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Energia M-1
Core stage of Energia-M. LOx/LH2 propellant rocket stage.

AKA: Energia M. Status: Development ended 1993. Thrust: 1,960.00 kN (440,620 lbf). Gross mass: 272,000 kg (599,000 lb). Unfuelled mass: 28,000 kg (61,000 lb). Specific impulse: 455 s. Specific impulse sea level: 352 s. Burn time: 550 s. Height: 20.00 m (65.00 ft). Diameter: 7.70 m (25.20 ft). Span: 7.70 m (25.20 ft).



Country: Russia. Engines: RD-0120M. Launch Vehicles: Energia M. Propellants: Lox/LH2.

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