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Ariane 2 was a European expendable space launch vehicle, operated by the European Space Agency (ESA) between 1986 and 1989 as part of Ariane family of rockets. The principal manufacturer for the Ariane 2 was Aérospatiale, while the lead agency for its development was the Centre National d'Etudes Spatiales (CNES), the French government's space agency. Development of the Ariane 2 was authorized in July 1979, months prior to the Ariane 1's first flight. Drawing heavily upon both the design and infrastructure of the Ariane 1, the new launcher was concurrently developed alongside the Ariane 3, with which it shared much of its design. It represented an advancement of the Ariane 1 rather than a replacement but was capable of lifting even heavier payloads into Geostationary transfer orbit (GTO). Developed largely within a two-year window, the Ariane 2 performed its maiden flight on 31 May 1986, actually flying after its Ariane 3 sibling.
Missions
6
Success Rate
83.3%
Successes
5
Failures
1
Success Streak
5
Partial Failures
0
Active 1986 to 1989
Rocket
Diameter: 3.8m
Height: 49m
Payload to Orbit
GTO: 2,175 kg
Liftoff Thrust
2,580 Kilonewtons
Stages
3