Encyclopedia Astronautica
Veronique P6-1


Solid propellant rocket stage. Loaded mass 500 kg. Thrust 20.00 kN.

Status: Retired 1952.
Gross mass: 500 kg (1,100 lb).
Height: 6.00 m (19.60 ft).
Diameter: 0.55 m (1.80 ft).
Thrust: 20.00 kN (4,496 lbf).
Number: 2 .

More... - Chronology...


Associated Countries
Associated Engines
Associated Launch Vehicles
  • Veronique P6 French sounding test vehicle. Test vehicle, powered by six powder rockets, to test the Veronique's unique wire guidance system. More...

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...

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