MicroMAS-2A |
USA |
Int. spacecraft nº: |
US spacecraft nº: |
Launch data:
|
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| Prime manufacturer | MIT Lincoln Lab. |
| Platform | 3U CubeSat |
| Operator | Massachusetts Institute of Technology - Space Systems Laboratory (MIT SSL) |
| Mass at launch | 5.5 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | 4 deployable fixed solar arrays |
| Stabilization | |
| Propulsion | None |
| DC power | |
| Design lifetime |
| Ref.: #7(JR745), #228 - update: 15.02.18 | Home |