Padside

Proton-M

Proton / UR-500 family · Khrunichev State Research and Production Space Center · Active

Wikipedia ↗Compare with… →

Proton-M is a three stage Russian heavy lift launch vehicle derived from the Soviet Proton launch vehicle. Image Credit: Alex Lane

Specifications

Thrust
10,532 kN
Height
58.2 m
Diameter
7.4 m
Launch mass
705 t
Stages
3
Launch cost
$65M
LEO capacity
23,000 kg
GTO capacity
6,920 kg
GEO capacity
3,250 kg
SSO capacity

Vehicle specifications from Launch Library; blanks are unpublished figures.

Flight record

Flights
1
Launches with a definitive outcome
Success rate
100%
1 of 1
Current success streak
1
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