R-7 Block ABVG

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R-7 aft end

Credit - © Mark Wade

Model: Soyuz M-0. Gross Mass: 42,200 kg (93,000 lb). Empty Mass: 3,000 kg (6,600 lb). Thrust (vac): 872.000 kN (196,033 lbf). Isp: 336 sec. Burn time: 145 sec. Propellants: Lox/Kerosene. Isp(sl): 298 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 20.00 m (65.00 ft). Country: Russia. No Engines: 1. Motor: RD-120K. Status: Development ended 2000. Last Flight: 0. No Launched: 0.

Model: R-7 8K71-0. Gross Mass: 43,100 kg (95,000 lb). Empty Mass: 3,500 kg (7,700 lb). Thrust (vac): 970.000 kN (218,060 lbf). Isp: 306 sec. Burn time: 120 sec. Propellants: Lox/Kerosene. Isp(sl): 250 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 19.00 m (62.00 ft). Country: Russia. No Engines: 1. Motor: RD-107-8D74. Status: Retired 1961. Cost $ : 5.000 million. First Flight: 1951. Last Flight: 1961. No Launched: 208. No Failed: 2.

Model: Vostok 8K72-0. Gross Mass: 43,300 kg (95,400 lb). Empty Mass: 3,710 kg (8,170 lb). Thrust (vac): 970.000 kN (218,060 lbf). Isp: 312 sec. Burn time: 120 sec. Propellants: Lox/Kerosene. Isp(sl): 254 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 19.00 m (62.00 ft). Country: Russia. No Engines: 1. Motor: RD-107-8D74. Status: Retired 1960. Cost $ : 5.000 million. First Flight: 1956. Last Flight: 1960. No Launched: 24. No Failed: 1.

Model: Luna 8K72-0. Gross Mass: 43,400 kg (95,600 lb). Empty Mass: 3,800 kg (8,300 lb). Thrust (vac): 990.000 kN (222,560 lbf). Isp: 312 sec. Burn time: 120 sec. Propellants: Lox/Kerosene. Isp(sl): 254 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 19.00 m (62.00 ft). Country: Russia. No Engines: 1. Motor: RD-107-8D74-1958. Status: Retired 1960. Cost $ : 5.000 million. First Flight: 1957. Last Flight: 1960. No Launched: 56. No Failed: 2.

Model: R-7A 8K74-0. Gross Mass: 42,800 kg (94,300 lb). Empty Mass: 3,200 kg (7,000 lb). Thrust (vac): 995.300 kN (223,752 lbf). Isp: 313 sec. Burn time: 120 sec. Propellants: Lox/Kerosene. Isp(sl): 256 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 19.00 m (62.00 ft). Country: Russia. No Engines: 1. Motor: RD-107-8D74K. Status: Retired 1967. Cost $ : 5.000 million. First Flight: 1957. Last Flight: 1967. No Launched: 132.

Model: Vostok 8A92-0. Gross Mass: 43,300 kg (95,400 lb). Empty Mass: 3,700 kg (8,100 lb). Thrust (vac): 995.300 kN (223,752 lbf). Isp: 313 sec. Burn time: 118 sec. Propellants: Lox/Kerosene. Isp(sl): 256 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 19.00 m (62.00 ft). Country: Russia. No Engines: 1. Motor: RD-107-8D74K. Status: Retired 1967. Cost $ : 5.000 million. First Flight: 1958. Last Flight: 1967. No Launched: 296. No Failed: 3.

Model: Vostok 8K72K-0. Gross Mass: 43,300 kg (95,400 lb). Empty Mass: 3,710 kg (8,170 lb). Thrust (vac): 970.000 kN (218,060 lbf). Isp: 313 sec. Burn time: 118 sec. Propellants: Lox/Kerosene. Isp(sl): 256 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 19.00 m (62.00 ft). Country: Russia. No Engines: 1. Motor: RD-107-8D74-1959. Status: Retired 1964. Cost $ : 5.000 million. First Flight: 1960. Last Flight: 1964. No Launched: 68.

Model: Voskhod 11A57-0. Gross Mass: 43,400 kg (95,600 lb). Empty Mass: 3,800 kg (8,300 lb). Thrust (vac): 995.300 kN (223,752 lbf). Isp: 314 sec. Burn time: 119 sec. Propellants: Lox/Kerosene. Isp(sl): 257 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 19.00 m (62.00 ft). Country: Russia. No Engines: 1. Motor: RD-107-8D74K. Status: Retired 1976. Cost $ : 5.000 million. First Flight: 1962. Last Flight: 1976. No Launched: 1356.

