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Proton/Briz K/M
Part of Proton
Briz M
Briz M
Credit: Khrunichev
Earlier 8K82K model Proton, but Briz M storable propellant upper stage replaced the Block D cryogenic stage.

AKA: 8K82KM;Proton KM;UR-500KM. Status: Retired 2003. First Launch: 1999-07-05. Last Launch: 2003-12-10. Number: 4 . Payload: 21,000 kg (46,000 lb). Thrust: 9,469.10 kN (2,128,738 lbf). Gross mass: 712,800 kg (1,571,400 lb). Height: 53.00 m (173.00 ft). Diameter: 4.15 m (13.61 ft). Span: 7.40 m (24.20 ft). Apogee: 185 km (114 mi).


More at: Proton/Briz K/M.

Family: orbital launch vehicle. Country: Russia. Engines: RD-253-14D14, 17D58E, S5.98M. Spacecraft: Raduga, Gorizont, Glonass, Spacebus 3000. Projects: Americom. Launch Sites: Baikonur, Baikonur LC81/24, Baikonur LC200/39. Stages: Proton K-2, Proton K-3, Proton M-1, Proton KM-4 Briz M. Agency: Chelomei bureau.

1999 July 5 - . 13:32 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/24. LV Family: Proton. Launch Vehicle: Proton/Briz K/M. FAILURE: Second stage explosion.. Failed Stage: 2.
2000 June 6 - . 02:59 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/24. LV Family: Proton. Launch Vehicle: Proton/Briz K/M.
2003 June 6 - . 22:15 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton/Briz K/M.
2003 December 10 - . 17:42 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/24. LV Family: Proton. Launch Vehicle: Proton/Briz K/M.

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