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Atlas V N22
United Launch Alliance
Atlas V N22 is a configuration of the Atlas V launch vehicle with no solid rocket boosters and a 2-engine Centaur upper stage. Known for reliability and precision in delivering payloads to orbit.
First Flight
August 21, 2002
Total Launches
15
Success Rate
100%
Stages
2
Technical Specifications
Dimensions
Height
58.3 m / 191 ft
Diameter
3.81 m / 12.5 ft
Mass
Total Mass
334,500 kg
737,400 lb
Payload Capacity
LEO
9,800 kg
21,605 lb
GTO
4,750 kg
10,472 lb
Thrust
Liftoff Thrust
3,827 kN
860,200 lbf