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Veronique R-1
LRBA solid rocket engine.

AKA: Veronique. Status: Retired 1952. Number: 1 . Thrust: 40.00 kN (8,992 lbf). Gross mass: 500 kg (1,100 lb). Unfuelled mass: 385 kg (848 lb). Burn time: 6.50 s. Height: 5.80 m (19.00 ft). Diameter: 0.55 m (1.80 ft).



Subtopics

Vero P2 LRBA solid rocket engine. Veronique P2 first stage.

Vero P6 LRBA solid rocket engine. Veronique P6 first stage.

Country: France. Launch Vehicles: Veronique R, Veronique. Propellants: Solid. Agency: LRBA.

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