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Related: How do single engine rockets control roll?

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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?

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    $\begingroup$ I'll point you to this answer. While the question was about attitude, the answer also addresses roll. Similar controls can be seen on one of the rockets you mentioned, the Soyuz-2-1v, which use RD-0110R as Vernier thrusters. $\endgroup$
    – Das_Geek
    Feb 26, 2020 at 22:01
  • $\begingroup$ A modified 0110 is used as veriners??? I need to see a diagram or something because I have NO clue how that would look. Did they just cut out the -0110 turbopump veriner system and weld it around the -193? $\endgroup$ Feb 26, 2020 at 22:08
  • $\begingroup$ @neph kosmonavtika.com/lanceurs/soyouz/version/14A15/fig1-1.jpg $\endgroup$ Feb 26, 2020 at 22:51
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    $\begingroup$ @OrganicMarble new SpaceForce! policy $\endgroup$
    – uhoh
    Feb 27, 2020 at 0:47
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    $\begingroup$ The problem with these kinds of questions is that one will not get a complete answer. ITAR, along with its equivalents in Europe, Russia, China, and India, is stupid in many ways, but there it is, and it is there, accompanied with threats of lengthy amounts of jail time. $\endgroup$ Feb 27, 2020 at 3:42

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