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R-21-1
N2O4/UDMH propellant rocket stage.

Status: Retired 1989. Gross mass: 16,600 kg (36,500 lb). Height: 12.00 m (39.00 ft). Diameter: 1.30 m (4.20 ft).

Country: Russia. Engines: RD R-21. Launch Vehicles: R-21. Propellants: N2O4/UDMH.
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