Saturn I
Saturn familyChryslerRetired
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
- LEO capacity
- 9,100 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
10flightswith a definitive outcome
100%success rate10 of 10
10success streakcurrent
Counted from padside's own launch record, the same basis as the stats page.