UPMSat 2 (original) (raw)
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UPMSat 2 [UPM]
The UPMSat 2 (Universidad Polit�cnica de Madrid Satellite 2) is an educational, scientific and in-orbit technological demonstration satellite built by the Technical University of Madrid � Universidad Politecnica de Madrid (UPM)
Its prime objective is to give students the competences for designing, building, testing, integrating, and operating a small satellite, but whose execution involves all the complexity of a complete space system.
The platform has a volume of 0.5 × 0.5 × 0,6 m3, of which about 40% are available for payloads, and a total mass of about 50 kg. It will operate in a Sun-synchronous orbit at 600 km.
| Nation: | Spain |
|---|---|
| Type / Application: | Technology |
| Operator: | Universidad Polit�cnica de Madrid Satellite |
| Contractors: | IRD / Universidad Polit�cnica de Madrid Satellite |
| Equipment: | |
| Configuration: | |
| Propulsion: | |
| Power: | Solar cells, batteries |
| Lifetime: | 2 years |
| Mass: | 45 kg |
| Orbit: | 517 km � 518 km, 97.46� |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks |
|---|---|---|---|---|---|
| UPMSat 2 | 2020-061E | 03.09.2020 | Ko ELV | Vega | with Athena, ION-SCV 1, ESAIL, NEMO-HD, �uSat 6, GHGSat C1, Flock-4v 1, ..., 26, Lemur-2 112, ..., 119, SpaceBEE 10, ..., 21, FSSCat A, B, NAPA 1, TARS, EG 2, OSM 1 CICERO, DIDO 3, PICASSO, SIMBA, TRISAT, AMICal-Sat, TT�100 |
References:
- F. Caramelli, F. Battie, A. Scaccia, S. Corbo, A. Dalloneau, F. Fabiani et al.: The first Vega ride-share mission flight