ICPS
E323529
ICPS (Interim Cryogenic Propulsion Stage) is a liquid hydrogen–liquid oxygen upper stage used on NASA’s Space Launch System to provide orbital insertion and translunar injection for early Artemis missions.
All labels observed (1)
| Label | Occurrences |
|---|---|
| ICPS canonical | 1 |
Statements (46)
| Predicate | Object |
|---|---|
| instanceOf |
cryogenic propulsion stage
ⓘ
rocket upper stage ⓘ spacecraft propulsion system ⓘ |
| abbreviationOf | Interim Cryogenic Propulsion Stage ⓘ |
| belongsToProgram |
Space Launch System
ⓘ
surface form:
Space Launch System program
|
| countryOfOrigin |
United States of America
ⓘ
surface form:
United States
|
| derivedFrom | Delta Cryogenic Second Stage ⓘ |
| designedAs | interim upper stage for SLS ⓘ |
| designedFor | human spaceflight support ⓘ |
| developedFor | NASA ⓘ |
| engineType |
RL10
ⓘ
surface form:
RL10 engine family
|
| fullName | Interim Cryogenic Propulsion Stage ⓘ |
| launchSite | Kennedy Space Center Launch Complex 39B ⓘ |
| launchVehicleConfiguration |
Space Launch System
ⓘ
surface form:
Space Launch System Block 1
|
| launchVehicleFamily |
Space Launch System
ⓘ
surface form:
NASA Space Launch System
|
| manufacturer | United Launch Alliance ⓘ |
| missionDestination | Moon ⓘ |
| missionProfile | Earth orbit to translunar trajectory ⓘ |
| operatedBy | NASA ⓘ |
| orbitType | Earth parking orbit ⓘ |
| oxidizer | liquid oxygen ⓘ |
| performs |
perigee raise burns
ⓘ
translunar injection burns ⓘ |
| primaryFunction |
orbital insertion
ⓘ
translunar injection ⓘ |
| propellantType |
liquid hydrogen
ⓘ
liquid oxygen ⓘ |
| propulsion | liquid hydrogen–liquid oxygen ⓘ |
| provides | in-space propulsion for SLS ⓘ |
| replacedBy |
Exploration Upper Stage
ⓘ
surface form:
Exploration Upper Stage (planned)
|
| replaces |
Delta Cryogenic Second Stage
ⓘ
surface form:
Delta Cryogenic Second Stage derivative
|
| role | upper stage ⓘ |
| spaceAgency | NASA ⓘ |
| stageNumber | second stage ⓘ |
| status | operational ⓘ |
| technologyType | expendable launch vehicle stage ⓘ |
| usedFor | deep space exploration missions ⓘ |
| usedOnLaunchVehicle | Space Launch System ⓘ |
| usedOnMission |
Artemis I
ⓘ
Artemis II ⓘ
surface form:
Artemis II (planned)
|
| usedOnMissionPhase | early Artemis missions ⓘ |
| usedOnMissionType |
Artemis program
ⓘ
surface form:
Artemis missions
lunar missions ⓘ |
| usedOnProgram | Artemis program ⓘ |
| usedWith | Orion spacecraft ⓘ |
| usesPropulsionCycle | cryogenic ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.