Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:capacity |
up to 8 kW
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:firstRun |
2001
|
| https://www.w3.org/2000/01/rdf-schema#label |
Spacebus 4000C2
|
| gptkbp:launchMass |
up to 4100 kg
|
| gptkbp:manufacturer |
gptkb:Thales_Alenia_Space
|
| gptkbp:part_of |
Spacebus 4000 series
|
| gptkbp:predecessor |
Spacebus 3000
|
| gptkbp:successor |
gptkb:Spacebus_Neo
|
| gptkbp:used_in |
gptkb:Turksat
gptkb:Nilesat gptkb:Arabsat gptkb:Eutelsat |
| gptkbp:usedFor |
geostationary communications satellites
|
| gptkbp:bfsParent |
gptkb:ChinaSat_6B
gptkb:Chinasat_12 gptkb:Chinasat_9 gptkb:Intelsat_25 |
| gptkbp:bfsLayer |
6
|