Mission Requirements
| Index | Domain | Description |
|---|---|---|
| M-0010 | General | The satellite will be launched in a LEO orbit corresponding to both its purpose and the international regulations. |
| M-0020 | General | The satellite must not contain entry resistant materials or completely detachable sections or appendages. |
| M-0030 | General | To comply with ESA's zero debris approach the satellite must reenter in less than 5 years. |
| M-0040 | General | The satellite must be able to control its attitude in case of payload acquisition requirements as well as high temperatures. |
| M-0100 | Structural | The satellite must abide to both its class' available standard, as well as the regulations imposed by the deployer entity. |
| M-0110 | Structural | The satellite must have all its deployable elements safely stowed during transport, storage and launch. |
| M-0120 | Structural | The satellite must be capable of of starting and using all its systems and appendices in a controlled manner. |
| M-0210 | Electronic | The satellite must keep its power source disconnected from all its subsystems during transport, storage and launch. |
| M-0220 | Electronic | The satellite must be capable of satisfactory harvesting all the necessary power during its entire lifespan. |
| M-0230 | Electronic | The satellite must regulate all its power and data lines, providing protection against potential electrical hazards. |
| M-0300 | Computational | The satellite must maintain complete control of its circuitry, data processes, communications, payloads and physical interfaces at all times. |
| M-0310 | Computational | The satellite must be able to store both the information obtained from payloads as well as telemetry: location, date, battery level, temperature, current and voltage in key nodes. |
| M-0400 | Communications | The satellite must be able to communicate and receive telecommands from both the ground station and other satellites. |
| M-0410 | Communications | The satellite must be able to maintain a satisfactory link budget and to allow control of the satellite by way of telecommands. |
| M-0420 | Communications | The satellite must be able to transmit and receive without an attitude requirement. |