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 (1)

Label Occurrences
S-I canonical 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 (1)

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