Power and Propulsion Element (PPE)
GPTKB entity
Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:fundedBy |
gptkb:NASA
|
| https://www.w3.org/2000/01/rdf-schema#label |
Power and Propulsion Element (PPE)
|
| gptkbp:launchDate |
2025
|
| gptkbp:launchVehicle |
gptkb:Falcon_Heavy
|
| gptkbp:length |
~12 meters
|
| gptkbp:manufacturer |
gptkb:Maxar_Technologies
|
| gptkbp:mass |
~8,500 kg
|
| gptkbp:mission |
gptkb:Artemis_program
|
| gptkbp:operator |
gptkb:NASA
|
| gptkbp:partOf |
gptkb:Lunar_Gateway
|
| gptkbp:plannedOrbit |
gptkb:near-rectilinear_halo_orbit_(NRHO)_around_the_Moon
|
| gptkbp:powerOutput |
60 kW
|
| gptkbp:primaryUse |
provide power and propulsion for Lunar Gateway
|
| gptkbp:propulsion |
solar electric propulsion
|
| gptkbp:provides |
attitude control for Lunar Gateway
communications for Lunar Gateway orbit transfer capability for Lunar Gateway |
| gptkbp:solarArrays |
gptkb:Roll-Out_Solar_Arrays_(ROSA)
|
| gptkbp:bfsParent |
gptkb:Lunar_Gateway
|
| gptkbp:bfsLayer |
5
|