Interim Cryogenic Propulsion Stage (ICPS)
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:derivedFrom |
gptkb:Delta_Cryogenic_Second_Stage_(DCSS)
|
| gptkbp:diameter |
5.1 meters
|
| gptkbp:engine |
gptkb:Aerojet_Rocketdyne_RL10B-2
|
| gptkbp:firstFlight |
2022
|
| https://www.w3.org/2000/01/rdf-schema#label |
Interim Cryogenic Propulsion Stage (ICPS)
|
| gptkbp:length |
13.7 meters
|
| gptkbp:manufacturer |
gptkb:Boeing
|
| gptkbp:mass |
approx. 30,000 kg
|
| gptkbp:numberOfEngines |
1
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:purpose |
trans-lunar injection
|
| gptkbp:replacedBy |
Exploration Upper Stage (EUS) (future)
|
| gptkbp:status |
operational
|
| gptkbp:thrust |
110 kN
|
| gptkbp:usedFor |
deep space missions
|
| gptkbp:usedOn |
gptkb:Artemis_II
gptkb:Space_Launch_System_(SLS) gptkb:Artemis_I |
| gptkbp:bfsParent |
gptkb:SLS_(Space_Launch_System)
|
| gptkbp:bfsLayer |
6
|