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Our NanoSat power system has been designed to meet the needs of low cost, low power missions.
The architecture is configured such that it can meet a variety of solar panel configurations and is compatible with most rechargeable battery systems, including lithium ion/polymer. A maximum power point tracking scheme is employed to maximise precious array power and the system has the ability to combine solar arrays of differing technologies and string lengths.
Track record: SNAP-1* and FalconSat-2*
NanoSat Power Datasheet: NanoSat Power
This subsystem is based on designs licensed from Surrey Satellite Technology Limited (SSTL). Subsystems for the missions marked '*' were developed and manufactured by SSTL alone. Clyde Space is wholly responsible for the development and manufacture of its subsystems and equipment.