ABOUT ATLAS V 421
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.
PAYLOAD CAPACITY
14,067 kg
TO LEO
31,018 lbs
6,890 kg
TO GTO
15,192 lbs
DIMENSIONS
Height58.3 m (191 ft)
Diameter3.8 m (12.5 ft)
Launch Mass433 kg (955 lbs)
Stages2
Apogee40,000 km
SATELLITES DEPLOYED (1)
⚙ RELATED ENGINES
🚀 OTHER UNITED LAUNCH ALLIANCE VEHICLES