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Ariane·Aérospatiale

Ariane 5 GS

retired
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Specifications

Status
retired
Height
55 m
Diameter
5.4 m
Mass
750,000 kg
Stages
2
Thrust
12,000 kN
Payload to GTO
6,600 kg
First flight
2005-08-11
Total launches
6
Success / Fail
6 / 0

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.

Propulsion

First stage

Vulcain 2936 kN
LH2 / LOX · gas-generator
ArianeGroupIsp 433s (vac)since 2002

Second stage

HM7B67 kN
LH2 / LOX · gas-generator
ArianeGroupIsp 446s (vac)since 1979

Payloads it launched

10 loaded
HELIOS 2B
LEO
RASCOM-QAF 1
GEO
HORIZONS-2
GEO
OPTUS D2
GEO
INTELSAT 11 (IS-11)
GEO
INSAT-4A
GEO
METEOSAT-9 (MSG-2)
GEO
SYRACUSE 3A
GEO
GALAXY 15 (G-15)
GEO
THAICOM 4
GEO