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gptkbp:instance_of
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gptkb:bus_services
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gptkbp:application
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gptkb:broadcasting
gptkb:scientific_research
weather monitoring
military communications
data relay
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gptkbp:cooling_system
|
active and passive systems
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gptkbp:design
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15 years
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gptkbp:financial_stability
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three-axis stabilization
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gptkbp:first_flight
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gptkb:1996
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|
https://www.w3.org/2000/01/rdf-schema#label
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A2100 satellite bus
|
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gptkbp:launch_vehicle
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gptkb:Atlas_V
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|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
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gptkbp:mass
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approximately 3,000 kg
|
|
gptkbp:orbit_type
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gptkb:Direc_TV_10
gptkb:Echo_Star_14
gptkb:Hispasat_1_E
gptkb:Intelsat_14
gptkb:Intelsat_22
gptkb:SES-3
gptkb:Telesat_Anik_F3
gptkb:geostationary_orbit
gptkb:SES-49
gptkb:Intelsat_15
gptkb:SES-1
gptkb:SES-10
gptkb:SES-20
gptkb:SES-16
gptkb:Intelsat_29e
gptkb:SES-12
gptkb:SES-14
gptkb:SES-15
gptkb:SES-17
gptkb:SES-18
gptkb:SES-19
gptkb:SES-24
SES-21
SES-22
SES-25
SES-26
SES-28
SES-29
SES-30
SES-31
SES-32
SES-33
SES-34
SES-35
SES-36
SES-38
SES-40
SES-41
SES-42
SES-43
SES-44
SES-46
SES-47
SES-48
SES-50
SES-23
SES-27
SES-37
SES-39
SES-45
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|
gptkbp:payload_capacity
|
up to 6,000 kg
|
|
gptkbp:powers
|
up to 10 k W
|
|
gptkbp:propulsion
|
chemical propulsion
|
|
gptkbp:protocol
|
multiple protocols supported
|
|
gptkbp:used_for
|
communications
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gptkbp:bfsParent
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gptkb:SBIRS_GEO-1
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gptkbp:bfsLayer
|
6
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