Atlas LV-3C Centaur D
Atlas familyConvairRetired
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
- Stages
- 2
- GTO capacity
- 1,800 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
7flightswith a definitive outcome
100%success rate7 of 7
0failuresincluding partial failures
7success streakcurrent
First flight August 11, 1965 · latest July 14, 1967
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Atlas Centaur D flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 1965 | 1 | 0 | 1 |
| 1966 | 4 | 0 | 4 |
| 1967 | 2 | 0 | 2 |