The Atlas I was a US expendable launch system manufactured by General Dynamics in the 1990s to launch a variety of satellites.
Specifications
- Thrust
- 1,939 kN
- Height
- 43.9 m
- Diameter
- 3.05 m
- Launch mass
- 164 t
- Stages
- 2
- Launch cost
- —
- LEO capacity
- 5,900 kg
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
11
Launches with a definitive outcome
Success rate
81.8%
9 of 11
Current success streak
7
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 I | GOES 10 — Success
- Atlas I | BeppoSAX — Success
- Atlas I | GOES 9 — Success
- Atlas I | UHF F/O F3 — Success
- Atlas I | GOES 8 — Success