Skip to main content

Ariane 6 Launch System Operational Concept Main Drivers

  • Chapter
  • First Online:
Space Operations: Inspiring Humankind's Future

Abstract

The European launchers belonging to the Ariane and Vega families are leaders on the commercial launch services market, with demonstrated high reliability after a very lengthy run of successful flights. Ariane 6 is the next-generation heavy-lift European launch system in the Ariane family. It is being developed with the objectives of providing users with high mass lift-capability performance, mission versatility, operational flexibility, high launch rate and low launch service cost. The European Space Agency (ESA), in its role as Launch System Architect (LSA), is in charge of ensuring the coherence between the launcher and the launch base and of verifying the launch system performance to reach those objectives. With this goal, the Launch System Architect (ESA), the launcher prime (ArianeGroup) and the launch base prime (CNES) are working together on building up an optimised launch operations plan. The launch operations plan starts with the arrival at the launch range of the launcher elements and the spacecraft to be launched together with its support ground equipment. It ends with the post-flight analysis, the launch facilities’ revalidation and their reconfiguration for the following launch. To ensure that the above-mentioned challenging set of objectives is met, the launch preparation and launch operations concept (“Operational Concept” or CONOPS) will be designed taking the mission cost as the main driver and pursuing the same service quality and reliability as that provided by Ariane 5 today. Therefore, with a view to customer needs, the CONOPS is being constantly optimised to minimise waste. The optimisation of CONOPS is being done while complying with the safety requirements imposed by the applicable law and regulations which ultimately constitute a guarantee of operational system robustness. This paper presents the drivers established to build the Ariane 6 Operational Concept, the related trade-offs performed and the rationale for the selected choices. Lastly, some aspects of the preliminary operations plan resulting from the CONOPS exercise are compared with former Ariane operations plans to show differences and highlight improvements with respect to users’ expectations.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 189.00
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Hardcover Book
USD 249.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Abbreviations

BAL:

Launcher assembly building

CC:

[Launcher] central core

CONOPS:

Concept of Operations (Operational Concept)

COP:

Combined operations plan

CSG:

Guiana Space Centre

ELA4:

Ariane launch complex 4

EMC:

Electro Magnetic Compatibility

ESR:

Equipped solid rocket

FSOA:

French Space Operations Act

LLPM:

Lower liquid propulsion module

LS:

Launch system

L/V:

Launch vehicle

MG:

Mobile gantry

PDCA:

Plan-Do-Check-Act

P/L:

Payload

PPF:

Payload preparation facilities

RLOX:

Liquid oxygen tank

UC:

Upper Composite

ULPM:

Upper liquid propulsion module

ZL:

Launch Zone

Reference

  1. Resta, P. D., Pilchen, G., Coulon, D., et al. (2016). The Ariane 6 Launch System Development Status. In 67th International Astronautical Congress (IAC). Guadalajara, Mexico, 26–30 September 2016.

    Google Scholar 

Download references

Acknowledgements

The ESA authors wish to thank ArianeGroup and CNES for this cooperative work effort allowing the Ariane 6 time and cost targets to be met.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Pier Domenico Resta .

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2019 Springer Nature Switzerland AG

About this chapter

Check for updates. Verify currency and authenticity via CrossMark

Cite this chapter

Resta, P.D., Monreal, J.A., Pouffary, B., Lemercier, S., Decadi, A., Arnoud, E. (2019). Ariane 6 Launch System Operational Concept Main Drivers. In: Pasquier, H., Cruzen, C., Schmidhuber, M., Lee, Y. (eds) Space Operations: Inspiring Humankind's Future. Springer, Cham. https://doi.org/10.1007/978-3-030-11536-4_5

Download citation

  • DOI: https://doi.org/10.1007/978-3-030-11536-4_5

  • Published:

  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-030-11535-7

  • Online ISBN: 978-3-030-11536-4

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics