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ELV in Italy proposes two microlauncher configurations that rely on propulsion common with Vega, and the next-generation Vega-C and -E launch vehicles. Sharing existing building blocks and those under development is aimed at reducing costs.
The Final Launch Vehicle comprises a Vega-C first-stage solid motor and a second stage using liquid oxygen–methane propellant common with the next-generation launcher, Vega-E.