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 511 version uses a 5m wide fairing, 1 solid rocket booster and one engine on the Centaur stage.

SPECIFICATIONS 11
Length 58.3 m
Diameter 3.81 m
Launch Mass T 590
Leo Capacity 10,986 kg
Gto Capacity 5,250 kg
Thrust 5,490 kN
Launch Cost Usd 130,000,000
Reusable No
Total Launches 1
Successful Launches 1
Maiden Flight 2022-01-21