Atlas V with 5m Fairing, 4 SRB, 1 Centaur upper stage engine.
Specifications
- Thrust
- —
- Height
- 60 m
- Diameter
- 3.8 m
- Launch mass
- 479 t
- Stages
- 2
- Launch cost
- $145M
- LEO capacity
- 17,410 kg
- GTO capacity
- 8,290 kg
- GEO capacity
- 3,530 kg
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
9
Launches with a definitive outcome
Success rate
100%
9 of 9
Current success streak
9
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 541 | USSF-12 — Success
- Atlas V 541 | GOES-T — Success
- Atlas V 541 | Mars 2020 (Perseverance rover & Ingenuity helicopter) — Success
- Atlas V 541 | GOES-S — Success
- Atlas V 541 | NROL-42 — Success