S2.726

home topic index

Engine Model: S2.726. Designer: SKB-30. Propellants: Nitric acid/Amine. Thrust(vac): 103.000 kN (23,155 lbf). Country: Russia. S2.726 used on Rocket Stages Used on stage: V-1000-1. on launch vehicle: V-1000. 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.