Ariane family
Ariane 5 GS
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 is built by ArianeGroup of France. Company background, funding, contracts and news for this operator are tracked on Space Index. It first flew on 11 August 2005 and last flew on 18 December 2009.
Flight record
Payload
| Geostationary transfer orbit | 6,600kg |
|---|
Vehicle
| Stages | 2 |
|---|---|
| Length | 55m |
| Diameter | 5.4m |
| Launch mass | 750t |
| Liftoff thrust | 12,000kN |
| Maiden flight | 2005-08-11 |
| Reusable | No |
Pads used
Orbits delivered
Launch history
| Date | Mission | Pad | Orbit | Outcome |
|---|---|---|---|---|
| 2009-12-18 | Ariane 5 GS | Helios 2B | Ariane Launch Area 3 | Sun-Synchronous Orbit | Success |
| 2007-12-21 | Ariane 5 GS | RASCOM-QAF 1 & Horizons-2 | Ariane Launch Area 3 | Geostationary Transfer Orbit | Success |
| 2007-10-05 | Ariane 5 GS | Intelsat 11 & Optus D2 | Ariane Launch Area 3 | Geostationary Transfer Orbit | Success |
| 2005-12-21 | Ariane 5 GS | INSAT-4A, Meteosat 9 | Ariane Launch Area 3 | Geostationary Transfer Orbit | Success |
| 2005-10-13 | Ariane 5 GS | Syracuse 3A & Galaxy 15 | Ariane Launch Area 3 | Geostationary Transfer Orbit | Success |
| 2005-08-11 | Ariane 5 GS | Thaicom 4 | Ariane Launch Area 3 | Geostationary Transfer Orbit | Success |
Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.
Further reading: Wikipedia