadir, operating in visible and near-infrared bands
BOL - bolometer array camera for cloud temperature measurement
WFC - wide field-of-view CCD camera
LSI-N and LSI-W - 2 CMOS medium field-of-view cameras for near-infrared imaging
VLF-ANT, R - radio antenna to receive signatures of lighting events
All instruments are powered by GaAs solar cells mounted on the spacecraft body, with estimated electrical power of 47.6W. The spacecraft features an unusual central-pillar bus, inherited from the
Sprite-Sat satellite. The attitude control is done by means of reaction wheels and magneto-torquers, and qualified for 0.1 degrees angular accuracy.
The satellite is intended for atmosphere research, especially for gathering statistics on cloud formation and the occurrence of
sprites in the upper atmosphere. Mission data are down-linked in S-band with maximal data rate of 38.4 kbit/s.[1]
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Cubesats are smaller. Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
