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Ariane 5 ES

Retired

ArianeGroup

The Ariane 5 ES (Evolution Storable) has an estimated LEO launch capacity of 21,000 kg (46,000 lb). It includes all the performance improvements of Ariane 5 ECA core and boosters but replaces the ESC-A second stage with the restartable EPS used on Ariane 5 GS variants. It was used to launch the Automated Transfer Vehicle (ATV) into a 260 km circular low Earth orbit inclined at 51.6° and has been used 3 times to launch 4 Galileo navigation satellites at a time directly into their operational orbit. The Ariane 5 ES flew 8 times from 2008 to 2018 with no failures.

Key figures

Total launches
8
Successes
8
Failures
0
Success rate
100.0 %
Success streak
8
Maiden flight
Mar 9, 2008
Reusable
No
Shortest launch interval ⓘ
224d 16h
Planned launches
0
Ariane, Ariane 5 family total
117 launches · 112 successes · 5 failures (6 variants)

🧐 Data check

Automatic plausibility checks — anomalies are surfaced transparently here:

  • ℹ️The figures above apply only to the “Ariane 5 ES” variant. The Launch Library counts each variant separately — the Ariane, Ariane 5 family totals 117 launches across 6 variants.

Technology

Length
45.7 m
Diameter
5.4 m
Launch mass
746 t
Liftoff thrust
11,400 kN
Stages
2
LEO (low Earth orbit)
21,000 kg

Engines & propellant

Boosters2× EAP-Feststoffbooster (P241)Feststoff (HTPB)
1st stage1× Vulcain 2Flüssigwasserstoff / Flüssigsauerstoff
2nd stage1× HM7B (ECA)Flüssigwasserstoff / Flüssigsauerstoff

Engine and propellant data from curated sources: Wikipedia — Ariane 5

Launches per year

of which in our database: 8

2008: 1 Successes120082011: 1 Successes120112012: 1 Successes120122013: 1 Successes120132014: 1 Successes120142016: 1 Successes120162017: 1 Successes120172018: 1 Successes12018
Successes Failures Other/planned

History & events

  1. Mar 9, 2008🚀 Maiden flightATV-1 "Jules Verne"View launchVideo

Sources