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Space · launch vehicle

Atlas V 421

ULA RETIRED
At a glance
Launches
9
Success rate
100%
9 ok · 0 failed
Payload to LEO
14,067 kg
Payload to GTO
6,890 kg
Status
Retired
First flight
11 Oct 2007
Reusable
No
Height
58.3 m
Diameter
3.8 m
Launch mass
433 t
Liftoff thrust
—
Stages
2
Launch cost
$123,000,000
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 421 version uses a 4m wide fairing, 2 solid rocket boosters and one engine on the Centaur stage.