Encyclopedia Astronautica
S-23


Avibrassolid rocket engine. 18 kN.

Gross mass: 200 kg (440 lb).
Unfuelled mass: 69 kg (152 lb).
Height: 2.20 m (7.20 ft).
Diameter: 0.30 m (0.98 ft).
Thrust: 18.00 kN (4,046 lbf).
Burn time: 20 s.

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Associated Countries
See also
Associated Manufacturers and Agencies
  • Avibras Brazilian manufacturer of rocket engines. Avibras, Brazil. 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
  • S-23 Solid rocket stage. 18.00 kN (4,047 lbf) thrust. Mass 200 kg (441 lb). More...

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