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Molniya 8K78-1
Part of R-7 Block A stage series
LOx/Kerosene propellant rocket stage. .

Status: Retired 1965. Thrust: 941.00 kN (211,545 lbf). Gross mass: 100,500 kg (221,500 lb). Unfuelled mass: 6,800 kg (14,900 lb). Specific impulse: 315 s. Specific impulse sea level: 248 s. Burn time: 301 s. Height: 28.00 m (91.00 ft). Diameter: 2.99 m (9.80 ft). Span: 2.60 m (8.50 ft).

Cost $ : 13.000 million.



Country: Russia. Engines: RD-108-8D75K. Launch Vehicles: Molniya 8K78/E6. Propellants: Lox/Kerosene.

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