| N1 Block Sr |
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Upper stage / space tug - developed 1971-1974 to support manned lunar expedition. Replaced Blok R/Blok S previously under development. Capable of five restarts and 11 days of flight. Could insert 24 metric tons into lunar orbit or 20 metric tons into geosynchronous orbit. Length: 16.50 m (54.10 ft). Basic Diameter: 5.20 m (17.00 ft). Span: 5.20 m (17.00 ft). Mass: 77,900 kg (171,700 lb). Main Engine: RD-56M. Main Engine Thrust: 147.880 kN (33,245 lbf). Main Engine Propellants: Lox/LH2. Main Engine Propellants: 66,400 kg (146,300 lb). Main Engine Isp: 441 sec. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |