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HomeLaunch HistoryRocket EncyclopediaFuture LaunchesStatistics & ChartsDashboard

Proton / UR-500 family

Proton-K/DM-2M

Soviet Union and Russia1994 to 2006
Drawing of the Proton-K/DM-2M

Proton-K with the Blok DM-2M upper stage, flown from 1994 to 2006, largely for Russian and Western communications satellites as Proton opens to commercial customers.

Launches
41
Success rate
95%
1 failure · 1 partial
First flight
20 January 1994
Gals 1
Last flight
17 June 2006
Kazsat
Builder
Khrunichev
Height
59 m
Diameter
4.2 m
Stages
4
Propellants
UDMH / N2O4, Kerosene / LOX
Payload to LEO
19,000 kg
Payload to GTO
4,350 kg

Launches per year

Proton-K/DM-2M
Other Proton / UR-500 rockets
Show as table
YearLaunchesProton-K/DM-2M
196520
196620
196740
196850
1969100
197050
197160
197220
197370
197460
197550
197650
197750
197880
197960
198050
198170
1982100
1983120
1984130
1985100
198690
1987130
1988130
1989110
1990110
199190
199280
199360
1994132
199570
199682
199795
199873
199996
2000149
200162
200296
200352
200482
200571
200661
200770
2008100
2009100
2010120
201190
2012110
2013100
201480
201580
201630
201740
201820
201950
202010
202120
202210
202320
202610

Proton / UR-500 rockets

RocketFlownLaunchesSuccess rateHeightPayload to LEO
UR-5001965 to 1966475%46.3 m8,400 kg
Proton / UR-500 K/D1967 to 19753863%57 m12,200 kg
Proton-K1968 to 20002990%50 m21,600 kg
Proton-K/DM1974 to 19906691%59 m19,000 kg
Proton-K/D-11975 to 19891292%57 m19,000 kg
Proton K/DM-21982 to 201211094%57.2 m19,000 kg
Proton-K/D-21988 to 19963100%57 m6,220 kg
Proton-K/DM-2M1994 to 20064195%59 m19,000 kg
Proton-K/17S401997 to 20026100%59 m6,000 kg
Proton-K/Briz-M1999 to 2003475%57 m19,760 kg
Proton-M Briz-M2001 to 20236891%53 m21,000 kg
Proton-M Briz-M Enhanced2004 to 20123391%53 m21,000 kg
Proton-M DM-2 Enhanced2007 to 20106100%53 m21,000 kg
Proton-M Blok DM-032010 to 2026875%58.2 m21,000 kg
Proton-M20211100%58.2 m23,000 kg