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Proton-K

Proton / UR-500 familyKhrunichev State Research and Production Space CenterRetired

Proton-K vehicle

Specifications

Thrust
8,847 kN
Height
50 m
Diameter
4.15 m
Launch mass
694 t
Stages
3
LEO capacity
19,760 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

29flightswith a definitive outcome
89.7%success rate26 of 29
3failuresincluding partial failures
9success streakcurrent

First flight November 16, 1968 · latest July 12, 2000

Counted from padside's own launch record, the same basis as the stats page.

Flights per year

  • Successful
  • Failed
Show the numbers for Proton flights per year
Proton flights per year
YearSuccessfulFailedTotal
1968101
1969000
1970000
1971101
1972011
1973202
1974202
1975000
1976202
1977213
1978101
1979101
1980000
1981101
1982101
1983101
1984000
1985101
1986112
1987202
1988000
1989101
1990101
1991101
1992000
1993000
1994000
1995101
1996101
1997000
1998101
1999000
2000101

Flights

5 of 29

All 29 flights