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Atlas V

ACTIVE
USA flag — Atlas V USA Official site external-link-icon-img
Atlas V launch vehicle, operated by United Launch Alliance

Built & Operated By

United Launch Alliance

Commercial · founded 2006

Family

Atlas

variant V · also Atlas V

About

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.

Vehicle Specifications

Height

60 m

Launch Mass

650 T

Thrust

3,826 kN

Stages

2

Configuration

Expendable

Launch Record

Total Launches

0

Successful

0

Failed

0

Performance

Launch Cost

$109.0M

Version: 2.21.8

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