The X-SAT Mercury Class from Blue Canyon Technologies is a Microsatellite Bus that is suited for operation in LEO (> 5 years), GEO (> 2 years), and Deep Space (> 2 years) missions. It has a payload mass capability of 40 kg and a payload volume of 14 x 17 x17 inches. This microsat bus has a pointing accuracy of ±0.002° (1-sigma), 3 axes, and 2 trackers. It requires a solar array power of 108 W and has an energy storage of 20.4 Ah.
