Proton-K/DM
Proton / UR-500 family · Khrunichev State Research and Production Space Center · Retired
The Proton-K was a Russian, previously Soviet, carrier rocket derived from the earlier Proton. It was built by Khrunichev, and launched from sites 81 and 200 at the Baikonur Cosmodrome in Kazakhstan.
Specifications
- Thrust
- 8,847 kN
- Height
- 59 m
- Diameter
- 4.15 m
- Launch mass
- 711 t
- Stages
- 4
- Launch cost
- —
- LEO capacity
- —
- GTO capacity
- —
- GEO capacity
- 1,880 kg
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
66
Launches with a definitive outcome
Success rate
92.4%
61 of 66
Current success streak
31
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.
Launches
- Proton-K/DM | Gorizont 20 — Success
- Proton-K/DM | Ekran — Success
- Proton-K/DM | Gorizont 15 — Success
- Proton-K/DM | Ekran — Success
- Proton-K/DM | Gorizont 14 — Success