Kartukov LL

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Engine Model: Kartukov LL. Designer: Kartukov. Developed in: 1946-48. Application: LL-1, LL-2, LL-3. Propellants: Solid. Thrust(vac): 14.700 kN (3,305 lbf). Country: Russia. Status: Developed 1946-48. 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.