S-I

E259958

S-I was the first-stage booster of NASA’s early Saturn I launch vehicle, providing the initial thrust for some of the United States’ first heavy-lift test flights in the Apollo era.

All labels observed (2)

Label Occurrences
S-I canonical 1
S-I first stage 1

How this entity was disambiguated

Statements (52)

Predicate Object
instanceOf launch vehicle first stage ⓘ
rocket stage ⓘ
coreTankOrigin Jupiter rocket tank ⓘ
countryOfOrigin United States ⓘ
designer Wernher von Braun ⓘ
developedBy Marshall Space Flight Center ⓘ
diameter 6.52 m ⓘ
engineArrangement cluster of eight engines ⓘ
engineType H-1 ⓘ
era early Apollo era ⓘ
firstFlightDate 1961-10-27 ⓘ
firstFlightWith SA-1 ⓘ
fuel RP-1 kerosene ⓘ
guidanceLocation instrument unit on upper stage ⓘ
height about 25.5 m ⓘ
lastFlightDate 1965-07-30 ⓘ
lastFlightWith SA-10 ⓘ
launchComplex Launch Complex 34 ⓘ
Launch Complex 37 ⓘ
launchSite Cape Canaveral Air Force Station ⓘ
launchVehicle Saturn I Block I ⓘ
linked to: Saturn I

Saturn I Block II ⓘ
linked to: Saturn I
numberOfEngines 8 ⓘ
numberOfFlights 10 ⓘ
numberOfOuterTanks 8 ⓘ
operator NASA ⓘ
outerTankOrigin Redstone rocket tanks ⓘ
oxidizer liquid oxygen ⓘ
partOf Saturn I ⓘ
program Saturn program ⓘ
propellantType liquid fuel ⓘ
replacedBy S-IB ⓘ
status retired ⓘ
structureType clustered tank design ⓘ
successor Saturn IB first stage ⓘ
linked to: Saturn IB
successRate 10 of 10 flights reached planned test objectives ⓘ
high ⓘ
thrustAtLiftoff about 1,500,000 lbf ⓘ
about 6.7 MN ⓘ
usedFor Apollo program test flights ⓘ
linked to: Apollo program

heavy-lift launch vehicle development ⓘ
suborbital test flights ⓘ
usedInMission SA-1 ⓘ
SA-10 ⓘ
SA-2 ⓘ
SA-3 ⓘ
linked to: SA-2

SA-4 ⓘ
SA-5 ⓘ
linked to: SA-4

SA-6 ⓘ
SA-7 ⓘ
SA-8 ⓘ
SA-9 ⓘ

How these facts were elicited

Referenced by (2)

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

SA-1 → stageTested → S-I first stage ⓘ
linked to: S-I