DBSE
Hardware/Vehicles/Ariane 2

Ariane 2

Retired

Aerospatiale / Matra · 3-stage orbital rocket · Part of the Ariane family

Total Launches
6
Success Rate
83.3%
Payload to LEO
—
First Flight
1986
Reusable
No

Specifications

Height49 m
Diameter3.8 m
Wet Mass217,000 kg
Payload to GTO2.2 t
Payload to SSON/A
ManufacturerAerospatiale / Matra
CountryFrance

Engines Used

Engine usage data lives in the Engine Dashboard.

Launch History

Reliability by Year

Related Entities

Ariane 1Vehicle familyAriane 3Vehicle familyAriane 44LVehicle familyAriane 42PVehicle familyAriane 40Vehicle familyAriane 44PVehicle familyAriane 42LVehicle familyViking 2BEngine

Data Sources for This Record

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