November 20, 2020

Programme overview

Versatile heavy-lift launchers for Europe.

Detailed objectives

Ariane 5’s twofold aim is to continue sustaining Europe’s independent space launch capability and to stay competitive in the commercial market. To this end, it is a heavy-lift launcher capable of orbiting two satellites weighing nearly 5 tonnes each at the same time. Its ES variant was also capable of launching the ATV cargo resupply spacecraft to the International Space Station (ISS) or four Galileo navigation satellites. This multiple-launch capability makes it one of the most competitive vehicles in the world, and its track record one of the most reliable. Up to December 2020, Ariane 5 has experienced only two complete failures on test flights and two partial failures in 109 launches —all variants included— since 1996, including 75 straight successes for the ECA version between 2003 and December 2020.

From 2020, only a single variant is being commercially operated: compared to Ariane 4’s lift capacity of 4.9 tonnes into geostationary transfer orbit (GTO), Ariane 5 ECA can carry twice the payload, with 10 tonnes into GTO for a dual launch and 10.8 tonnes for a single launch.

Ariane 5 thus offers the versatility to loft all kinds of payload into different Earth orbits, from small satellites weighing less than 1 tonne to heavy payloads of up to 20 tonnes, as well as 6 tonnes to the Earth-Moon and Earth-Sun Lagrange points (as it did for the Herschel and Planck telescopes).

Starting in 2022, Ariane 5 will be operated commercially alongside  the new Ariane 6 launcher. Ariane 62 will cater to intermediate launches while Ariane 64 will be for heavy-lift missions. This modularity will ensure even more competitive launch services for Europe, with production costs 40% lower than for Ariane 5, and the launch rate will increase from 6-7 launches to 11 launches a year. The transition from Ariane 5 to Ariane 6 is then planned to last until 2023.

Programme history

Ariane 5 launch log up to its 109th flight in August 2020. Credits: ESA.

Ariane 5 was designed to evolve in line with new market needs and technical innovations. Two distinct evolution programmes—Ariane 5 Evolution, initiated in 1995, and Ariane 5 Plus in 1998—thus gave rise to new variants of the launcher, bringing performance gains for launches into geostationary transfer orbit. Ariane 5 Evolution sought to enhance the performance of the lower composite (with Vulcain 2, a more powerful engine for Ariane 5 ECA’s cryogenic stage, and a lighter structure for the two solid boosters). Ariane 5 Plus focused on the power and versatility of the upper stage (HM-7B engine for Ariane 5 ECA).

An Ariane 5 ES lifts off with four Galileo satellites.

Credits: ESA/Stephane Corvaja, 2016.

Since Ariane 5’s first flight in 1996, there have been five variants and several evolutions:
  • G (Generic): the generic variant of Ariane 5, operated commercially for 13 launches between 1996 and 2003.
  • ECA: operated commercially since 2002, both stages of this variant offer performance gains over Ariane 5 G. With 76 launches to its credit up to December 2020, Ariane 5 ECA is today the only variant still being operated commercially since Ariane 4 was retired from service in 2003 and Ariane 5 ES in July 2018.
  • G+: alongside the ECA variant, this was an enhanced and more reliable G variant conceived after the failure of flight V517, the maiden launch of ECA. Operated commercially for three successful launches in 2004.
  • GS: enhanced version of the G+ variant incorporating evolutions to ECA. Operated commercially for six launches between 2005 and 2009.
  • ES (Evolution Storable): strengthened variant built in 2008 to launch ATV cargo resupply spacecraft to the ISS. After the ATV was retired from service in 2014, Ariane 5 ES was then operated up to July 2018 to deploy the Galileo constellation in groups of four satellites.
  • ME (Midlife Evolution) : version initialement prévue pour 2017-2018, mais annulée pour être remplacée par Ariane 6 pour 2020. Elle prévoyait une forte augmentation de sa performance en passant de 10 tonnes de charge utile en géostationnaire à 12 tonnes. Le nouvel étage supérieur devait remplacer le moteur HM-7B par un moteur Vinci, plus puissant et réallumable, qui équipera bientôt Ariane 6.

Configuration of Ariane 5 variants. Credits: ESA/D. Ducros

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