Problem: Larger missions require higher performance for orbital maneuvers. Solution: The GO-2 system is designed to be modular, allowing for multiple units to be stacked together for higher thrust solutions. GO-2 Insights: For larger missions, GO-2's stackable design allows for multiple systems to be integrated into the same spacecraft. Up to 2.4 mN to thrust (with the 6-cluster), ideal for larger satellite platforms. Example configurations: Config (# of GO-2's) 2 4

GO-2 delivers continuous, adjustable, and differential low thrust to enable smooth, precise translational and rotational control. This supports safer, more accurate, RPO profiles, from precise phasing to final approach and station-keeping.

Problem: You need small, reliable nudges to stay clear of other satellites and orbital debris and to keep your ground track tight. Solution: Continuous low thrust keeps you on-slot and out of harm’s way, without disruption to your mission. GO-2 Insights: Maintain continuous, precise thrust without interrupting your primary mission. Max out thrust for quicker phasing or collision avoidance. Operate at the lower end of the thrust range for ultra-fine, continuous grou

Problem: High resolution imagers need high pointing accuracy with tight jitter control and rapid retargeting; reaction wheels alone can saturate or inject jitter. Solution: GO-2 provides continuous, adjustable low thrust to offload reaction wheels, damp jitter, and provides precise pointing with high pointing accuracy. GO-2 Insights: Fine thrust control and throttling across 5-400 μN with a minimum impulse bit of around 800 nNs enables gentle control during imaging wi

Problem: LEO missions must meet 5-years post-mission disposal rules; using just drag can often be too slow. Solution: Use GO-2's large total impulse (up to –12.4 kNs) for an efficient and safe deorbit well within compliance. GO-2 Insights: Ideal for decommissioning satellites ranging from 6U to hundreds of kilograms small sats; satellites can decommission over many months to their desired altitude given the GO-2's long lifetime. If necessary, GO-2's can be stacked wi