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Avio · Operational · eu · Launch Vehicle

Vega-C

European small-lift launcher; returned to flight December 2024 after 2022 mission failure.

Verified 2026-09-24 · First flight 2022-07-13

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Systems cutaway

Systems
Vega-C — systems cutaway schematicPropulsion
P120C solid-propellant first stage (same as Ariane 6 strap-on); Zefiro-40 S2; Zefiro-9 S3; AVUM+ liquid upper stage; 4,323 kN liftoff thrust.
src ↗
Structures
3 m diameter; 34.8 m height; four-stage design.
src ↗
Vega-C34.8 m
Propulsion↗

P120C solid-propellant first stage (same as Ariane 6 strap-on); Zefiro-40 S2; Zefiro-9 S3; AVUM+ liquid upper stage; 4,323 kN liftoff thrust.

Structures↗

3 m diameter; 34.8 m height; four-stage design.

Specs & Metrics

Payload to LEO ↑ better
2,300 kg
Maximum payload mass deliverable to low Earth orbit (~200–400 km circular), in the vehicle's stated reference configuration.
Liftoff Thrust ↑ better
4323 kN
P120C first stage; some sources list ~4,500 kN
Total first-stage thrust at liftoff (sea-level), in kilonewtons, summing all active engines and solid strap-ons.
Liftoff Mass ↓ better
210 t
Total vehicle mass at liftoff including propellant, payload, and all stages, in metric tonnes.
Vehicle Height ↓ better
34.8 m
Full stack height at liftoff, in metres, including fairing or spacecraft.

Subsystems

propulsion↗

P120C solid-propellant first stage (same as Ariane 6 strap-on); Zefiro-40 S2; Zefiro-9 S3; AVUM+ liquid upper stage; 4,323 kN liftoff thrust.

structures↗

3 m diameter; 34.8 m height; four-stage design.

Program roadmap

Vega-C program roadmap2024-12-05AchievedReturn to flight after the fail…↗2026-05-19AchievedFirst Vega-C launch operated by…↗20242027
  • achieved

    Return to flight after the failure of its second mission at the end of 2022

    2024-12-05↗
  • achieved

    First Vega-C launch operated by Avio as launch service operator (VV29, SMILE)

    2026-05-19↗