R-36-1

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Model: R-36--1. Gross Mass: 122,300 kg (269,600 lb). Empty Mass: 6,400 kg (14,100 lb). Thrust (vac): 2,651.700 kN (596,126 lbf). Isp: 301 sec. Burn time: 120 sec. Propellants: N2O4/UDMH. Isp(sl): 269 sec. Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft). Length: 18.90 m (62.00 ft). Country: Ukraine. No Engines: 1. Motor: RD-251. Status: Retired 1975. Cost $ : 6.000 million. First Flight: 1963. Last Flight: 1975. No Launched: 157.

Verniers 4 x RD-68M, 285 kN, maximum 42 degree gimbal angle.

Model: R-36-0-1. Gross Mass: 125,000 kg (275,000 lb). Empty Mass: 8,500 kg (18,700 lb). Thrust (vac): 2,640.000 kN (593,490 lbf). Isp: 301 sec. Burn time: 120 sec. Propellants: N2O4/UDMH. Isp(sl): 269 sec. Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft). Length: 18.90 m (62.00 ft). Country: Ukraine. No Engines: 1. Motor: RD-251. Status: Retired 1971. Cost $ : 6.000 million. First Flight: 1965. Last Flight: 1971. No Launched: 26.

Model: Tsyklon 2-1. Gross Mass: 122,300 kg (269,600 lb). Empty Mass: 6,400 kg (14,100 lb). Thrust (vac): 2,640.000 kN (593,490 lbf). Isp: 301 sec. Burn time: 120 sec. Propellants: N2O4/UDMH. Isp(sl): 269 sec. Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft). Length: 18.90 m (62.00 ft). Country: Ukraine. No Engines: 1. Motor: RD-251. Status: Active. Cost $ : 6.000 million. First Flight: 1969. Last Flight: 2006. No Launched: 107. Other designations: 11S681.

SL-11; 11K68;R-36M

Model: Tsyklon 3-1. Gross Mass: 127,000 kg (279,000 lb). Empty Mass: 8,300 kg (18,200 lb). Thrust (vac): 3,032.000 kN (681,620 lbf). Isp: 301 sec. Burn time: 120 sec. Propellants: N2O4/UDMH. Isp(sl): 270 sec. Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft). Length: 18.75 m (61.51 ft). Country: Ukraine. No Engines: 1. Motor: RD-261. Status: Active. Cost $ : 6.000 million. First Flight: 1977. Last Flight: 2004. No Launched: 249. No Failed: 1. Other designations: 11S691.

SL-14;11K69

Model: R-36M2-1. Gross Mass: 161,520 kg (356,090 lb). Empty Mass: 13,620 kg (30,020 lb). Thrust (vac): 4,523.000 kN (1,016,810 lbf). Isp: 318 sec. Burn time: 130 sec. Propellants: N2O4/UDMH. Isp(sl): 293 sec. Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft). Length: 22.30 m (73.10 ft). Country: Ukraine. No Engines: 1. Motor: RD-264. Status: Active. Cost $ : 6.000 million. First Flight: 1977. Last Flight: 2007. No Launched: 125. No Failed: 1. Other designations: SS-18 Satan; RS-20.

Surplus ICBMs; failures based on ICBM tests through 1994.

Used on Launch Vehicles:

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