CryoSat-2 - eoPortal Directory - Satellite MissionsExplore further
2018-5-2u2002·u2002The S/C mass is about 720 kg (including 36 kg propellant), the design life is 3.5 years (goal of 5.5 years). Spacecraft power generation is provided by two triple-junction GaAs solar arrays with an efficiency of 27.5% (two oriented solar panels), each panel provides power of …
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