Atlas V with 5m Fairing, 3 SRB, 1 Centaur upper stage engine.
Specifications
- Thrust
- —
- Height
- 60 m
- Diameter
- 3.8 m
- Launch mass
- 479 t
- Stages
- 2
- Launch cost
- $140M
- LEO capacity
- 15,530 kg
- GTO capacity
- 7,450 kg
- GEO capacity
- 3,080 kg
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
5
Launches with a definitive outcome
Success rate
100%
5 of 5
Current success streak
5
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 531 | SES-20 & SES-21 — Success
- Atlas V 531 | NROL-101 — Success
- Atlas V 531 | AEHF-3 (USA-246) — Success
- Atlas V 531 | AEHF-2 (USA-235) — Success
- Atlas V 531 | AEHF-1 (USA-214) — Success