Encyclopedia Astronautica
SEPR-732


Sud solid rocket engine. 200 kN.

Gross mass: 1,500 kg (3,300 lb).
Height: 2.50 m (8.20 ft).
Diameter: 0.56 m (1.83 ft).
Thrust: 200.00 kN (44,960 lbf).

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Associated Countries
See also
Associated Manufacturers and Agencies
  • Sud French manufacturer of rocket engines. Sud Aviation, France. 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
  • SE4400-1 Solid propellant rocket stage. Loaded mass 1,500 kg. Thrust 200.00 kN. More...

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