Encyclopedia Astronautica
15D169


Yuzhnoye solid rocket engine. 142 kN.

Gross mass: 10,000 kg (22,000 lb).
Unfuelled mass: 1,000 kg (2,200 lb).
Height: 3.20 m (10.40 ft).
Diameter: 2.15 m (7.05 ft).
Thrust: 142.00 kN (31,922 lbf).
Burn time: 195 s.

More... - Chronology...


Associated Countries
See also
Associated Manufacturers and Agencies
  • Yuzhnoye Ukrainian manufacturer of rockets, spacecraft, and rocket engines. Yangel Design Bureau, Dnepropetrovsk, Ukraine. 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
  • MR-UR-100-2 N2O4/UDMH rocket stage. 142.00 kN (31,923 lbf) thrust. Mass 10,000 kg (22,046 lb). More...

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