S-IVB

E130633

The S-IVB was the single-engine upper stage of NASA’s Saturn launch vehicles, used to place Apollo spacecraft into Earth orbit and send them toward the Moon.

All labels observed (6)

How this entity was disambiguated

Statements (45)

Predicate Object
instanceOf rocket stage
upper stage
burnCapability restartable in orbit
countryOfOrigin United States
developedFor Saturn I Block II
linked to: Saturn I
diameter 21.7 ft
6.6 m
era 1960s
1970s
expendedAs heliocentric orbit stage in some missions
impactor on the Moon in some missions
firstFlight 1964
fuelTankConfiguration common bulkhead between fuel and oxidizer tanks
guidanceSystem instrument unit mounted above stage
launchVehicleFamily Saturn family of launch vehicles
length 17.8 m
58.6 ft
manufacturer Douglas Aircraft Company
notableMission Apollo 11
Apollo 13
Apollo 8
numberOfEngines 1
operator NASA
oxidizer liquid oxygen
partOf Saturn I
Saturn IB
Saturn V
propellantType liquid hydrogen
propulsionType liquid-fueled rocket engine
rocketEngine J-2
stageNumberOnSaturnIB second stage
stageNumberOnSaturnV third stage
status retired
successorTo S-IV stage
linked to: S-IV
thrustVacuum about 1,033 kN
about 232,000 lbf
usedFor placing Apollo spacecraft into Earth orbit
translunar injection
usedForMissionPhase parking Earth orbit insertion
translunar injection burn
usedInProgram Apollo program
usedOnVehicle Saturn IB
Saturn V
usedWithSpacecraft Apollo Command and Service Module
Apollo Lunar Module

How these facts were elicited

Referenced by (8)

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

Saturn V thirdStage S-IVB
J-2 usedOnStage Saturn V S-IVB stage
linked to: S-IVB
J-2 usedOnStage Saturn IB S-IVB stage
linked to: S-IVB
Skylab 1 rocketStageUsed Saturn V S-IVB third stage
linked to: S-IVB
Saturn IB secondStage S-IVB
CSM-103 separatedFrom Saturn V S-IVB stage in translunar trajectory
linked to: S-IVB
S-IV successor S-IVB
Mobile Launcher 2 compatibleWith Saturn V third stage (S-IVB)
linked to: S-IVB