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RT-23-3
N2O4/UDMH propellant rocket stage.

Status: Retired 1998. Thrust: 206.00 kN (46,310 lbf). Gross mass: 15,000 kg (33,000 lb). Height: 3.60 m (11.80 ft). Diameter: 2.40 m (7.80 ft).

Country: Russia. Engines: RD-866. Launch Vehicles: RT-23 15Zh44, RT-23U 15Zh60, RT-23 15Zh52, RT-23U 15Zh61. Propellants: N2O4/UDMH. Agency: Yuzhnoye.
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