| 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. |
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