
Dawn CubeSat Propulsion Module
Dawn Aerospace
The EnduroSat CubeSat Electric Power System (EPS I) has the highest power efficiency in its class. It supports a wide range of outputs making it a versatile solution fully compliant with the CubeSat standard. Our CubeSat EPS module has flight heritage, including the ISS-level requirements.
Features:
Includes:
Qualification:
Space qualification tests are performed on the Qualification Engineering Model. Qualification test levels and duration will follow the ESA standard ECSS-E-ST-10-03C and GEVS: GSFC-STD-7000A.
Parameter | Value |
---|---|
Input Voltage | up to 5.5 V per channel |
Input Current | up to 1.8 A per channel |
Number of Channels | 3 |
Battery Power | 10.2 Wh |
Battery Voltage | 3.7 V nominal |
Power Consumption | 20 mA @3.7 V |
Power Output | 3.3 V |
Power Output | 5 V |
Power Output | BCR (5 V max) |
Interface | UART |
Interface | I2C |
Interface | USB |
Mass | 208 g |
The EnduroSat CubeSat Electric Power System (EPS I) has the highest power efficiency in its class. It supports a wide range of outputs making it a versatile solution fully compliant with the CubeSat standard. Our CubeSat EPS module has flight heritage, including the ISS-level requirements.
Features:
Includes:
Qualification:
Space qualification tests are performed on the Qualification Engineering Model. Qualification test levels and duration will follow the ESA standard ECSS-E-ST-10-03C and GEVS: GSFC-STD-7000A.