RAIKO
RAIKO
Spacecraft name RAIKO
Form factor CubeSat
Units or mass 2U
Mass in kg 2.603 kg
Status Reentry 2013-08-06. Was operational until 2013-07-15. For the last 20 days only beacons.
Launched 2012-07-21
NORAD ID 38852
Deployer J-SSOD (JEM Small Satellite Orbital Deployer)
Launcher H-IIB (H2B)
Deployment Deployed from ISS on 2012-10-04
Entity name Tohoku University
Institution University
Entity type Academic / Education
Country Japan
Launch brokerer JAXA
Partners Wakayama University
Oneliner

Demonstrate technologies for larger satellites including CMOS and CCD sensors.

Description

Demonstration of new electronics or mechanism usable for 50-kg microsatellites, which are CMOS color sensor, CCD color sensor, CCD star sensor, and film deployment mechanism.

Failure cause Assumed that the frequency lock function of on-board receiver was easily terminated because the satellite rotation speed was fast.
Sources [1] [2]
Photo sources [1]
Keywords Ku-band

Last modified: 2023-06-08

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Created by Erik Kulu

Email: erik.kulu@nanosats.eu
LinkedIn: linkedin.com/in/erikkulu

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