Kolibri 2000 [GDK]
The Kolibri-2000 microsatellite is an educational microsatellite mission. It was launched from the Progress-M1 7 cargo freighter supply craft to the International Space Station, on it way back to Earth, into a 385 km × 388 km orbit inclined at 51.6 degrees. The spacecraft was designed and manufactured by the Special Design Office of space instrument engineering, Space Research Institute of the Russian Academy of sciences, in collaboration with local space industry. The spacecraft mission is educational, and radio amateur frequencies are employed to return data to participating educational institutions in Obninsk (Russia) and Sydney (Australia). Instruments on board include a flux-gate magnetometer, and a particle and electric field analyser. The spacecraft measures 1.25 m high with a diameter of 0.5 m, carries a 2 m gravity gradient boom and four deployable solar panels.
Nation: | Russia, Australia |
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Type / Application: | Magnetospheric research, Amateur communication |
Operator: | |
Contractors: | Space Research Institute (IKI) |
Equipment: | particle analyzer, electrical field analyzer, electrical field flux-gate magnetometer |
Configuration: | Hexagonal prism, 4 solar arrays, 2 m gravity gradient boom |
Propulsion: | None |
Power: | 4 deployable solar arrays, batteries |
Lifetime: | |
Mass: | 21 kg |
Orbit: | 385 km × 388 km, 51.6° |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
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Kolibri 2000 (RS 21) | 2001-051C | 26.11.2001 | Ba LC-1/5 | Soyuz-FG | with Progress-M1 7 |