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Model: RT-1-1. Thrust (vac): 900.000 kN (202,320 lbf). Burn time: 30 sec. Propellants: Solid. Diameter: 1.95 m (6.39 ft). Length: 4.80 m (15.70 ft). Country: Russia. No Engines: 1. Motor: RT-2-1. Status: Retired 1965. Used as: RT-2. Release conditions: OKB-1.

Model: Temp-2S-1. Gross Mass: 26,600 kg (58,600 lb). Propellants: Solid. Diameter: 1.79 m (5.87 ft). Length: 8.60 m (28.20 ft). Country: Russia. No Engines: 1. Motor: RD RT-21 (1). Status: Retired 1991. Used as: Temp-2S. Release conditions: MITT.

Model: Start-1. Gross Mass: 26,000 kg (57,000 lb). Empty Mass: 3,000 kg (6,600 lb). Thrust (vac): 980.000 kN (220,310 lbf). Isp: 263 sec. Burn time: 60 sec. Propellants: Solid. Isp(sl): 238 sec. Diameter: 1.61 m (5.28 ft). Span: 1.61 m (5.28 ft). Length: 8.50 m (27.80 ft). Country: Russia. No Engines: 1. Motor: MIHT-1. Status: Active. Cost $ : 4.000 million. First Flight: 1981. Last Flight: 2007. No Launched: 58.

All estimated

Model: 15D339. Gross Mass: 25,000 kg (55,000 lb). Thrust (vac): 1,050.000 kN (236,040 lbf). Propellants: Solid. Diameter: 2.40 m (7.80 ft). Length: 4.80 m (15.70 ft). Country: Russia. No Engines: 1. Motor: 15D339. Status: Retired 1998. First Flight: 1982. Last Flight: 1998. No Launched: 20. Used as: RT-23.St2. Release conditions: Yuzhnoe.

Model: Topol'-M-1. Gross Mass: 26,000 kg (57,000 lb). Empty Mass: 3,000 kg (6,600 lb). Thrust (vac): 980.000 kN (220,310 lbf). Burn time: 60 sec. Propellants: Solid. Diameter: 1.80 m (5.90 ft). Length: 8.50 m (27.80 ft). Country: Russia. No Engines: 1. Motor: 15Zh58A. Status: Active. First Flight: 1994. Last Flight: 2007. No Launched: 19. Used as: Topol. Other designations: Topol'-M1. Release conditions: MITT.

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