An Atlas V with a 4 meter diameter fairing, no boosters and a single centaur upper stage engine.
Specifications
- Thrust
- 3,827 kN
- Height
- 58.3 m
- Diameter
- 3.8 m
- Launch mass
- 590 t
- Stages
- 2
- Launch cost
- $115M
- LEO capacity
- 9,050 kg
- GTO capacity
- 4,950 kg
- GEO capacity
- —
- SSO capacity
- 6,670 kg
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
41
Launches with a definitive outcome
Success rate
100%
41 of 41
Current success streak
41
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 401 | JPSS 2 (Joint Polar Satellite System spacecraft No. 2) & LOFTID — Success
- Atlas V 401 | Lucy — Success
- Atlas V 401 | Landsat 9 — Success
- Atlas V 401 | InSight, Mars Cube One 1 & Mars Cube One 2 — Success
- Atlas V 401 | TDRS-M — Success