Related: How do single engine rockets control roll?
While many single-nozzle rockets are gas generator powered & can deflect the pump exhaust asymmetrically to produce a torque, staged combustion motors cannot. For rockets like Zenit and Atlas V, which have multiple nozzles, this is no problem. However, rockets using a single nozzle staged combustion engine, such as the Naro-1 & Angara (RD-191), Soyuz-2-1v (RD-193), and similar, how is roll control provided?
