ABOUT

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.

SPECIFICATIONS 10
Length 58.3 m
Diameter 3.8 m
Launch Mass T 433
Leo Capacity 14,067 kg
Gto Capacity 6,890 kg
Launch Cost Usd 123,000,000
Reusable No
Total Launches 9
Successful Launches 9
Maiden Flight 2007-10-11