 Artist's impression ofHayabusa2firing its ion thrusters |
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Mission type | Asteroid sample-return |
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Operator | JAXA |
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COSPAR ID | 2014-076A |
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SATCATno. | 40319 |
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Website | www.hayabusa2.jaxa.jp/en/ |
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Mission duration | 6 years (planned) (7 years, 6 months and 29 days elapsed) |
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Spacecraft type | Hayabusa |
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Manufacturer | NEC |
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Launch mass | 610 kg (1,340 lb) |
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Dry mass | 490 kg (1,080 lb) |
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Dimensions | Spacecraft bus: 1 × 1.6 × 1.25 m (3 ft 3 in × 5 ft 3 in × 4 ft 1 in) Solar panel: 6 m × 4.23 m (19.7 ft × 13.9 ft) |
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Power | 2.6 kW (at 1 au), 1.4 kW (at 1.4 au) |
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Launch date | 3 December 2014, 04:22:04 UTC |
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Rocket | H-IIA 202 |
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Launch site | Tanegashima Space Center, LA-Y |
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Contractor | Mitsubishi Heavy Industries |
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Landing date | Re-entry capsule: 5 December 2020 UTC |
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Landing site | Woomera, Australia |
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Closest approach | 3 December 2015 |
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Distance | 3,090 km (1,920 mi) |
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Arrival date | 27 June 2018, 09:35 UTC |
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Departure date | 12 November 2019 |
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Sample mass | 5.4 grams(including gas samples) |
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Landing date | 21 February 2019 |
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Landing date | 11 July 2019 |
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Closest approach | 5 December 2020 UTC |
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