15D23

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Model: 15D23. Gross Mass: 34,600 kg (76,200 lb). Empty Mass: 4,000 kg (8,800 lb). Thrust (vac): 893.000 kN (200,754 lbf). Burn time: 75 sec. Propellants: Solid. Diameter: 1.84 m (6.03 ft). Length: 8.70 m (28.50 ft). Country: Russia. No Engines: 1. Motor: 15D23. Status: Retired 1992. Used as: RT-2. Release conditions: OKB-1. Model: 15D23P. Gross Mass: 34,550 kg (76,160 lb). Empty Mass: 3,750 kg (8,260 lb). Thrust (vac): 980.000 kN (220,310 lbf). Burn time: 75 sec. Propellants: Solid. Diameter: 1.84 m (6.03 ft). Length: 9.20 m (30.10 ft). Country: Russia. No Engines: 1. Motor: 15D23P. Status: Retired 1974. First Flight: 1969. Last Flight: 1974. No Launched: 4. Used as: RT-2. Release conditions: Arsenal. Used on Launch Vehicles: RT-2. 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.