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Hardware/Vehicles/Angara-1.2

Angara-1.2

Retired

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

Total Launches
7
Success Rate
100%
Payload to LEO
—
First Flight
2014
Reusable
No

Specifications

Height42.8 m
Diameter2.9 m
Wet Mass171,000 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

Naro-1Vehicle familyAngara A5Vehicle 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