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The Ariane 4 was a European expendable space launch system, developed by the Centre National d'Études Spatiales (CNES), the French space agency, for the European Space Agency (ESA). In 1982, the Ariane 4 program was approved by ESA. Drawing heavily upon the preceding Ariane 3, it was designed to provide a launcher capable of delivering heavier payloads and at a lower cost per kilogram than the earlier members of the Ariane family. The Ariane 4 was principally an evolution of the existing technologies used, as opposed to being revolutionary in its design ethos; this approach quickly gained the backing of most ESA members, who funded and participated in its development and operation. Capable of being equipped with a wide variety of strap-on boosters, the Ariane 4 gained a reputation for being an extremely versatile launcher.
Missions
116
Success Rate
97.4%
Successes
113
Failures
3
Success Streak
74
Partial Failures
0
Active 1991 to 2001
Rocket
Diameter: 3.8m
Height: 58.72m
Payload to Orbit
GTO: 3,460 kg
Liftoff Thrust
4,334 Kilonewtons
Stages
3
Strap-ons
4
Active 1988 to 2001
Rocket
Diameter: 3.8m
Height: 58.72m
Payload to Orbit
GTO: 4,220 kg
Liftoff Thrust
5,800 Kilonewtons
Stages
3
Strap-ons
4
Active 1989 to 2003
Rocket
Diameter: 3.8m
Height: 58.72m
Payload to Orbit
GTO: 4,720 kg
Liftoff Thrust
6,000 Kilonewtons
Stages
3
Strap-ons
4
Active 1990 to 2002
Rocket
Diameter: 3.8m
Height: 58.72m
Payload to Orbit
GTO: 2,930 kg
Liftoff Thrust
4,334 Kilonewtons
Stages
3
Strap-ons
2
Active 1993 to 2002
Rocket
Diameter: 3.8m
Height: 58.72m
Payload to Orbit
GTO: 3,480 kg
Liftoff Thrust
4,538 Kilonewtons
Stages
3
Strap-ons
2
Active 1990 to 1999
Rocket
Diameter: 3.8m
Height: 58.72m
Payload to Orbit
LEO: 5,000 kg
GTO: 2,000 kg
Liftoff Thrust
3,034 Kilonewtons
Stages
3