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Molniya 8K78-2
Part of R-7 Block I stage series Family
LOx/Kerosene propellant rocket stage. .

Status: Retired 1965. Thrust: 294.00 kN (66,093 lbf). Gross mass: 24,300 kg (53,500 lb). Unfuelled mass: 2,000 kg (4,400 lb). Specific impulse: 330 s. Burn time: 200 s. Height: 2.84 m (9.31 ft). Diameter: 2.56 m (8.39 ft). Span: 2.56 m (8.39 ft).

Cost $ : 3.000 million.



Country: Russia. Engines: RD-0107, RD-0108. Launch Vehicles: Molniya 8K78, Molniya 8K78/E6. Propellants: Lox/Kerosene.

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