ABOUT SATURN I
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.
PAYLOAD CAPACITY
9,100 kg
TO LEO
20,066 lbs
LIFTOFF THRUST
6,700
KILONEWTONS
1,506,220
POUNDS-FORCE
~8,985
HORSEPOWER