Molniya 8K78M-3

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Molniya 8K78M-3

Part of Block L

LOx/Kerosene propellant rocket stage. Standardized improved version for Molniya-type communications satellite payloads.

Status: Active. Thrust: 66.60 kN (14,972 lbf). Gross mass: 6,660 kg (14,680 lb). Unfuelled mass: 1,160 kg (2,550 lb). Specific impulse: 340 s. Burn time: 250 s. Height: 3.20 m (10.40 ft). Diameter: 2.40 m (7.80 ft). Span: 2.56 m (8.39 ft).

Family: Space Tugs. Country: Russia. Engines: S1.5400A. Launch Vehicles: Molniya 8K78, Molniya 8K78M, Molniya 8K78M 2BL, Kvant-1. Propellants: Lox/Kerosene.

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