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
Manufacturer
United Launch AllianceStatus
RetiredFirst flight
11 Oct 2007Reusable
NoHeight
58.3 mDiameter
3.8 mLaunch mass
433 tLiftoff thrust
—Stages
2Launch cost
$123,000,000Booster 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.
Source The Space Devs — Launch Library 2
Last checked 29 Sept 2026
