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Hardware/Vehicles/Angara A5/Persei

Angara A5/Persei

Retired

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

Total Launches
0
Success Rate
—
Payload to LEO
24.5 t
First Flight
—
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 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

Naro-1Vehicle familyAngara-1.2Vehicle familyAngara A5Vehicle familyRD-191Engine

Data Sources for This Record

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