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Zenit-B
Zenit stage 2. LOx/Kerosene propellant rocket stage.

AKA: Zenit-2. Status: Active. Thrust: 912.00 kN (205,025 lbf). Gross mass: 90,600 kg (199,700 lb). Unfuelled mass: 9,000 kg (19,800 lb). Specific impulse: 349 s. Burn time: 315 s. Height: 11.50 m (37.70 ft). Diameter: 3.90 m (12.70 ft). Span: 3.90 m (12.70 ft).

Cost $ : 15.000 million.



Country: Ukraine. Engines: RD-120. Launch Vehicles: Zenit-2, Zenit-2 11K77.05, Zenit-3SL, Zenit-2M, Zenit-3SLB. Propellants: Lox/Kerosene.

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