Launch Vehicles

Description

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Electron is a two-stage orbital expendable launch vehicle (with an optional third stage) developed by the American aerospace company Rocket...

The Falcon 1 was the first launch vehicle developed and manufactured by SpaceX in 2006. It is an expendable, two stage rocket where each st...

The Full Thrust variants first stage includes all systems necessary for an operational re-use of stages while the second stage is operated...

Falcon 9 is a two-stage rocket designed and manufactured by SpaceX for the reliable and safe transport of satellites and the Dragon spacecr...

The Full Thrust variants first stage includes all systems necessary for an operational re-use of stages while the second stage is operated...

The Falcon 9 v1.0 first stage was used on the first five Falcon 9 launches, and powered by nine SpaceX Merlin 1C rocket engines arranged in...

Falcon 9 v1.1 is a significantly redesigned version of the its predecessor, including a higher payload capacity. This version arranges the...

The Falcon Heavy is a variant of the Falcon 9 full thrust launch vehicle and consists of a standard Falcon 9 rocket core, with two addition...

Firefly Alpha (Firefly α) is a two-stage orbital expendable launch vehicle developed by the American aerospace company Firefly Aerospace to...

Firefly Alpha (Firefly α) is a two-stage orbital expendable launch vehicle developed by the American aerospace company Firefly Aerospace to...

Juno II was an American space launch vehicle used during the late 1950s and early 1960s. It was derived from the Jupiter missile, which was...

The Juno I was a four-stage American booster rocket which launched America's first satellite, Explorer 1 in 1958. A member of thr redstone...

LauncherOne is a two stage orbital launch vehicle developed by Virgin Orbit since 2007. It is an air launch to orbit rocket, designed to la...

Little Joe was a solid-fueled booster rocket used by NASA for eight launches from 1959-1960 from Wallops Island, Virginia to test the launc...

American rocket used from 1963 to 1966 for five uncrewed suborbital tests of the Apollo spacecraft launch escape system and of the command...

The Minotaur I launch system is derived from converted Minuteman II ICBMs and is used to launch small satellites for the US Government. The...

The Minotaur IV launch system is derived from the Peacekeeper ICBM. The first three stages are taken directly from decommissioned Peacekeep...

The Minotaur IV HAPS launch system is derived from the Peacekeeper ICBM. The first three stages are taken directly from decommissioned Peac...

The Minotaur IV+ launch system is derived from the Peacekeeper ICBM. The first three stages are taken directly from decommissioned Peacekee...

American all-solid orbital launch vehicle based on a Pegasus and Peacekeeper rocket.It has been designed as a quick reaction launch vehicle...

American all-solid orbital launch vehicle based on a Pegasus and Peacekeeper rocket.It has been designed as a quick reaction launch vehicle...

American all-solid orbital launch vehicle based on a Pegasus and Peacekeeper rocket.It has been designed as a quick reaction launch vehicle...

American all-solid orbital launch vehicle based on a Pegasus and Peacekeeper rocket.It has been designed as a quick reaction launch vehicle...

American all-solid orbital launch vehicle based on a Pegasus and Peacekeeper rocket.It has been designed as a quick reaction launch vehicle...

Neutron is an upcoming medium-lift two-stage launch vehicle under development by Rocket Lab. Neutron features a reusable first stage fueled...

The New Glenn is a privately funded orbital launch vehicle in development by Blue Origin. New Glenn is described as a 7-meter-diameter (23...

The New Glenn 9x4 is a further enhanced variant of the current New Glenn rocket (the "7x2" configuration) by Blue Origin. The New Glenn 9x4...

The New Shepard reusable launch system is a vertical-takeoff, vertical-landing (VTVL), suborbital manned rocket that is being developed by...