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Kvant-1-1
LOx/Kerosene propellant rocket stage. 4 RD-0124-14D23 verniers. Empty mass estimated.

AKA: Kvant-1. Status: Design 1994. Thrust: 1,102.20 kN (247,784 lbf). Gross mass: 74,000 kg (163,000 lb). Unfuelled mass: 7,000 kg (15,400 lb). Specific impulse: 335 s. Specific impulse sea level: 297 s. Burn time: 195 s. Height: 10.30 m (33.70 ft). Diameter: 2.60 m (8.50 ft). Span: 2.60 m (8.50 ft).



Country: Russia. Engines: RD-0124-14D23, RD-120K. Launch Vehicles: Kvant-1. Propellants: Lox/Kerosene.

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