UWE-3
Description
UWE-3 is a 1U CubeSat from the University of Wuerzburg demonstrating a modular, fault-tolerant satellite bus and a real-time miniature attitude determination and control system using magnetorquers and a reaction wheel, becoming one of the longest-operating picosatellites of its class.
Specifications
| Mass | approx. 1 kg |
|---|---|
| Form factor | 1U CubeSat, 10 x 10 x 10 cm |
| Orbit | Sun-synchronous LEO, ~592 x 693 km, 97.76 deg inclination |
| Launch date | 2013-11-21 |
| Launch vehicle | Dnepr |
| Payload | Real-time attitude determination and control system (magnetorquers, reaction wheel, sensors) |