Proton-M Briz-M
Proton / UR-500 family · Khrunichev State Research and Production Space Center · Active
Specifications
- Thrust
- 10,000 kN
- Height
- 53 m
- Diameter
- 7.4 m
- Launch mass
- 712 t
- Stages
- 4
- Launch cost
- —
- LEO capacity
- 21,000 kg
- GTO capacity
- 4,500 kg
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
68
Launches with a definitive outcome
Success rate
91.2%
62 of 68
Current success streak
19
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
—
Between consecutive booster flights
Counted from padside's own launch record — the same basis as the Stats page.