DBSE
Hardware/Vehicles/Naro-1

Naro-1

Retired

KARI / Khrunichev · 2-stage orbital rocket · Part of the Angara family

Total Launches
0
Success Rate
—
Payload to LEO
0.1 t
First Flight
2009
Reusable
No

Specifications

Height33.5 m
Diameter2.9 m
Wet Mass140,000 kg
Payload to GTON/A
Payload to SSO0.1 t
ManufacturerKARI / Khrunichev
CountrySouth Korea

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

Angara-1.2Vehicle familyAngara A5Vehicle familyAngara A5/PerseiVehicle familyKARI / KhrunichevManufacturerRD-191Engine

Data Sources for This Record

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