Orion spacecraft service module (planned)
GPTKB entity
Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
spacecraft service module
|
| gptkbp:countryOfOrigin |
gptkb:European_Union
|
| gptkbp:culturalHeritage |
gptkb:Automated_Transfer_Vehicle_(ATV)
|
| gptkbp:diameter |
4.1 meters
|
| gptkbp:engine |
gptkb:AJ10-190
|
| gptkbp:firstFlight |
2022
|
| https://www.w3.org/2000/01/rdf-schema#label |
Orion spacecraft service module (planned)
|
| gptkbp:launchVehicle |
gptkb:Space_Launch_System
|
| gptkbp:length |
4 meters
|
| gptkbp:mainEngineThrust |
27 kN
|
| gptkbp:manufacturer |
gptkb:ESA
gptkb:Airbus_Defence_and_Space |
| gptkbp:mass |
15,461 kg (fully loaded)
|
| gptkbp:operator |
gptkb:NASA
|
| gptkbp:partOf |
gptkb:Orion_spacecraft
|
| gptkbp:propulsion |
MMH/N2O4
|
| gptkbp:provides |
gptkb:water
power air propulsion thermal control consumables for crew |
| gptkbp:purpose |
support crewed deep space missions
|
| gptkbp:solarArrays |
4
19 meters |
| gptkbp:usedIn |
gptkb:Artemis_II_(planned)
gptkb:Artemis_I |
| gptkbp:bfsParent |
gptkb:RL10_engine
|
| gptkbp:bfsLayer |
6
|