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 of America
surface form: 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 Space Force Station
surface form: Cape Canaveral Air Force Station
launchVehicle Saturn I
surface form: Saturn I Block I

Saturn I
surface form: Saturn I Block II
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
surface form: Saturn IB first stage
successRate 10 of 10 flights reached planned test objectives
high
thrustAtLiftoff about 1,500,000 lbf
about 6.7 MN
usedFor Apollo program
surface form: Apollo program test flights

heavy-lift launch vehicle development
suborbital test flights
usedInMission SA-1
SA-10
SA-2
SA-2
surface form: SA-3

SA-4
SA-4
surface form: SA-5

SA-6
SA-7 Grail man-portable air-defense system
surface form: 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.