Ariane 6

Ariane 6
Ariane 62 (left) and Ariane 64 (right)
Function
ManufacturerArianeGroup
Country of originEuropean multi-national[a]
Project cost3.215 billion[1]
Cost per launch
  • A62: €70 million (2018 est.)[2]
  • A64: €115 million (2018 est.)[2]
Size
Height63 m (207 ft)
Diameter5.4 m (18 ft)
Mass
  • A62: 530,000 kg (1,170,000 lb)
  • A64: 860,000 kg (1,900,000 lb)
Stages2
Capacity
Payload to LEO
Mass
  • A62: 10,350 kg (22,820 lb)[3]
  • A64: 21,650 kg (47,730 lb)[3]
Payload to GTO
Orbital inclination
Mass
  • A62: 4,500 kg (9,900 lb)[3]
  • A64: 11,500 kg (25,400 lb)[3]
Payload to GEO
Orbital inclination
MassA64: 5,000 kg (11,000 lb)[3]
Payload to SSO
Orbital inclination97.4°
Mass
  • A62: 7,200 kg (15,900 lb)[3]
  • A64: 15,500 kg (34,200 lb)[3]
Payload to LTO
Orbital inclination97.4°
Mass
  • A62: 3,500 kg (7,700 lb)[3]
  • A64: 8,600 kg (19,000 lb)[3]
Associated rockets
FamilyAriane
ComparableFalcon 9, Falcon Heavy, Terran R, H3, Vulcan Centaur
Launch history
StatusActive
Launch sitesGuiana Space Centre, ELA-4
Total launches1
Partial failure(s)1 (VA262)
First flight9 July 2024 (2024-07-09)[4]
Boosters – P120C
No. boosters2 or 4
Diameter3 m (9.8 ft)
Propellant mass142,000 kg (313,000 lb)
Maximum thrust3,500 kN (790,000 lbf) each
Total thrust
  • A62: 7,000 kN (1,600,000 lbf)
  • A64: 14,000 kN (3,100,000 lbf)
Burn time130 seconds
PropellantHTPB / AP / Al
First stage
Diameter5.4 m (18 ft)
Propellant mass140,000 kg (310,000 lb)
Powered by1 × Vulcain 2.1
Maximum thrust1,370 kN (310,000 lbf)
Burn time468 seconds
PropellantLOX / LH2
Second stage
Diameter5.4 m (18 ft)
Propellant mass31,000 kg (68,000 lb)
Powered by1 × Vinci
Maximum thrust180 kN (40,000 lbf)
Burn timeUp to 900 seconds and four burns[5]
PropellantLOX / LH2

Ariane 6 is a European expendable launch system operated by Arianespace and developed and produced by ArianeGroup on behalf of the European Space Agency (ESA). It replaces Ariane 5, as part of the Ariane launch vehicle family.

This two-stage rocket utilizes liquid hydrogen and liquid oxygen (hydrolox) engines. The first stage features an upgraded Vulcain engine from Ariane 5, while the second uses the Vinci engine, designed specifically for this rocket. The Ariane 62 variant uses two P120C solid rocket boosters, while Ariane 64 uses four. The P120C booster is shared with Europe's other launch vehicle, Vega C, and is an improved version of the P80 rocket stage used on the original Vega.

Selected in December 2014 over an all-solid-fuel option, Ariane 6 was originally targeted for a 2020 launch. However, the program encountered delays, with the first launch occurring on 9 July 2024. The second launch has been delayed from a December 2024 target date to 1Q2025, per Arianespace in November 2024.[6]

Ariane 6 was designed to halve launch costs and increase annual capacity from seven to eleven missions compared to its predecessor,[needs update] but the program has faced controversy over high costs and lack of reusability versus competitors' rockets, such as SpaceX's Falcon 9. European officials defend the program, saying it provides crucial independent space access for its member states.


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  1. ^ "Desire for Competitive Ariane 6 Nudges ESA Toward Compromise in Funding Dispute with Contractor". Spacenews. 3 April 2015. Retrieved 18 September 2024.
  2. ^ a b Cite error: The named reference Smith 2018 was invoked but never defined (see the help page).
  3. ^ a b c d e f g h i Lagier, Roland (March 2021). "Ariane 6 User's Manual Issue 2 Revision 0" (PDF). Arianespace. Archived (PDF) from the original on 14 February 2022. Retrieved 29 December 2021.
  4. ^ Mathewson, Samantha (8 June 2024). "At long last: Europe's new Ariane 6 rocket set to debut on July 9". Space.com. Archived from the original on 8 June 2024. Retrieved 8 June 2024.
  5. ^ "Ariane 6 Vinci engine: successful qualification tests". ArianeGroup (Press release). 22 October 2018. Archived from the original on 17 June 2024. Retrieved 11 July 2024.
  6. ^ Next Ariane 6 launch slips to early 2025, Jeff Foust, SpaceNews, 8 November 2024.