Atlas·Convair
Atlas V 511
active
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Specifications
- Status
- active
- Height
- 58.3 m
- Diameter
- 3.81 m
- Mass
- 590,000 kg
- Stages
- 2
- Thrust
- 5,490 kN
- Payload to LEO
- 10,986 kg
- Payload to GTO
- 5,250 kg
- First flight
- 2022-01-21
- Total launches
- 1
- Success / Fail
- 1 / 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 511 version uses a 5m wide fairing, 1 solid rocket booster and one engine on the Centaur stage.
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
Payloads it launched
2 loaded