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Atlas V 552 – United Launch Alliance

  • Family: Atlas
  • Length: 58.3 m
  • Diameter: 3.81 m
  • Low Earth Orbit Capacity: 20520 kg

The Atlas V 552 was manufactured by United Launch Alliance with the first launch on . Atlas V 552 has 0 successful launches and 0 failed launches with a total of 0 launches. 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 552 version uses a 5m wide fairing, 5 solid rocket boosters and two engines on the Centaur stage.

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