Atlas SLV-3C Centaur
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
- 1,939 kN
- Height
- 21 m
- Diameter
- 3.05 m
- Launch mass
- 120 t
- Stages
- 2
- LEO capacity
- 800 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
17flightswith a definitive outcome
88.2%success rate15 of 17
6success streakcurrent
Counted from padside's own launch record, the same basis as the stats page.