miniGimbal-2X
- Angular Precision
- < 0.2 deg
- Angular Range
- 360 deg azimuth / 125 deg elevation
- Lifetime
- > 5 years (>65k cycles)
- RF Losses
- < 2.5db up to 28GHz
- Payload Mass
- up to 3Kg
- Operating Voltage Range
- -
- Volume
- -
- Mass
- -
A satellite equipped with a cluster of control-moment gyroscopes provides the necessary control authority to reorient the spacecraft between target acquisition and collection. A satellite of 100 kgm^2 of inertia is being considered for the following use case,
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