Zenit-V

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Zenit-V

Part of Block D

Zenit stage 3. LOx/Kerosene propellant rocket stage. Adaptation of Block D for Zenit.

AKA: Zenit-3. Status: In production. Thrust: 84.92 kN (19,091 lbf). Gross mass: 17,300 kg (38,100 lb). Unfuelled mass: 2,720 kg (5,990 lb). Specific impulse: 352 s. Burn time: 650 s. Height: 5.60 m (18.30 ft). Diameter: 3.70 m (12.10 ft). Span: 3.70 m (12.10 ft).

Cost $ : 20.000 million.

Country: Russia. Engines: RD-58M, RD-58Z. Launch Vehicles: Kvant launch vehicle, Zenit-3SL, Zenit-3SLB. Propellants: Lox/Kerosene.

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