XI IV [ISSL]
The code name of ISSL's CubeSat is "XI" (X-factor Investigator). This derives from its cubic shape (XI means domino in Japanese).
The XI mission is on-orbit verifications of the technology necessary for super-small satellite system. Acquiring indispensable technology on spacecraft, such as communication, power and electronics, it will establish the development methodology of the small satellite. And by extensively using commercial-off-the-shell components, the total development cost will be drastically reduced and a database on the space-use of the COTS parts will be built. A number of Cubesat-XI prototypes have been built - the fourth is the first flight model with the fifth being its backup.
Nation: | Japan |
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Type / Application: | Technology |
Operator: | University of Tokyo |
Contractors: | University of Tokyo |
Equipment: | |
Configuration: | CubeSat (1U) |
Propulsion: | None |
Power: | Solar cells, batteries |
Lifetime: | |
Mass: | 1 kg |
Orbit: | 822 km × 828 km, 98.73° (#4); 682 km × 708 km, 98.18° (#5) |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
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XI 1 (XI-I) | - | not launched | ||||
XI 2 (XI-II) | - | not launched | ||||
XI 3 (XI-III) | - | not launched | ||||
XI 4 (XI-IV, CO 57, CubeSat-OSCAR 57) | 2003-031J | 30.06.2003 | Pl LC-133/3 | Rokot-KM | with MOST, MIMOSA, CanX 1, AAU-Cubesat, DTUSat, CUTE 1, QuakeSat, Monitor-E GVM | |
XI 5 (XI-V, CO 58, CubeSat-OSCAR 58) | 2005-043F | 27.10.2005 | Pl LC-132/1 | Kosmos-3M | with TopSat 1, China-DMC+4, Mozhayets 5, Sina 1, SSETI-Express, UWE 1, Ncube 2, Rubin 5-ASOLANT |