E1P F2 |
USA |
Spacecraft n°: |
US spacecraft n°: |
Launch data:
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| Prime manufacturer | Montana Space Grant Consortium |
| Platform | CubeSat |
| Operator | Montana Space Grant Consortium |
| Mass at launch | 1 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | 0.1m in size |
| Equipment | |
| Solar array | Solar cells |
| Stabilization | |
| Propulsion | None |
| DC power | |
| Design lifetime |