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UR-200-2

RD-0205 8D46

RD-0205 8D46
RD-0205 8D46 on stage 8S816 (UR-200)
Credit: © Mark Wade

N2O4/UDMH propellant rocket stage. TsNIIMash has 1:10 structural simulation model. Developed 1960-1965. Orevo has sectioned hardware. All data accurate except empty mass prorated between first and second stages.

AKA: 8K81 Stage 2. Status: Retired 2007. Thrust: 612.90 kN (137,785 lbf). Gross mass: 25,810 kg (56,900 lb). Unfuelled mass: 2,400 kg (5,200 lb). Specific impulse: 322 s. Burn time: 113 s. Height: 10.00 m (32.00 ft). Diameter: 2.20 m (7.20 ft). Span: 2.20 m (7.20 ft).



Country: Russia. Engines: RD-0205, RD-0206, RD-0207. Launch Vehicles: Initial UR-500, UR-200, UR-200A, Proton-K/DM-2, Proton-K/DM-2M. Propellants: N2O4/UDMH.

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