Veronique AGI

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Engine Model: Veronique AGI. Designer: LRBA. Propellants: Nitric acid/Turpentine. Thrust(vac): 40.000 kN (8,992 lbf). Burn time: 49 sec. Country: France. Veronique AGI used on Rocket Stages Used on stage: Veronique. on launch vehicle: Veronique. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.