Rockets

Atlas·Convair

Atlas V

active
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Specifications

Status
active
Height
60 m
Mass
650,000 kg
Stages
2
Thrust
3,826 kN
Total launches
0
Success / Fail
0 / 0

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.

Propulsion

Boosters

GEM 631,663 kN
solid (HTPB) · solid
Northrop GrummanIsp 279s (vac)since 20200–5 strap-ons

First stage

RD-1803,830 kN
RP-1 / LOX · staged-combustion
NPO EnergomashIsp 338s (vac)since 2000

Second stage

RL10110 kN
LH2 / LOX · expander
Aerojet RocketdyneIsp 451s (vac)since 1963Centaur