VELOX P1, P2 (original) (raw)
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VELOX-P2 [TU M�nchen]
VELOX-P is a 1U CubeSat mission by Nanyang Technological University, Singapore, to develop and orbit a CubeSat for technology demonstration, to test in-house attitude determination and control system, power subsystem, and to support a dual-FOV sun sensor payload. The Cubesat VELOX Pwill be launched into experimental high inclination circular orbit at 300 km on an Interorbital Neptune flight from off-shore California with a number of other spacecraft. For its 8-12 weeks in orbit, VELOX P will log telemetry data from its various subsystems and send them down to our mission control center for analysis. As the Neptune launch vehicle is much delayed, a launch date can not be estimated.
VELOX-P2 is also 1U cubesat mission for technology demonstration to test in house ADAC system, power sub-system and to support a dual FOV suns sensor payload.
| Nation: | Singapore |
|---|---|
| Type / Application: | Technology |
| Operator: | Nanyang Technological University, Singapore |
| Contractors: | Nanyang Technological University, Singapore |
| Equipment: | |
| Configuration: | CubeSat (1U) |
| Propulsion: | None |
| Power: | Solar cells, batteries |
| Lifetime: | |
| Mass: | 1 kg |
| Orbit: | 593 km × 699 km, 97.80� (#2) |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks |
|---|---|---|---|---|---|
| VELOX-P | - | ? | Neptune | with ? | |
| VELOX P2 | 2013-066Y | 21.11.2013 | Do LC-370/13 | Dnepr | with DubaiSat 2, STSAT 3, WNISAT 1, SkySat 1, BRITE-PL, AprizeSat 7, AprizeSat 8, UniSat 5, Delfi-n3Xt, Dove 3, Dove 4, Triton 1, CINEMA 2, CINEMA 3, CubeBug 2, GOMX 1, NEE 02 Krysaor, FUNcube 1, HiNCube, ZACUBE 1, ICUBE 1, HumSat-D, PUCP-SAT 1, First-MOVE, UWE 3, Pocket-PUCP, BeakerSat 1, QubeScout S1, $50SAT, Wren, BPA 3 |