Encyclopedia Astronautica
Berenice-2


Solid rocket stage. 91.70 kN (20,615 lbf) thrust. Mass 1,050 kg (2,315 lb).

Status: Retired 1972.
Gross mass: 1,050 kg (2,310 lb).
Unfuelled mass: 310 kg (680 lb).
Height: 3.80 m (12.40 ft).
Diameter: 0.56 m (1.83 ft).
Thrust: 91.70 kN (20,615 lbf).
Burn time: 18 s.

More... - Chronology...


Associated Countries
Associated Engines
  • SEPR 740 SEPR solid rocket engine. 91.7 kN. Out of production. Isp=230s. Used on Berenice, Titus. First flight 1962. More...

Associated Launch Vehicles
  • Berenice French sounding rocket. Berenice was Onera's successor to the Antares re-entry vehicle test booster. It was nearly double the mass of Antares. More...

Associated Manufacturers and Agencies
  • ONERA French manufacturer of rocket engines and rockets. Office National d'Etudes et de Recherches Aerospatiales, 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...

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