Delfi-C3 [Technical University of Delft]
Delfi-C3 is the first nanosatellite student project from the Technical University of Delft in the Netherlands. The satellite is based on the CubeSat concept and a number of novel technologies were tested on board the satellite:
After launch, the satellite received the designations DO 64 or Delfi-OSCAR 64.
Nation: | Netherlands |
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Type / Application: | Technology |
Operator: | Technical University of Delft |
Contractors: | Technical University of Delft; Pumpkin, Inc. (bus) |
Equipment: | |
Configuration: | CubeSat (3U) |
Propulsion: | None |
Power: | 4 deployable fixed solar arrays, batteries |
Lifetime: | 1 year (design); +6 years reached |
Mass: | 3 kg |
Orbit: | 615 km × 633 km, 97.99° |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
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Delfi C3 (DO 64, Delfi-OSCAR 64) | 2008-021G | 28.04.2008 | Sr SLP | PSLV-CA | with Cartosat 2A, IMS 1, CanX 6, CanX 2, AAUSAT 2, Cute 1.7 + APD II, COMPASS 1, SEEDS 2, Rubin 8-AIS |