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Space · launch vehicle

Atlas V 511

ULA RETIRED
At a glance
Launches
1
Success rate
100%
1 ok · 0 failed
Payload to LEO
10,986 kg
Payload to GTO
5,250 kg
Status
Retired
First flight
21 Jan 2022
Reusable
No
Height
58.3 m
Diameter
3.81 m
Launch mass
590 t
Liftoff thrust
5,490 kN
Stages
2
Launch cost
$130,000,000
Booster landings
—
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.