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
- 1,704 kN
- Height
- 33 m
- Diameter
- 3.05 m
- Launch mass
- —
- Stages
- 2
- Launch cost
- —
- LEO capacity
- —
- GTO capacity
- 1,800 kg
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
7
Launches with a definitive outcome
Success rate
100%
7 of 7
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 Centaur D | Surveyor 4 — Success
- Atlas Centaur D | Surveyor 3 — Success
- Atlas Centaur D | Surveyor Model 3 — Success
- Atlas Centaur D | Surveyor 2 — Success
- Atlas Centaur D | Surveyor 1 — Success