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R-36-2
Status: Retired 1975. Thrust: 940.40 kN (211,410 lbf). Gross mass: 49,300 kg (108,600 lb). Unfuelled mass: 3,700 kg (8,100 lb). Specific impulse: 317 s. Burn time: 160 s. Height: 9.40 m (30.80 ft). Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft).
Cost $ : 2.000 million.
| R-36-0-2 N2O4/UDMH propellant rocket stage. . |
| R-36M2-1 N2O4/UDMH propellant rocket stage. Surplus ICBMs; failures based on ICBM tests through 1994. |
| R-36M-2 N2O4/UDMH rocket stage. 760.00 kN (170,855 lbf) thrust. Mass 49,000 kg (108,027 lb). |
| R-36M2-2 N2O4/UDMH propellant rocket stage. Surplus ICBMs; failures based on ICBM tests through 1994. |
| Tsyklon 2-2 N2O4/UDMH propellant rocket stage. . |
| Tsyklon 3-2 N2O4/UDMH propellant rocket stage. . |
Country: Ukraine. Engines: RD-252. Launch Vehicles: R-36 8K67, Tsiklon, Tsiklon-2A, R-36 8K67M, R-36 8K67P, R-36 8K67MA, R-36 8K67PM. Propellants: N2O4/UDMH.
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