Encyclopedia Astronautica
SEP 402


Aerospatiale solid rocket engine. 300 kN.

Gross mass: 8,800 kg (19,400 lb).
Unfuelled mass: 800 kg (1,760 lb).
Height: 2.00 m (6.50 ft).
Diameter: 1.93 m (6.33 ft).
Thrust: 300.00 kN (67,440 lbf).
Burn time: 70 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
  • MSBS M4-2 Solid rocket stage. 300.00 kN (67,443 lbf) thrust. Mass 8,800 kg (19,401 lb). More...

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