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V-1000-1
Nitric acid/Amine propellant rocket stage

Status: Retired 1973. Thrust: 103.00 kN (23,155 lbf). Height: 8.00 m (26.20 ft). Diameter: 0.55 m (1.80 ft).



Country: Russia. Engines: S2.726. Launch Vehicles: V-1000. Propellants: Nitric acid/Amine.

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