Atlas SLV-3
Atlas familyConvairRetired
The Atlas SLV-3, or SLV-3 Atlas was an American expendable launch system derived from the SM-65 Atlas / SM-65D Atlas missile. It was a member of the Atlas family of rockets.
Specifications
- Thrust
- 3,824 kN
- Height
- 21 m
- Diameter
- 3.05 m
- Launch mass
- 120 t
- Stages
- 1
- LEO capacity
- 800 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
4flightswith a definitive outcome
100%success rate4 of 4
0failuresincluding partial failures
4success streakcurrent
First flight June 1, 1966 · latest April 20, 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 SLV-3 flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 1966 | 2 | 0 | 2 |
| 1967 | 2 | 0 | 2 |