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Molniya 8K78M-1
Part of R-7 Block A stage series Family
LOx/Kerosene propellant rocket stage. .

Status: Active. Thrust: 976.70 kN (219,571 lbf). Gross mass: 100,600 kg (221,700 lb). Unfuelled mass: 6,798 kg (14,987 lb). Specific impulse: 315 s. Specific impulse sea level: 248 s. Burn time: 291 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-108-8D727. Launch Vehicles: Molniya 8K78M, Molniya 8K78M 2BL, Molniya 8K78M ML, Soyuz 11A511L, Soyuz 11A511M, Soyuz-U, Molniya 8K78M SOL. Propellants: Lox/Kerosene.

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