RT-23-3

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Model: RT-23-3. Gross Mass: 15,000 kg (33,000 lb). Thrust (vac): 206.000 kN (46,310 lbf). Propellants: N2O4/UDMH. Diameter: 2.40 m (7.80 ft). Length: 3.60 m (11.80 ft). Country: Russia. No Engines: 1. Motor: RD-866. Status: Retired 1998. First Flight: 1982. Last Flight: 1998. No Launched: 20. Used as: RT-23.St3. Release conditions: Yuzhnoe. Used on Launch Vehicles: RT-23. 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.