DBSE
Hardware/Vehicles/UR-500K

UR-500K

Retired

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

Total Launches
0
Success Rate
—
Payload to LEO
19 t
First Flight
1967
Reusable
No

Interactive Model

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Specifications

Height50 m
Diameter7.4 m
Wet Mass694,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerKhrunichev
CountryRussia

Engines Used

Engine usage data lives in the Engine Dashboard.

Launch History

No launches attributed to this vehicle in the database yet.

Reliability by Year

Reliability data not available yet.

Related Entities

UR-500Vehicle 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