R-36M2-3 (original) (raw)

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R-36M2-3

N2O4/UDMH propellant rocket stage. Main engine could be throttled to 800 kgf.

Status: Active. Thrust: 18.60 kN (4,181 lbf). Gross mass: 4,266 kg (9,404 lb). Unfuelled mass: 2,356 kg (5,194 lb). Specific impulse: 317 s. Burn time: 1,000 s. Height: 1.00 m (3.20 ft). Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft).

Country: Ukraine. Engines: RD-869. Launch Vehicles: R-36MU 15A18, R-36M2 15A18M, Dnepr. Propellants: N2O4/UDMH.

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