Engine Model: Talos Mk 11 Mod 2. Designer: Hercules. Gross Mass: 1,500 kg (3,300 lb). Propellants: Solid. Thrust(vac): 516.000 kN (116,001 lbf). Burn time: 5.20 sec. Diameter: 0.76 m (2.49 ft). Length: 3.40 m (11.10 ft). Country: USA. The Talos motor was fitted with a conical adapter for mating to the second stage. Differential drag forces caused separation. Four fins were arranged at the aft end in a cruciform configuration and drove the vehicle to approximately one revolution per second burnout roll rate.
Talos Mk 11 Mod 2 used on Rocket Stages