Proton-M Blok DM-03
Proton / UR-500 familyKhrunichev State Research and Production Space CenterActive
Proton-M Blok DM-03 is a four stage Russian heavy lift launch vehicle derived from the Soviet Proton launch vehicle. It is a Proton-M with an added DM-03 Fourth stage.
Specifications
- Thrust
- 10,532 kN
- Height
- 58.2 m
- Diameter
- 7.4 m
- Launch mass
- 712 t
- Stages
- 4
- Launch cost
- $65M
- LEO capacity
- 21,000 kg
- GTO capacity
- 6,920 kg
- GEO capacity
- 3,250 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
8flightswith a definitive outcome
75%success rate6 of 8
2failuresincluding partial failures
6success streakcurrent
First flight December 5, 2010 · latest February 12, 2026 · 08:52 UTC
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 flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 2010 | 0 | 1 | 1 |
| 2011 | 0 | 0 | 0 |
| 2012 | 0 | 0 | 0 |
| 2013 | 0 | 1 | 1 |
| 2014 | 0 | 0 | 0 |
| 2015 | 1 | 0 | 1 |
| 2016 | 0 | 0 | 0 |
| 2017 | 0 | 0 | 0 |
| 2018 | 0 | 0 | 0 |
| 2019 | 2 | 0 | 2 |
| 2020 | 0 | 0 | 0 |
| 2021 | 0 | 0 | 0 |
| 2022 | 1 | 0 | 1 |
| 2023 | 1 | 0 | 1 |
| 2024 | 0 | 0 | 0 |
| 2025 | 0 | 0 | 0 |
| 2026 | 1 | 0 | 1 |