Model: Soyuz 11A511-0. Gross Mass: 43,000 kg (94,000 lb). Empty Mass: 3,550 kg (7,820 lb). Thrust (vac): 994.300 kN (223,528 lbf). Isp: 314 sec. Burn time: 118 sec. Propellants: Lox/Kerosene. Isp(sl): 257 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 19.60 m (64.30 ft). Country: Russia. No Engines: 1. Motor: RD-107-11D511. Status: Retired 1975. Cost $ : 5.000 million. First Flight: 1962. Last Flight: 1975. No Launched: 144. Other designations: 11S59 Blocks A,B,V,G.

Model: Molniya 8K78-0. Gross Mass: 43,400 kg (95,600 lb). Empty Mass: 3,800 kg (8,300 lb). Thrust (vac): 995.300 kN (223,752 lbf). Isp: 314 sec. Burn time: 119 sec. Propellants: Lox/Kerosene. Isp(sl): 257 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 19.00 m (62.00 ft). Country: Russia. No Engines: 1. Motor: RD-107-8D74K. Status: Retired 1965. Cost $ : 5.000 million. First Flight: 1963. Last Flight: 1965. No Launched: 16.

Model: Molniya 8K78M-0. Gross Mass: 43,400 kg (95,600 lb). Empty Mass: 3,770 kg (8,310 lb). Thrust (vac): 995.300 kN (223,752 lbf). Isp: 314 sec. Burn time: 119 sec. Propellants: Lox/Kerosene. Isp(sl): 257 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 19.00 m (62.00 ft). Country: Russia. No Engines: 1. Motor: RD-107-8D728. Status: Active. Cost $ : 5.000 million. First Flight: 1964. Last Flight: 2007. No Launched: 4268.

Model: Vostok 8A92M-0. Gross Mass: 43,300 kg (95,400 lb). Empty Mass: 3,700 kg (8,100 lb). Thrust (vac): 995.300 kN (223,752 lbf). Isp: 313 sec. Burn time: 120 sec. Propellants: Lox/Kerosene. Isp(sl): 256 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 19.00 m (62.00 ft). Country: Russia. No Engines: 1. Motor: RD-107-8D74K. Status: Retired 1991. Cost $ : 5.000 million. First Flight: 1964. Last Flight: 1991. No Launched: 380. No Failed: 1.

Model: Soyuz 11A511U2-0. Gross Mass: 42,810 kg (94,370 lb). Empty Mass: 3,550 kg (7,820 lb). Thrust (vac): 996.300 kN (223,977 lbf). Isp: 314 sec. Burn time: 118 sec. Propellants: Lox/Kerosene. Isp(sl): 257 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 19.60 m (64.30 ft). Country: Russia. No Engines: 1. Motor: RD-107-11D511P. Status: Retired 1996. Cost $ : 5.000 million. First Flight: 1975. Last Flight: 1996. No Launched: 416.

Model: Soyuz ST-0. Gross Mass: 44,400 kg (97,800 lb). Empty Mass: 3,810 kg (8,390 lb). Thrust (vac): 1,021.097 kN (229,552 lbf). Isp: 310 sec. Burn time: 120 sec. Propellants: Lox/Kerosene. Isp(sl): 264 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 19.60 m (64.30 ft). Country: Russia. No Engines: 1. Motor: RD-117. Status: In production. First Flight: 2001. Last Flight: 2007. No Launched: 132.

Gross mass includes 1190 kg of hydrogen peroxide and 280 kg of liquid nitrogen expended during ascent but not contributing to propulsion.

Model: Soyuz 11A511U-0. Gross Mass: 44,500 kg (98,100 lb). Empty Mass: 3,784 kg (8,342 lb). Thrust (vac): 994.300 kN (223,528 lbf). Isp: 310 sec. Burn time: 120 sec. Propellants: Lox/Kerosene. Isp(sl): 264 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 19.60 m (64.30 ft). Country: Russia. No Engines: 1. Motor: RD-107-11D511. Status: Design 2000. Cost $ : 5.000 million. First Flight: 2003. Last Flight: 2007. No Launched: 112.

Gross mass includes 1190 kg of hydrogen peroxide and 280 kg of liquid nitrogen expended during ascent but not contributing to propulsion.

Used on Launch Vehicles:

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