Saturn family

Saturn I

RetiredUnited StatesChryslerSpec: 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.

Flights flown10
Success rate100%10/10
Payload to LEO9,100kg
Maiden flight1961-10-27
Peak year19643 flights

Saturn I is built by Chrysler of the United States. It first flew on 27 October 1961 and last flew on 30 July 1965.

Flight record

10 records
100% success rate10 of 10 flown
1961peak 1964 · 3 flights1965
First flight1961-10-27
Latest flight1965-07-30
Failures0
Consecutive successes10
Fastest turnaround66d 5h

Payload

Per mission profile
Low Earth orbit9,100kg

Vehicle

I spec
Stages3
Length55m
Diameter6.6m
Launch mass510t
Liftoff thrust6,700kN
Maiden flight1961-10-27
ReusableNo

Pads used

2 pads

Orbits delivered

2 orbits
Low Earth Orbit6Suborbital4

Launch history

10 launches
DateMissionPadOrbitOutcome
1965-07-30Saturn I | Pegasus 3Space Launch Complex 37BLow Earth OrbitSuccess
1965-05-25Saturn I | Pegasus 2Space Launch Complex 37BLow Earth OrbitSuccess
1965-02-16Saturn I | Pegasus 1Space Launch Complex 37BLow Earth OrbitSuccess
1964-09-18Saturn I | Saturn-SA 7Space Launch Complex 37BLow Earth OrbitSuccess
1964-05-28Saturn I | Saturn-SA 6Space Launch Complex 37BLow Earth OrbitSuccess
1964-01-29Saturn I | Saturn SA-5Space Launch Complex 37BLow Earth OrbitSuccess
1963-03-28Saturn I | Saturn SA-4Launch Complex 34SuborbitalSuccess
1962-11-16Saturn I | Saturn SA-3Launch Complex 34SuborbitalSuccess
1962-04-25Saturn I | Saturn SA-2Launch Complex 34SuborbitalSuccess
1961-10-27Saturn I | Saturn SA-1Launch Complex 34SuborbitalSuccess

Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.

Further reading: Wikipedia