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gptkbp:instance_of
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gptkb:satellite
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gptkbp:bfsLayer
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6
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gptkbp:bfsParent
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gptkb:Spacebus_4000_series
|
|
gptkbp:application
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gptkb:Telecommunications_company
onboard computer
|
|
gptkbp:collection_size
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up to 80 m²
|
|
gptkbp:communication
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C-band
Ku-band
|
|
gptkbp:connects
|
modular
|
|
gptkbp:controls
|
attitude control system
|
|
gptkbp:cooling_system
|
passive thermal control
|
|
gptkbp:cultural_heritage
|
gptkb:Spacebus_3000
|
|
gptkbp:data_bus_width
|
3.5 m x 2.5 m x 2.5 m
|
|
gptkbp:debut_year
|
gptkb:1995
multiple successful launches
|
|
gptkbp:electrification
|
solar panels
|
|
gptkbp:financial_performance
|
three-axis stabilization
|
|
gptkbp:frequency
|
L-band
S-band
|
|
gptkbp:fuel_capacity
|
up to 1000 kg
|
|
gptkbp:home_ground
|
telemetry and command
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Spacebus 4000 B
|
|
gptkbp:involved_units
|
over 30
|
|
gptkbp:launch_site
|
gptkb:Centre_Spatial_Guyanais
|
|
gptkbp:launch_vehicle
|
gptkb:Ariane_4
3000 kg
|
|
gptkbp:lifespan
|
15 years
|
|
gptkbp:manufacturer
|
gptkb:Thales_Alenia_Space
|
|
gptkbp:mission
|
gptkb:Telesat_Anik_F2
gptkb:Eutelsat_70_B
gptkb:SES-10
gptkb:Hispasat_1_C
gptkb:Turksat_3_A
gptkb:Eutelsat_117_West_B
gptkb:SES-4
gptkb:Eutelsat_115_West_B
gptkb:Eutelsat_172_B
gptkb:Intelsat_37e
gptkb:Eutelsat_113_West_A
gptkb:SES-6
gptkb:satellite
gptkb:Intelsat_901
deployable antennas
Eutelsat W1
|
|
gptkbp:propulsion
|
chemical propulsion
|
|
gptkbp:seating_capacity
|
up to 5000 kg
up to 10 k W
|