Power and Propulsion Element
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:collaboratesWith |
gptkb:European_Space_Agency
|
| https://www.w3.org/2000/01/rdf-schema#label |
Power and Propulsion Element
|
| gptkbp:launchDate |
2025
|
| gptkbp:launchVehicle |
gptkb:Falcon_Heavy
|
| gptkbp:length |
~18 meters (with arrays deployed)
|
| gptkbp:location |
Near-rectilinear halo orbit (NRHO) around the Moon
|
| gptkbp:manufacturer |
gptkb:Maxar_Technologies
|
| gptkbp:mass |
~8,500 kg
|
| gptkbp:missionType |
gptkb:satellite
|
| gptkbp:operator |
gptkb:NASA
|
| gptkbp:partOf |
gptkb:Lunar_Gateway
|
| gptkbp:propulsion |
solar electric propulsion
|
| gptkbp:provides |
attitude control for Gateway
communications for Gateway orbital transfer capability for Gateway |
| gptkbp:purpose |
provide power to Gateway
provide propulsion to Gateway |
| gptkbp:solarArrays |
gptkb:Roll-Out_Solar_Array_(ROSA)
|
| gptkbp:status |
under development
|
| gptkbp:bfsParent |
gptkb:NASA_Gateway_program
gptkb:NASA_Lunar_Gateway_program |
| gptkbp:bfsLayer |
6
|