Centaur upper stage
E288033
The Centaur upper stage is a high-energy rocket stage developed by the United States that pioneered the use of liquid hydrogen and liquid oxygen propellants to boost payloads from low Earth orbit to higher orbits and interplanetary trajectories.
All labels observed (4)
| Label | Occurrences |
|---|---|
| Centaur upper stage canonical | 3 |
| Atlas V Centaur upper stage | 1 |
| Dual-Engine Centaur | 1 |
| Single-Engine Centaur | 1 |
Statements (50)
| Predicate | Object |
|---|---|
| instanceOf |
expendable launch vehicle stage
ⓘ
rocket upper stage ⓘ |
| configurationVariant |
Centaur
ⓘ
surface form:
Centaur D
Centaur ⓘ
surface form:
Centaur D-1A
Centaur G-Prime ⓘ
surface form:
Centaur D-1T
Centaur G-Prime ⓘ
surface form:
Centaur G
Centaur G-Prime ⓘ Centaur G-Prime ⓘ
surface form:
Centaur II
Centaur G-Prime ⓘ
surface form:
Centaur III
Centaur V ⓘ Centaur V ⓘ
surface form:
Centaur V-AC
Centaur T ⓘ
surface form:
Centaur V-SEC
|
| countryOfOrigin |
United States of America
ⓘ
surface form:
United States
|
| developer |
Convair
ⓘ
General Dynamics ⓘ Lockheed Martin ⓘ United Launch Alliance ⓘ |
| engineManufacturer | Aerojet Rocketdyne ⓘ |
| engineTypeUsed | RL10 ⓘ |
| firstFlight | 1962-05-08 ⓘ |
| firstLaunchVehicle | Atlas LV-3C ⓘ |
| notableCapability |
high specific impulse
ⓘ
multiple restarts in space ⓘ |
| notableMission |
Cassini–Huygens
ⓘ
surface form:
Cassini–Huygens mission
New Horizons ⓘ
surface form:
New Horizons mission
Pioneer plaque project ⓘ
surface form:
Pioneer interplanetary missions
Surveyor lunar lander launches ⓘ Voyager program ⓘ
surface form:
Voyager missions
|
| operatedBy | United Launch Alliance ⓘ |
| oxidizer | liquid oxygen ⓘ |
| pioneeredUseOf | liquid hydrogen and liquid oxygen propellant combination for upper stages ⓘ |
| primaryFunction |
boost payloads from low Earth orbit to higher orbits
ⓘ
send payloads on interplanetary trajectories ⓘ |
| propellant |
liquid hydrogen
ⓘ
liquid oxygen ⓘ |
| status | operational ⓘ |
| typicalEngineCount |
1
ⓘ
2 ⓘ |
| usedForMissionType |
Earth observation satellite deployment
ⓘ
geostationary transfer orbit missions ⓘ interplanetary science missions ⓘ national security payload deployment ⓘ |
| usedOnLaunchVehicle |
Atlas II
ⓘ
Atlas III ⓘ Atlas V ⓘ Atlas-Centaur ⓘ Titan IIIE ⓘ Titan IV ⓘ Vulcan Centaur ⓘ |
| usesCryogenicPropellants | true ⓘ |
Referenced by (6)
Full triples — surface form annotated when it differs from this entity's canonical label.
this entity surface form:
Dual-Engine Centaur
this entity surface form:
Single-Engine Centaur