Atlas V with 4m fairing, 1 SRB, 1 Centaur upper stage engine.
Specifications
- Thrust
- —
- Height
- 58.3 m
- Diameter
- 3.8 m
- Launch mass
- —
- Stages
- 2
- Launch cost
- $115M
- LEO capacity
- 8,080 kg
- GTO capacity
- 5,950 kg
- GEO capacity
- 1,935 kg
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
6
Launches with a definitive outcome
Success rate
100%
6 of 6
Current success streak
6
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 411 | Solar Orbiter — Success
- Atlas V 411 | SBIRS GEO Flight 4 (SBIRS GEO-3) — Success
- Atlas V 411 | OSIRIS-REx — Success
- Atlas V 411 | NROL-34 (2 x NOSS (USA-229)) — Success
- Atlas V 411 | NROL-28 (USA-200) — Success