The Atlas-Agena was an American expendable launch system derived from the SM-65 Atlas missile. It was a member of the Atlas family of rockets, and was launched 109 times between 1960 and 1978.
Specifications
- Thrust
- 1,340 kN
- Height
- 36 m
- Diameter
- 3 m
- Launch mass
- 155 t
- Stages
- 2
- Launch cost
- —
- LEO capacity
- 1,000 kg
- GTO capacity
- —
- GEO capacity
- 700 kg
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
48
Launches with a definitive outcome
Success rate
91.7%
44 of 48
Current success streak
25
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 Agena D | ATS 3 — Success
- Atlas SLV-3 Agena D | Lunar Orbiter 5 — Success
- Atlas SLV-3 Agena D | Mariner 5 — Success
- Atlas SLV-3 Agena D | KH-7 38 — Success
- Atlas SLV-3 Agena D | KH-7 37 — Success