The Atlas-Centaur was a US expendable launch vehicle derived from the SM-65 Atlas D missile. Launches were conducted from Launch Complex 36 at the Cape Canaveral Air Force Station in Florida.
Specifications
- Thrust
- —
- Height
- 21 m
- Diameter
- 3.05 m
- Launch mass
- 120 t
- Stages
- 2
- Launch cost
- —
- LEO capacity
- 800 kg
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
32
Launches with a definitive outcome
Success rate
93.8%
30 of 32
Current success streak
19
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 SLV-3D Centaur | Intelsat 506 — Success
- Atlas SLV-3D Centaur | Intelsat 505 — Success
- Atlas SLV-3D Centaur | Intelsat 504 — Success
- Atlas SLV-3D Centaur | Intelsat 503 — Success
- Atlas SLV-3D Centaur | FLTSATCOM 5 — Success