United Launch Alliance

Atlas V 551

551

Atlas V 551
Active

Overview

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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 standard payload fairing sizes are 4 or 5 meters in diameter and of various lengths. Fairings sizes as large as 7.2 m in diameter and up to 32.3 m in length have been considered. The rocket is assembled in Decatur, Alabama and Harlingen, Texas.

Manufacturer

United Launch Alliance

Variant

551

Alias

N/A

Maiden Flight

January 19, 2006

Technical Specifications

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59.7 m

Length

3.8 m

Diameter

1 t

Launch Mass

12269 kN

Liftoff Thrust

18850 kg

LEO Capacity

8890 kg

GTO Capacity

Launch Record

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19

Total Launches

19

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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