American orbital launch vehicle used between 2000 and 2005.
Specifications
- Thrust
- 4,149 kN
- Height
- 52.8 m
- Diameter
- 3.05 m
- Launch mass
- 214 t
- Stages
- 2
- Launch cost
- —
- LEO capacity
- 8,640 kg
- GTO capacity
- 4,055 kg
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
2
Launches with a definitive outcome
Success rate
100%
2 of 2
Current success streak
2
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 Agena B | MBSAT — Success
- Atlas Agena B | Eutelsat W4 — Success