Computer model of Rosetta | |
Mission type | Comet orbiter/lander |
---|---|
Operator | European Space Agency |
COSPAR ID | 2004-006A |
SATCAT № | 28169 |
Website | www.esa.int/rosetta |
Mission duration | 9 years, 11 months and 2 days elapsed |
Spacecraft properties | |
Manufacturer | Astrium |
Launch mass | Orbiter: 2,900 kg (6,400 lb) Lander: 100 kg (220 lb) |
Dry mass | Orbiter: 1,230 kg (2,710 lb) |
Payload mass | Orbiter: 165 kg (364 lb) Lander: 27 kg (60 lb) |
Dimensions | 2.8 × 2.1 × 2 m (9.2 × 6.9 × 6.6 ft) |
Power | 850 watts at 3.4 AU[1] |
Start of mission | |
Launch date | 2 March 2004, 07:17 UTC |
Rocket | Ariane 5G+ V-158 |
Launch site | Kourou ELA-3 |
Contractor | Arianespace |
Flyby of Mars | |
Closest approach | 25 February 2007 |
Distance | 250 km (160 mi) |
Flyby of 2867 Šteins | |
Closest approach | 5 September 2008, 20:38 UTC |
Distance | 800 km (500 mi) |
Flyby of 21 Lutetia | |
Closest approach | 10 July 2010, 16:10 UTC |
Distance | 3,162 km (1,965 mi) |
67P/Churyumov–Gerasimenko orbiter | |
Orbital insertion | May 2014 (planned) |
Orbit parameters | |
Periapsis | 200 km (120 mi) planned |
Transponders | |
Band | S band (low gain antenna) X band (high gain antenna) |
Bandwidth | 7.8 bit/s (S Band) 22 kbit/s (X Band)[2] |