RT-2-1

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Engine Model: RT-2-1. Designer: OKB-1. Propellants: Solid. Thrust(vac): 900.000 kN (202,320 lbf). Burn time: 30 sec. Diameter: 1.95 m (6.39 ft). Length: 4.80 m (15.70 ft). Country: Russia. RT-2-1 used on Rocket Stages Used on stage: RT-1. on launch vehicle: Bulava. Used on stage: RT-1. on launch vehicle: Pioner. Used on stage: RT-1. on launch vehicle: RT-1. Used on stage: RT-1. on launch vehicle: RT-23. Used on stage: RT-1. on launch vehicle: Temp-2S. Used on stage: RT-1. on launch vehicle: Topol. 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.