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gptkbp:instance_of
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gptkb:satellite
|
|
gptkbp:communication_system
|
C-band
Ku-band
Ka-band
|
|
gptkbp:control_system
|
digital control system
|
|
gptkbp:cooling_system
|
passive thermal control
|
|
gptkbp:data_usage
|
high data rate communications
|
|
gptkbp:debut
|
multiple launches since 1996
|
|
gptkbp:design
|
modular design
geostationary satellite
|
|
gptkbp:development
|
early 1990s
A2100 A
A2100 B
A2100 C
A2100 M
|
|
gptkbp:first_flight
|
gptkb:1996
|
|
gptkbp:frequency
|
multiple frequency bands
|
|
gptkbp:home_ground
|
ground control stations
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lockheed Martin A2100
|
|
gptkbp:integration
|
integrated payloads
|
|
gptkbp:key_feature
|
high throughput
high power output
long operational life
flexible payload configurations
advanced communication capabilities
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral
gptkb:Baikonur_Cosmodrome
gptkb:Kourou
|
|
gptkbp:launch_vehicle
|
gptkb:Atlas_V
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:market_segment
|
commercial satellite market
government satellite market
|
|
gptkbp:notable_users
|
gptkb:Telesat
gptkb:Inmarsat
gptkb:Hughes_Network_Systems
gptkb:Intelsat
gptkb:SES_S._A.
|
|
gptkbp:operational_use
|
15 years
|
|
gptkbp:orbit_type
|
gptkb:geostationary_orbit
deployable antennas
|
|
gptkbp:payload_capacity
|
up to 20 transponders
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:production_years
|
gptkb:1996
|
|
gptkbp:propulsion
|
gptkb:Team_Rocket
chemical propulsion
|
|
gptkbp:purpose
|
communications
|
|
gptkbp:regulatory_compliance
|
FCC compliance
ITU compliance
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
A2100 X
|
|
gptkbp:weight
|
approximately 3,000 kg
|
|
gptkbp:bfsParent
|
gptkb:Advanced_Extremely_High_Frequency
gptkb:GPS_IIF_series
gptkb:Boeing_702
|
|
gptkbp:bfsLayer
|
6
|