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Proton-M Briz-M

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

Proton-M Briz-M vehicle

Specifications

Thrust
10,000 kN
Height
53 m
Diameter
7.4 m
Launch mass
712 t
Stages
4
LEO capacity
21,000 kg
GTO capacity
4,500 kg
GEO capacity
3,250 kg

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

Flight record

68flightswith a definitive outcome
91.2%success rate62 of 68
6failuresincluding partial failures
19success streakcurrent

First flight April 7, 2001 · latest March 12, 2023

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

Flights per year

  • Successful
  • Failed
Show the numbers for Proton-M Briz-M flights per year
Proton-M Briz-M flights per year
YearSuccessfulFailedTotal
2001101
2002101
2003000
2004303
2005404
2006314
2007314
2008516
2009101
2010101
2011202
2012202
2013909
2014628
2015617
2016303
2017404
2018202
2019303
2020101
2021101
2022000
2023101

Flights

5 of 68

All 68 flights