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gptkbp:instance_of
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gptkb:satellite
|
|
gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Eutelsat_36_B
|
|
gptkbp:application
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gptkb:computer
gptkb:Telecommunications_company
on-board computer
|
|
gptkbp:communication
|
batteries
solar panels
C-band
Ku-band
Ka-band
power distribution unit
|
|
gptkbp:connects
|
geostationary satellite bus
|
|
gptkbp:controls
|
thrusters
reaction wheels
magnetic torquers
|
|
gptkbp:cooling_system
|
passive thermal control
active thermal control
|
|
gptkbp:debut_year
|
multiple successful launches
|
|
gptkbp:design
|
15 years
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Spacebus 4000 series
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz
gptkb:Falcon_9
gptkb:opera
gptkb:Atlas_V
|
|
gptkbp:manufacturer
|
gptkb:Thales_Alenia_Space
|
|
gptkbp:market_segment
|
military satellites
commercial satellites
government satellites
|
|
gptkbp:mass
|
3000 kg
|
|
gptkbp:mission
|
gptkb:satellite
|
|
gptkbp:notable_users
|
gptkb:Eutelsat
gptkb:Inmarsat
gptkb:Intelsat
gptkb:Turksat
SESS. A.
|
|
gptkbp:powers
|
5 k W
|
|
gptkbp:produced_by
|
operational
in service
proven technology
|
|
gptkbp:propulsion
|
gptkb:rocket
chemical propulsion
|
|
gptkbp:seating_capacity
|
up to 6000 kg
|
|
gptkbp:successor
|
gptkb:Spacebus_4000_B
gptkb:Spacebus_4000_C
gptkb:Spacebus_4000_H
|