Vesta

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Engine Model: Vesta. Designer: LRBA. Propellants: Nitic acid/Turpentine. Thrust(vac): 140.000 kN (31,470 lbf). Burn time: 56 sec. Country: France. Vesta used on Rocket Stages Used on stage: Vesta. 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.