Vega E

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Payload LEO

3,000 kg

Payload SSO

2,800 kg

Assessment

Evolution of the Vega family; replaces the two upper stages of the Vega C with a single upper stage powered by the LOX/methane M10 engine. Maiden flight targeted for 2027. SSO figure based on 700 km.

Source (provider information)

Technical data

Liftoff thrust4,323 kN

Stages3

PropellantSolid + LOX/methane (upper stage)

ReusabilityExpendable

Lead time–

Provider launch sites

Guiana Space Centre – Vega E launch facility (Kourou)Guiana Space Centre – Vega launch complex ELV/ZLV (Kourou)

Price

Price on request

To the provider: Avio

Prices shown are the providers' official figures and are always non-binding – only the individual quote is binding.