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CFTH-HB solid rocket engine. 24 kN.

Gross mass: 30 kg (66 lb).
Unfuelled mass: 14 kg (30 lb).
Height: 1.60 m (5.20 ft).
Diameter: 0.10 m (0.32 ft).
Thrust: 24.00 kN (5,395 lbf).
Burn time: 0.90 s.

More... - Chronology...


Associated Countries
See also
Associated Manufacturers and Agencies
  • CFTH-HB French manufacturer of rocket engines and rockets. CFTH-HB, 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
  • Epona-1 Solid rocket stage. 24.00 kN (5,395 lbf) thrust. Mass 30 kg (66 lb). More...

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