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Atlas V 401
🇺🇸EELV
1:110 Scale
H:53.0 cmD:3.5 cm
~55 bricks tall~4 studs wide
Maiden Launch2002-08-21
2 Stages
Height / Length
58.3 m
Diameter
3.8 m
Launch Mass
334,000 kg
Takeoff Thrust
3,827 kN
LEO Capacity
9,750 kg
GTO Capacity
4,750 kg
Mission Profile
The Atlas V 401 is a two-stage American launch vehicle in the Atlas family, the baseline configuration with no solid rocket boosters and a 4 m diameter payload fairing under the EELV programme. Standing 58.3 m tall with a 3.8 m core diameter and a liftoff mass of 334 tonnes, it generates 3,827 kN of liftoff thrust and can deliver 9,750 kg to low Earth orbit or 4,750 kg to geostationary transfer orbit. First flying in August 2002 as the inaugural Atlas V mission, the Atlas V 401 has been the most frequently launched configuration, deploying commercial, military, and NASA payloads with near-perfect reliability.
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