Encyclopedia Astronautica
RT-2-1


OKB-1 solid rocket engine. 900 kN.

Height: 4.80 m (15.70 ft).
Diameter: 1.95 m (6.39 ft).
Thrust: 900.00 kN (202,320 lbf).
Burn time: 30 s.

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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...

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