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Hardware/Vehicles/Angara A5

Angara A5

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

Total Launches
5
Success Rate
80%
Payload to LEO
24.5 t
First Flight
2014
Reusable
No

Interactive Model

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Specifications

Height42.8 m
Diameter2.9 m
Wet Mass773,000 kg
Payload to GTO5.4 t
Payload to SSO7.5 t
ManufacturerKhrunichev
CountryRussia

Engines Used

Engine usage data lives in the Engine Dashboard.

Launch History

Reliability by Year

Related Entities

Naro-1Vehicle familyAngara-1.2Vehicle familyAngara A5/PerseiVehicle familyRD-191Engine

Data Sources for This Record

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