Statements (65)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:satellite
|
| gptkbp:application |
communications
|
| gptkbp:communication |
C-band
Ku-band Ka-band |
| gptkbp:connects |
geostationary satellite bus
|
| gptkbp:controls |
reaction wheels
|
| gptkbp:cooling_system |
passive and active systems
|
| gptkbp:debut_year |
multiple launches
|
| gptkbp:design |
15 years
|
| gptkbp:developer |
1990s
|
| gptkbp:features |
environmental protection
low power consumption multi-mission capability compact design redundant systems advanced navigation systems high thermal stability advanced signal processing advanced telemetry lightweight structure high operational flexibility onboard processing capabilities high altitude operation multi-band operation advanced ground control systems flexible payload options high data throughput high efficiency solar arrays high gain antennas high power capacity high reliability components modular payload integration advanced control algorithms high data integrity high radiation tolerance high frequency stability high thermal insulation high performance batteries advanced fault detection high efficiency converters high performance antennas modular power system modular thermal control |
| gptkbp:first_flight |
gptkb:1995
|
| https://www.w3.org/2000/01/rdf-schema#label |
Spacebus 4000 C3
|
| gptkbp:launch_vehicle |
gptkb:Ariane_4
|
| gptkbp:manufacturer |
gptkb:Thales_Alenia_Space
|
| gptkbp:market_segment |
commercial satellites
government satellites |
| gptkbp:mass |
approximately 3,000 kg
|
| gptkbp:mission |
gptkb:satellite
|
| gptkbp:notable_users |
gptkb:Telesat
gptkb:Eutelsat gptkb:Intelsat SESS. A. |
| gptkbp:powers |
up to 10 k W
|
| gptkbp:propulsion |
chemical propulsion system
|
| gptkbp:reliability |
high reliability
|
| gptkbp:seating_capacity |
up to 1,000 kg
|
| gptkbp:setting |
modular design
|
| gptkbp:successor |
gptkb:Spacebus_4000_B
|
| gptkbp:bfsParent |
gptkb:Turksat_4_B
gptkb:Nilesat_244 |
| gptkbp:bfsLayer |
6
|