Raiko
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| Mission type | Technology |
|---|---|
| Operator | Tohoku University Wakayama University |
| Spacecraft properties | |
| Spacecraft type | 2U CubeSat |
| Launch mass | 2 kilograms (4.4 lb) |
| Start of mission | |
| Launch date | 21 July 2012, 02:06 UTC[1] |
| Rocket | H-IIB |
| Launch site | Tanegashima Y2 |
| Deployed from | ISS |
| Deployment date | 4 October 2012 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Inclination | 51.65 degrees |
Raiko (Japanese: 雷鼓, literally thunder drum) is a Japanese satellite which was built and operated by Tohoku and Wakayama Universities. A two-unit CubeSat, Raiko was deployed from the International Space Station on October 4, 2012, having been launched in July.
Raiko was launched aboard the Kounotori 3 spacecraft,[2] atop an H-IIB carrier rocket flying from Pad 2 of the Yoshinobu Launch Complex at the Tanegashima Space Centre. The launch occurred at 02:06 UTC on 21 July 2012.[1] Four other CubeSats were launched with Raiko; We-Wish, Niwaka, TechEdSat and F-1. The five CubeSats was delivered to the International Space Station for deployment. CubeSats were deployed from Japanese Experiment Module Kibo via the J-SSOD system on October 4, 2012 .[3][4]
Named after a Japanese god of thunder,[5] Raiko is a 2-kilogram (4.4 lb) spacecraft, which will be used for technology demonstration. It carries a camera with a fish-eye lens for Earth imaging,[6] a prototype star tracker, a deployable membrane to slow the satellite, lowering its orbit, a photographic system to measure the satellite's movement relative to the International Space Station, and a Ku-band antenna for communications and Doppler ranging experiments.[7]
We-Wish, Raiko, FITSat 1, F-1, and TechEdSat travelled to orbit aboard HTV-3.[8]
References
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<references />, or <references group="..." />External links
- Official web page (Japanese)
- @RAIKO_CUBESAT on TwitterLua error in Module:WikidataCheck at line 28: attempt to index field 'wikibase' (a nil value).
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