RT-3

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Model: RT-1-3. Gross Mass: 3,000 kg (6,600 lb). Thrust (vac): 240.000 kN (53,950 lbf). Burn time: 42 sec. Propellants: Solid. Diameter: 1.40 m (4.50 ft). Length: 2.80 m (9.10 ft). Country: Russia. No Engines: 1. Motor: RD RT-1-3. Status: Retired 1965. Used as: RT-1.St3. Release conditions: OKB-1. Model: Topol'-M-3. Gross Mass: 6,000 kg (13,200 lb). Empty Mass: 1,000 kg (2,200 lb). Thrust (vac): 245.000 kN (55,078 lbf). Burn time: 56 sec. Propellants: Solid. Diameter: 1.34 m (4.39 ft). Length: 3.10 m (10.10 ft). Country: Russia. No Engines: 1. Motor: 15Zh58V. Status: Active. First Flight: 1994. Last Flight: 2007. No Launched: 19. Used as: Topol.St3. Other designations: Topol'-M3. Release conditions: MITT. Used on Launch Vehicles: Bulava. RT-1. 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.