Atlas V 4 Vehicle Overview
A complete overview of the Atlas V 4 launch vehicle, including launch stats, vehicle info and launch locations.
![Atlas V N22 rocket](https://spacelaunchnow-prod-east.nyc3.digitaloceanspaces.com/media/launcher_images/atlas_v_n22_image_20210813082339.jpeg)
Basic Info
Name
Atlas V 4
Family
Atlas
Manufacturer
First Launch
21 Aug 2002
Successful Launches
62
Failed Launches
0
Rocket Info (Atlas V N22)
Status
Active
Stages
2
Length
58 m
Diameter
3.8 m
Reusability
Not Reusable
Payload Info (Atlas V N22)
LEO Capacity
13,034 kg
Launch Cost
$110M
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 4 versions use a 4m wide fairing.
Launch Sites used by Atlas V 4
Cape Canaveral Space Force Station
![Cape Canaveral Space Force Station launch site](https://rocket-launch-today.s3.us-east-1.amazonaws.com/cape_canaveral_space_force_station_09be931494.jpg)
Historic U.S. military rocket launch site, pivotal in space exploration and national security.
Vandenberg SFB
![Vandenberg SFB launch site](https://rocket-launch-today.s3.us-east-1.amazonaws.com/vandenberg_sfb_f5f6115752.jpeg)
U.S. Space Force facility in California for spacecraft launches and missile testing.