United Launch Alliance

Atlas V

V

Atlas V
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

V

Alias

Atlas V

Maiden Flight

N/A

Technical Specifications

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60 m

Length

Diameter

1 t

Launch Mass

3826 kN

Liftoff Thrust

LEO Capacity

GTO Capacity

Launch Record

/03
0

Total Launches

0

Successful

0

Failed

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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