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
- Launch cost
- —
- LEO capacity
- 800 kg
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
4
Launches with a definitive outcome
Success rate
100%
4 of 4
Current success streak
4
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-3 | PRIME 3 — Success
- Atlas SLV-3 | PRIME 2 — Success
- Atlas SLV-3 | PRIME 1 — Success
- Atlas SLV-3 | ATDA — Success