Izotov LK-700

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Engine Model: Izotov LK-700. Designer: Izotov. Developed in: 1966-69. Application: LK-700. Propellants: N2O4/UDMH. Thrust(vac): 131.000 kN (29,449 lbf). Chambers: 1. Country: Russia. Status: Developed 1966-69. 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.