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HomeLaunch HistoryRocket EncyclopediaFuture LaunchesStatistics & ChartsDashboard

Proton / UR-500 family

Proton-K/D-2

Soviet Union and Russia1988 to 1996
Drawing of the Proton-K/D-2

Proton-K with the Blok D-2 upper stage, used for the Phobos 1 and Phobos 2 Mars probes in 1988 and the ill-fated Mars 96 in 1996.

Launches
3
Success rate
100%
0 failures
First flight
7 July 1988
Fobos-1
Last flight
16 November 1996
Mars-96
Builder
Khrunichev
Height
57 m
Diameter
4.2 m
Stages
4
Propellants
UDMH / N2O4, Kerosene / LOX
Payload to LEO
6,220 kg
Payload to GTO
4,350 kg

Launches per year

Proton-K/D-2
Other Proton / UR-500 rockets
Show as table
YearLaunchesProton-K/D-2
196520
196620
196740
196850
1969100
197050
197160
197220
197370
197460
197550
197650
197750
197880
197960
198050
198170
1982100
1983120
1984130
1985100
198690
1987130
1988132
1989110
1990110
199190
199280
199360
1994130
199570
199681
199790
199870
199990
2000140
200160
200290
200350
200480
200570
200660
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