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N1M 1965 - B
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Gross Mass: 620,000 kg (1,360,000 lb). Empty Mass: 75,000 kg (165,000 lb). Thrust (vac): 21,960.000 kN (4,936,800 lbf). Isp: 346 sec. Burn time: 85 sec. Propellants: Lox/Kerosene. Diameter: 6.80 m (22.30 ft). Span: 9.80 m (32.10 ft). Length: 30.00 m (98.00 ft). Country: Russia. No Engines: 8. Engine: 11D52M. Status: Study 1965. As per N1 improvement study, 1965. Further stretch of Block B and thrust increased again to 280 tonnes per engine.
Used on Launch Vehicles:
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