Status: Out of Production. Date: 1995. Thrust: 850.40 kN (191,178 lbf). Unfuelled mass: 1,080 kg (2,380 lb). Specific impulse: 331 s. Specific impulse sea level: 304 s. Height: 2.44 m (7.99 ft). Diameter: 1.40 m (4.50 ft).
Engine: 1,080 kg (2,380 lb). Chamber Pressure: 176.30 bar. Area Ratio: 4.96. Thrust to Weight Ratio: 80.29. Oxidizer to Fuel Ratio: 2.6.
Country: Russia. Propellants: Lox/Kerosene. Agency: Glushko bureau. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9RetroSearch is an open source project built by @garambo | Open a GitHub Issue
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