Encyclopedia Astronautica
SICBM

Thiokol solid rocket engine. 979 kN.

Gross mass: 11,600 kg (25,500 lb).
Height: 7.50 m (24.60 ft).
Diameter: 1.17 m (3.83 ft).
Thrust: 979.00 kN (220,087 lbf).
Burn time: 40 s.

Associated Countries

See also

Associated Manufacturers and Agencies

Thiokol American manufacturer of rocket engines and rockets. Thiokol Corporation, Ogden, UT, USA. More...

Associated Propellants

Solid Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...

Associated Stages

SICBM-1 Solid propellant rocket stage. Loaded mass 11,600 kg. Thrust 979.00 kN. More...