R-36M2-1 (original) (raw)

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R-36M2-1

Part of R-36-2

N2O4/UDMH propellant rocket stage. Surplus ICBMs; failures based on ICBM tests through 1994.

AKA: RS-20;SS-18 Satan. Status: Active. Thrust: 4,523.00 kN (1,016,810 lbf). Gross mass: 161,520 kg (356,090 lb). Unfuelled mass: 13,620 kg (30,020 lb). Specific impulse: 318 s. Specific impulse sea level: 293 s. Burn time: 130 s. Height: 22.30 m (73.10 ft). Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft).

Cost $ : 6.000 million.

Country: Ukraine. Engines: RD-264. Launch Vehicles: R-36MU 15A18, R-36M2 15A18M, Dnepr. Propellants: N2O4/UDMH.

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