Saturn I

E46120

American space launch vehicle expendable launch vehicle rocket

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.

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All labels observed (14)

Label	Occurrences
Saturn I canonical	18
Saturn IB	4
Saturn I Block II	3
Saturn I rocket	2
Saturn I Block I	1
Saturn I SA-10	1
Saturn I SA-5	1
Saturn I SA-6	1
Saturn I SA-7	1
Saturn I SA-8	1
Saturn I SA-9	1
Saturn I first stage	1
Saturn I first stage S-I	1
Saturn I program	1

Statements (48)

Predicate	Object
instanceOf	American space launch vehicle ⓘ expendable launch vehicle ⓘ rocket ⓘ
configuration	two-stage rocket ⓘ
countryOfOrigin	United States of America ⓘ surface form: 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 Kennedy Air Force Station Launch Complex 34 ⓘ surface form: Cape Canaveral Air Force Station Launch Complex 34 Cape Canaveral LC-37B ⓘ surface form: Cape Canaveral Air Force Station Launch Complex 37
liftoffMass	about 460000 kg ⓘ
liftoffThrust	about 6800 kN ⓘ
manufacturer	Chrysler ⓘ
namedAfter	Saturn ⓘ surface form: Saturn (planet)
notablePayload	Apollo boilerplate spacecraft ⓘ Pegasus micrometeoroid satellites ⓘ
operator	Marshall Space Flight Center ⓘ surface form: 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	RL10 ⓘ surface form: 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 ⓘ

Referenced by (37)

Full triples — surface form annotated when it differs from this entity's canonical label.

Apollo program → launchVehicle → Saturn I ⓘ

this entity surface form: Saturn IB

Saturn V → predecessor → Saturn I ⓘ

this entity surface form: Saturn IB

Skylab program → launchVehicleUsed → Saturn I ⓘ

this entity surface form: Saturn IB

Kennedy Space Center Launch Complex 39A → launchVehicleSupported → Saturn I ⓘ

this entity surface form: Saturn IB

Wernher von Braun → notableWork → Saturn I ⓘ

this entity surface form: Saturn I rocket

Apollo astronauts → usedLaunchVehicle → Saturn I ⓘ

United States rocket program → developed → Saturn I ⓘ

this entity surface form: Saturn I rocket

RP-1 → usedIn → Saturn I ⓘ

Redstone rocket → successor → Saturn I ⓘ

S-IVB → partOf → Saturn I ⓘ

S-IVB → developedFor → Saturn I ⓘ

this entity surface form: Saturn I Block II

J-2 → usedOn → Saturn I ⓘ

Mimas → catalogDesignation → Saturn I ⓘ

Saturn IB → relatedVehicle → Saturn I ⓘ

LC-34 → rocketLaunched → Saturn I ⓘ

S-I → partOf → Saturn I ⓘ

S-I → launchVehicle → Saturn I ⓘ

this entity surface form: Saturn I Block I

S-I → launchVehicle → Saturn I ⓘ

this entity surface form: Saturn I Block II

S-IV → partOf → Saturn I ⓘ

S-IV → firstFlightVehicle → Saturn I ⓘ

this entity surface form: Saturn I Block II