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N1 Block V-II
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Gross Mass: 805,000 kg (1,774,000 lb). Empty Mass: 115,000 kg (253,000 lb). Thrust (vac): 7,840.000 kN (1,762,500 lbf). Isp: 440 sec. Burn time: 380 sec. Propellants: Lox/LH2. Diameter: 10.00 m (32.00 ft). Span: 10.00 m (32.00 ft). Length: 50.00 m (164.00 ft). Country: Russia. No Engines: 4. Engine: NK-15VM. Status: Study 1965. N1 improvement study, 1965. Lox/LH2 replacement for Block B second stage.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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