🚀Launchpad

Atlas V 421

United Launch Alliance

Hersteller
United Launch Alliance
Familie
Atlas, Atlas V
Erstflug
2007-10-11
Länge
58.3 m
Durchmesser
3.8 m
Nutzlast LEO
14.067 kg
Nutzlast GTO
6.890 kg
Starts
9
Erfolgreich
9

Atlas V is an expendable launch system in the Atlas rocket family. It was formerly operated by Lockheed Martin and is now operated by United Launch Alliance (ULA), a joint venture with Boeing. Each Atlas V rocket uses a Russian-built RD-180 engine burning kerosene and liquid oxygen to power its first stage and an American-built RL10 engine burning liquid hydrogen and liquid oxygen to power its Centaur upper stage. The RD-180 engines are provided by RD Amross, while Aerojet Rocketdyne provides both the RL10 engines and the strap-on boosters used in some configurations. The 421 version uses a 4m wide fairing, 2 solid rocket boosters and one engine on the Centaur stage.