ArianeGroup

Ariane 5 GS

GS

Ariane 5 GS
Retired

Overview

/01

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.

Manufacturer

ArianeGroup

Variant

GS

Alias

N/A

Maiden Flight

August 11, 2005

Technical Specifications

/02
55 m

Length

5.4 m

Diameter

1 t

Launch Mass

12000 kN

Liftoff Thrust

LEO Capacity

6600 kg

GTO Capacity

Launch Record

/03
6

Total Launches

6

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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