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.

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
First flight August 11, 2005 · 08:20 UTC · latest December 18, 2009
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Ariane 5 GS flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 2005 | 3 | 0 | 3 |
| 2006 | 0 | 0 | 0 |
| 2007 | 2 | 0 | 2 |
| 2008 | 0 | 0 | 0 |
| 2009 | 1 | 0 | 1 |