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)
| Label | Occurrences |
|---|---|
| S-IVB canonical | 3 |
| Saturn IB S-IVB stage | 1 |
| Saturn V S-IVB stage | 1 |
| Saturn V S-IVB stage in translunar trajectory | 1 |
| Saturn V S-IVB third stage | 1 |
| Saturn V third stage (S-IVB) | 1 |
Statements (45)
| Predicate | Object |
|---|---|
| instanceOf |
rocket stage
ⓘ
upper stage ⓘ |
| burnCapability | restartable in orbit ⓘ |
| countryOfOrigin |
United States of America
ⓘ
surface form:
United States
|
| developedFor |
Saturn I
ⓘ
surface form:
Saturn I Block II
|
| 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 rocket family
ⓘ
surface form:
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
ⓘ
surface form:
S-IV stage
|
| 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
ⓘ
surface form:
Apollo Command and Service Module
Apollo Lunar Module ⓘ |
Referenced by (8)
Full triples — surface form annotated when it differs from this entity's canonical label.
this entity surface form:
Saturn V S-IVB stage
this entity surface form:
Saturn IB S-IVB stage
this entity surface form:
Saturn V S-IVB third stage
this entity surface form:
Saturn V S-IVB stage in translunar trajectory
this entity surface form:
Saturn V third stage (S-IVB)