Atlas V with 4m Fairing, 3 SRB, 1 Centaur upper stage engine.
Specifications
- Thrust
- —
- Height
- 59.1 m
- Diameter
- 3.8 m
- Launch mass
- 479 t
- Stages
- 2
- Launch cost
- $130M
- LEO capacity
- 15,260 kg
- GTO capacity
- 7,700 kg
- GEO capacity
- 2,820 kg
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
3
Launches with a definitive outcome
Success rate
100%
3 of 3
Current success streak
3
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 431 | Echostar 19 (Jupiter-2) — Success
- Atlas V 431 | Intelsat 14 — Success
- Atlas V 431 | INMARSAT 4 F1 — Success