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Engine Model: 15Zh58V. Designer: MITT. Gross Mass: 6,000 kg (13,200 lb). Empty Mass: 1,000 kg (2,200 lb). Propellants: Solid. Thrust(vac): 245.000 kN (55,078 lbf). Burn time: 56 sec. Diameter: 1.34 m (4.39 ft). Length: 3.10 m (10.10 ft). Country: Russia.
Engine Model: RD RT-21-3. Designer: MITT. Gross Mass: 8,700 kg (19,100 lb). Empty Mass: 1,000 kg (2,200 lb). Propellants: Solid. Thrust(vac): 245.000 kN (55,078 lbf). Diameter: 1.34 m (4.39 ft). Length: 3.90 m (12.70 ft). Country: Russia.
RT-134 used on Rocket Stages
- Used on stage: RT-2. on launch vehicle: RT-1.
- Used on stage: RT-3. on launch vehicle: RT-1.
- Used on stage: RT-3. on launch vehicle: Topol.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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