Proton-K/DM-2 DM1

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Proton-K/DM-2 DM1

Part of Proton

Version of the 11S861 with adapter for Lockheed Martin AS 4000 bus spacecraft.

Payload: 5,000 kg (11,000 lb). Thrust: 9,500.00 kN (2,135,600 lbf). Gross mass: 691,500 kg (1,524,400 lb). Height: 57.20 m (187.60 ft). Diameter: 4.15 m (13.61 ft). Span: 7.40 m (24.20 ft). Apogee: 40,000 km (24,000 mi).

LEO Payload: 5,000 kg (11,000 lb). Payload: 4,350 kg (9,590 lb) to a GTO.

Family: orbital launch vehicle. Country: Russia. Engines: RD-0210, RD-0212, RD-58M, RD-253-11D48. Stages: Proton K-1, Proton K-2, Proton K-3, Proton 11S861. Agency: Chelomei bureau.

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