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Version 1
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Initial specifications and requirements
| Parameter | Requirements | Justification |
|---|
| Mechanical subsystem | | |
| Payload physical envelope | | |
| Payload mass | | |
| Power subsystem | | |
| Payload energy consumption | | |
| Downlink radio energy consumption | | |
| Peak power available | | |
| Communications | | |
| Downlink data rate (usable bits) | | |
| Downlink frequency band | | |
| Downlink power/EIRP needed | | |
| Launch and orbit | | |
| Orbit type | | |
| Orbit height | | |
| Orbit inclination | | |
| Other parameters | | |
| ADCS | | |
| Slewrate (max, precision) | | |
| Momentum budget | | |