Space · launch vehicle
Ariane 5 GS
AG
RETIRED
At a glance
Launches
6
Success rate
100%
6 ok · 0 failed
Payload to LEO
—
Payload to GTO
6,600 kg
Manufacturer
ArianeGroupStatus
RetiredFirst flight
11 Aug 2005Reusable
NoHeight
55 mDiameter
5.4 mLaunch mass
750 tLiftoff thrust
12,000 kNStages
2Launch cost
—Booster landings
—Links
WikipediaAbout
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.
Source The Space Devs — Launch Library 2
Last checked 29 Sept 2026
