RT-2

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Model: RT-1-2. Gross Mass: 10,000 kg (22,000 lb). Empty Mass: 1,500 kg (3,300 lb). Thrust (vac): 500.000 kN (112,400 lbf). Burn time: 30 sec. Propellants: Solid. Diameter: 1.49 m (4.88 ft). Length: 4.00 m (13.10 ft). Country: Russia. No Engines: 1. Motor: RD RT-15-2. Status: Retired 1965. Used as: RT-15. Release conditions: OKB-1. Model: Pioner-2. Gross Mass: 8,700 kg (19,100 lb). Propellants: Solid. Diameter: 1.47 m (4.82 ft). Length: 4.40 m (14.40 ft). Country: Russia. No Engines: 1. Motor: RD RT-21-2. Status: Retired 1991. Used as: RT-21.St2. Release conditions: MITT. Model: Temp-2S-3. Gross Mass: 8,700 kg (19,100 lb). Empty Mass: 1,000 kg (2,200 lb). Thrust (vac): 245.000 kN (55,078 lbf). Propellants: Solid. Diameter: 1.34 m (4.39 ft). Length: 3.90 m (12.70 ft). Country: Russia. No Engines: 1. Motor: RD RT-21-3. Status: Retired 1988. Used as: Topol.St3. Release conditions: MITT. Used on Launch Vehicles: Pioner. RT-1. Temp-2S. 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.