The RD-0243 (Russian: Ракетный Двигатель-0243, romanized: Raketnyy Dvigatel-0243, lit. 'Rocket Engine 0243') is a propulsion module composed of an RD-0244 main engine and a RD-0245 vernier thruster. Both are liquid-fuel rocket engines, burning a hypergolic mixture of unsymmetrical dimethylhydrazine (UDMH) fuel with dinitrogen tetroxide (N2O4) oxidizer. The RD-0244 main engine operates in the oxidizer rich staged combustion cycle, while the vernier RD-0245 uses the simpler gas generator cycle. Since volume is at a premium on submarine launches, this module is submerged on the propellant tank.[3] Its development period was from 1977 to 1985, having had its first launch on December 27, 1981. Originally developed for the RSM-54, it was used later for the Shtil'.[1]
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| Liquid fuel
 | | Cryogenic | | Hydrolox (LH2 / LOX)
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 | Methalox (CH4 / LOX)
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 | Semi- cryogenic
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NK-15NK-33, 44RD-58RD-0105, 0109RD-0107, 0108, 0110RD-0110RRD-0124RD-107, 108, 117, 118RD-120RD-170, 171RD-180RD-191, 151, 181RD-193S1.5400
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 | Storable | | Hypergolic (Aerozine, UH 25, MMH, or UDMH
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17D61RD-0202 to 0206, 0208 to 0213RD-0207, 0214RD-0216, 0217, 0235RD-0233, 0234RD-0236RD-0237RD-0255 to 0257RD-215 to 219RD-250 to 252, 261, 262RD-253, 275RD-263, 268, 273RD-270S5.92S5.98M
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 | Other |  | 
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| Solid fuel
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* Different versions of the engine use different propellant combinationsEngines in italics are under development
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