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Ariane 5 GS

Ariane familyArianeGroupRetired

At the time of the failure of the first Ariane 5 ECA flight in 2002, all Ariane 5 launchers in production were ECA versions. Some of the ECA cores were modified to use the original Vulcain engine and tank volumes while the failure was investigated; these vehicles were designated Ariane 5 GS. The GS used the improved EAP boosters of the ECA variant and the improved EPS of the G+ variant, but the increased mass of the modified ECA core compared to the G and G+ core resulted in slightly reduced payload capacity. Ariane 5 GS could carry a single payload of 6,600 kg (14,600 lb) or a dual payload of 5,800 kg (12,800 lb) to GTO. The Ariane 5 GS flew 6 times from 2005 to 2009 with no failures.

Ariane 5 GS vehicle

Specifications

Thrust
12,000 kN
Height
55 m
Diameter
5.4 m
Launch mass
750 t
Stages
2
GTO capacity
6,600 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

6flightswith a definitive outcome
100%success rate6 of 6
6success streakcurrent

Counted from padside's own launch record, the same basis as the stats page.

Flights

5 of 6

All 6 flights