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Proton-K/DM-2M

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Proton-K/DM-2M
Part of Proton Family
This four stage version uses the Block DM-2M / 11S861-01 upper stage, which has its own self-contained guidance unit. This reduces payload but does not require the spacecraft's guidance system to provide steering commands to booster. Used for launches of Russian geosynchronous satellites from 1994 on.
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AKA: 8K82K / 11S861-01;D-1e;SL-12;UR-500K. Status: Active. First Launch: 1994-01-20. Last Launch: 2006-06-17. Number: 41 . Payload: 1,880 kg (4,140 lb). Thrust: 8,847.00 kN (1,988,884 lbf). Gross mass: 712,460 kg (1,570,700 lb). Height: 59.00 m (193.00 ft). Diameter: 4.15 m (13.61 ft). Span: 7.40 m (24.20 ft). Apogee: 40,000 km (24,000 mi).

Payload: 1,880 kg (4,140 lb) to a GEO. Launch Price $: 70.000 million in 1994 dollars.

More at: Proton-K/DM-2M.
Family: orbital launch vehicle. Country: Russia. Engines: RD-0212, RD-58S, RD-253-11D48. Spacecraft: Glonass, FS-1300, HS 601, Gals, Ekspress, Spacebus 3000, AS 2100, Kupon, Yamal, LMI, Yakhta. Projects: Americom, Anik, Asiasat, Astra, DirecTV, Intelsat, Panamsat, Sirius, Telstar series. Launch Sites: Baikonur, Baikonur LC81/23, Baikonur LC81/24, Baikonur LC200/39. Stages: UR-200-2, Proton K-1, Proton K-2, Proton 11S861-01. Agency: Chelomei bureau, Echostar.
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