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| No. | Requirement | Reference / Reason |
|---|---|---|
| 1 | The payload must conform to the volume and shape of the 3U cubesat standard. | TODO (DTEG reference) Points |
| 2 | The payload must have a mass of at least 4kg (8.8lb) | TODO (DTEG reference) |
| 3 | A maximum of 20% of the payload mass can be non-functional. | TODO (DTEG reference) |
| 4 | The payload must not influence the flight of the rocket in any way. (It should be "replaceable with ballast mass"). | TODO (DTEG / HeroX reference) |
| 5 | The payload must be able to launch in a window of X hours maximum. | Can't reduce pad time requirements of rocket. |
| 6 | TODO all the deployable rules | Stem from Derived Requirements no. 17 |
Objective Requirements
Driven by the primary mission of the payload. Not necessary for a safe/legal flight, but necessary for a nominal experiment.
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