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Atlas V 421

Atlas familyUnited Launch AllianceRetired

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.

Atlas V 421 vehicle

Specifications

Thrust
7,204 kN
Height
58.3 m
Diameter
3.8 m
Launch mass
433 t
Stages
2
Launch cost
$123M
LEO capacity
14,067 kg
GTO capacity
6,890 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

9flightswith a definitive outcome
100%success rate9 of 9
9success streakcurrent

Counted from padside's own launch record, the same basis as the stats page.

Flights

5 of 9

All 9 flights