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Thiokol 156
Thiokol solid rocket engine. Developed to 1966.

AKA: Thiokol 156 inch. Status: Developed to 1966. Thrust: 14,746.10 kN (3,315,055 lbf). Gross mass: 385,554 kg (850,001 lb). Unfuelled mass: 68,038 kg (149,998 lb). Specific impulse: 263 s. Specific impulse sea level: 238 s. Burn time: 50 s. Height: 24.38 m (79.98 ft). Diameter: 3.96 m (12.99 ft).

Thrust (sl): 13,344.500 kN (2,999,963 lbf). Thrust (sl): 1,360,777 kgf.



Country: USA. Propellants: Solid. Stages: Thiokol 156. Agency: Thiokol.

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