The Saturn I was a rocket designed as the United States' first medium lift launch vehicle for up to 20,000-pound (9,100 kg) low Earth orbit payloads.
Specifications
- Thrust
- 6,700 kN
- Height
- 55 m
- Diameter
- 6.6 m
- Launch mass
- 510 t
- Stages
- 3
- Launch cost
- —
- LEO capacity
- 9,100 kg
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
10
Launches with a definitive outcome
Success rate
100%
10 of 10
Current success streak
10
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
- Saturn I | Pegasus 3 — Success
- Saturn I | Pegasus 2 — Success
- Saturn I | Pegasus 1 — Success
- Saturn I | Saturn-SA 7 — Success
- Saturn I | Saturn-SA 6 — Success