Encyclopedia Astronautica
RD RT-1-3


OKB-1 solid rocket engine. 240 kN.

Gross mass: 3,000 kg (6,600 lb).
Height: 2.80 m (9.10 ft).
Diameter: 1.40 m (4.50 ft).
Thrust: 240.00 kN (53,950 lbf).
Burn time: 42 s.

More... - Chronology...


Associated Countries
See also
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
  • RT-1-3 Solid propellant rocket stage. Loaded mass 3,000 kg. Thrust 240.00 kN. More...

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