DBSE
Hardware/Vehicles/Proton-M

Proton-M

Retired

Khrunichev · 3-stage orbital rocket · Part of the Proton family

Total Launches
15
Success Rate
86.7%
Payload to LEO
21 t
First Flight
2004
Reusable
No

Interactive Model

Open full size →

Specifications

Height53 m
Diameter7.4 m
Wet Mass712,800 kg
Payload to GTO4.5 t
Payload to SSON/A
ManufacturerKhrunichev
CountryRussia

Engines Used

Engine usage data lives in the Engine Dashboard.

Launch History

Reliability by Year

Related Entities

UR-500Vehicle familyUR-500KVehicle familyProton-KVehicle familyProton-K/DM-2Vehicle familyProton-K/DMVehicle familyProton-K/Briz-MVehicle familyProton-M/Briz-MVehicle familyUR-500K/Blok DVehicle familyRD-276Engine

Data Sources for This Record

Specifications
GCAT / Wikipedia · verified quarterly
Launch History
LL2 API · updated every 6h
Engine Data
Manufacturer + Wikidata