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Vega-C (Avio S.p.A)

Vega-C is a single-body rocket nearly 35 m high with that weighs 210 tonnes on the launch pad. As with Vega, its main elements are three solid-propellant stages, an upper stage powered by a reignitabl…

Vikram-I (Skyroot Aerospace)

4-stage orbital launch vehicle developed by Indian private company Skyroot Aerospace, with capability of up to 350 kg to Low Earth Orbit. The first 3 stages are powered by solid fuel rocket motors, to…

Volna (Makeyev Rocket Design Bureau)

Space launch vehicle Volna is a converted Submarine-launched ballistic missile used for launching satellites into orbit. It is based on the R-29R designed by State Rocket Center Makayev and related to…

Vostok 8A92 (RKK Energiya)

Vostok was a family of rockets derived from the Soviet R-7 Semyorka ICBM and was designed for the human spaceflight programme….

Vostok 8A92M (RKK Energiya)

Vostok was a family of rockets derived from the Soviet R-7 Semyorka ICBM and was designed for the human spaceflight programme….

Vostok 8K72 (RKK Energiya)

Vostok was a family of rockets derived from the Soviet R-7 Semyorka ICBM and was designed for the human spaceflight programme….

Vostok-K (Soviet Space Program)

The Vostok-K was an expendable carrier rocket used by the Soviet Union for thirteen launches between 1960 and 1964, six of which were manned.

The Vostok-K made its maiden flight on 22 Decem…

Vostok-L 8K72 (Energia)

The Vostok-L was a rocket used by the Soviet Union to conduct several early tests of the Vostok spacecraft…

Vulcan VC2S (United Launch Alliance)

Vulcan Centaur is a two-stage-to-orbit, heavy-lift launch vehicle under development by United Launch Alliance (ULA) since 2014. It is principally designed to meet launch demands for the U.S. governmen…