Encyclopedia Astronautica
Veronique


LRBA solid rocket engine. 40 kN.

Gross mass: 500 kg (1,100 lb).
Unfuelled mass: 385 kg (848 lb).
Height: 5.80 m (19.00 ft).
Diameter: 0.55 m (1.80 ft).
Thrust: 40.00 kN (8,992 lbf).
Burn time: 6.50 s.

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Associated Countries
See also
Associated Manufacturers and Agencies
  • LRBA French manufacturer of rocket engines and rockets. LRBA, 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
  • Veronique Nitric acid/Turpentine rocket stage. 40.00 kN (8,992 lbf) thrust. Mass 1,300 kg (2,866 lb). More...

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