American orbital launch vehicle used between 2000 and 2005.
Specifications
- Thrust
- 4,149 kN
- Height
- 52.8 m
- Diameter
- 3.05 m
- Launch mass
- 213 t
- Stages
- 2
- Launch cost
- —
- LEO capacity
- 10,218 kg
- GTO capacity
- 4,498 kg
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
4
Launches with a definitive outcome
Success rate
100%
4 of 4
Current success streak
4
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 | NROL-23 — Success
- Atlas | UHF F/O F11 — Success
- Atlas | Asiasat 4 — Success
- Atlas | Echostar VII — Success