DBSE
Hardware/Vehicles/UR-500

UR-500

Retired

Khrunichev · 2-stage orbital rocket · Part of the Proton family

Total Launches
4
Success Rate
75%
Payload to LEO
8.4 t
First Flight
1965
Reusable
No

Interactive Model

Open full size →

Specifications

Height39 m
Diameter7.4 m
Wet Mass595,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerKhrunichev
CountryRussia

Engines Used

Engine usage data lives in the Engine Dashboard.

Launch History

Reliability by Year

Related Entities

UR-500KVehicle familyProton-KVehicle familyProton-K/DM-2Vehicle familyProton-K/DMVehicle familyProton-K/Briz-MVehicle familyProton-M/Briz-MVehicle familyProton-MVehicle familyUR-500K/Blok DVehicle familyRD-275Engine

Data Sources for This Record

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