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R-36-1
AKA: R-36--1. Status: Retired 1975. Thrust: 2,651.70 kN (596,126 lbf). Gross mass: 122,300 kg (269,600 lb). Unfuelled mass: 6,400 kg (14,100 lb). Specific impulse: 301 s. Specific impulse sea level: 269 s. Burn time: 120 s. Height: 18.90 m (62.00 ft). Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft).
Cost $ : 6.000 million.
| R-36-0-1 N2O4/UDMH propellant rocket stage. . |
| R-36M-1 N2O4/UDMH rocket stage. 4522.00 kN (1,016,586 lbf) thrust. Mass 210,000 kg (462,971 lb). |
| Tsyklon 2-1 N2O4/UDMH propellant rocket stage. SL-11; 11K68;R-36M. |
| Tsyklon 3-1 N2O4/UDMH propellant rocket stage. SL-14;11K69. |
Country: Ukraine. Engines: RD-251. 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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