Atlas V is the fifth major version in the Atlas rocket family. It is an expendable launch system originally designed by Lockheed Martin, now being operated by United Launch Alliance (ULA), a joint venture between Lockheed and Boeing.
Specifications
- Thrust
- 7,203 kN
- Height
- 58.3 m
- Diameter
- 3.81 m
- Launch mass
- 590 t
- Stages
- 2
- Launch cost
- $135M
- LEO capacity
- 13,490 kg
- GTO capacity
- 6,475 kg
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
2
Launches with a definitive outcome
Success rate
100%
2 of 2
Current success streak
2
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
—
Between consecutive booster flights
Counted from padside's own launch record — the same basis as the Stats page.
Launches
- Atlas V 521 | AMC 16 — Success
- Atlas V 521 | Rainbow 1 — Success