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R-36M2-2
Part of R-36-2 Family
N2O4/UDMH propellant rocket stage. Surplus ICBMs; failures based on ICBM tests through 1994.

Status: Active. Thrust: 760.00 kN (170,850 lbf). Gross mass: 41,114 kg (90,640 lb). Unfuelled mass: 4,374 kg (9,643 lb). Specific impulse: 340 s. Burn time: 190 s. Height: 5.70 m (18.70 ft). Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft).

Cost $ : 3.000 million.



Country: Ukraine. Engines: RD-0255. Launch Vehicles: R-36MU 15A18, R-36M2 15A18M, Dnepr. Propellants: N2O4/UDMH.

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