CHEOPS
Spacecraft propulsion supplied by ArianeGroup
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CHEOPS
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Category | Astronomy |
| Operator | DLR, CNES | |
| Orbit | SSO | |
| Sat position | 800 kms | |
| Launch date | 2017 | |
| Launch mass | - | |
| Design life | 3.5 years | |
| Launcher | - | |
| Satellite / Bus | Myriade Evolutions | |
| Manufacturer | SSTL (competitive design phase) | |
| Orbital Propulsion Centre Contribution
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4x 1 N hydrazine thrusters
