Saturn I

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Saturn I was an early American expendable launch vehicle developed by NASA that served as a precursor to the more powerful Saturn IB and Saturn V rockets used in the Apollo program.

Aliases (2)

Statements (48)
Predicate Object
instanceOf American space launch vehicle
expendable launch vehicle
rocket
configuration two-stage rocket
countryOfOrigin United States
designFeature clustered first stage using Redstone and Jupiter tankage
designLead Wernher von Braun
developer NASA
diameter 6.52 m
era early 1960s
failedLaunches 0
firstFlightDate 1961-10-27
firstStageEngines 8
firstStageEngineType Rocketdyne H-1
firstStageFuel RP-1
firstStageName S-I
firstStageOxidizer liquid oxygen
height 55 m
lastFlightDate 1965-07-30
launchSitesUsed Cape Canaveral Air Force Station Launch Complex 34
Cape Canaveral Air Force Station Launch Complex 37
liftoffMass about 460000 kg
liftoffThrust about 6800 kN
manufacturer Chrysler
namedAfter Saturn (planet)
notablePayload Apollo boilerplate spacecraft
Pegasus micrometeoroid satellites
operator NASA Marshall Space Flight Center
partOf Saturn rocket family
predecessorOf Saturn IB
Saturn V
primaryUse development of large launch vehicle technology
test flights for Apollo program
program Apollo program
propellantTypeFirstStage RP-1/LOX
propellantTypeSecondStage liquid hydrogen/liquid oxygen
secondStageEngines 6
secondStageEngineType RL10A-3
secondStageFuel liquid hydrogen
secondStageName S-IV
secondStageOxidizer liquid oxygen
status retired
successfulLaunches 10
successor Saturn IB
Saturn V
totalLaunches 10
usedFor testing Apollo spacecraft structural and dynamic loads
validating orbital operations for Apollo hardware


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