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gptkbp:instance_of
|
gptkb:bus_services
|
|
gptkbp:communication_system
|
C-band
Ku-band
|
|
gptkbp:control_system
|
digital control system
|
|
gptkbp:data_usage
|
up to 1 Gbps
|
|
gptkbp:debut
|
2000-12-20
|
|
gptkbp:decommissioned
|
gptkb:2010
|
|
gptkbp:design_features
|
modular design
high reliability
redundant systems
|
|
gptkbp:development_cost
|
estimated at $100 million
|
|
gptkbp:first_flight
|
gptkb:1986
|
|
gptkbp:home_ground
|
ground control stations worldwide
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Boeing 601 bus
|
|
gptkbp:launch_date
|
1986-03-05
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral
gptkb:Baikonur_Cosmodrome
gptkb:Kourou
|
|
gptkbp:launch_vehicle
|
gptkb:Atlas_II
|
|
gptkbp:legacy
|
gptkb:Boeing_601_series
|
|
gptkbp:manufacturer
|
gptkb:Boeing
|
|
gptkbp:notable_users
|
gptkb:Telesat
gptkb:Intelsat
gptkb:Hughes_Communications
gptkb:SES_S._A.
|
|
gptkbp:number_built
|
over 30
|
|
gptkbp:operated_by
|
various telecommunications companies
|
|
gptkbp:operational_use
|
15 years
|
|
gptkbp:orbit_type
|
gptkb:geostationary_orbit
|
|
gptkbp:payload_capacity
|
up to 3,000 kg
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:propulsion
|
chemical propulsion
|
|
gptkbp:purpose
|
communications
|
|
gptkbp:related_to
|
gptkb:Boeing_702_HP
gptkb:Boeing_702_SP
gptkb:Boeing_702_series
gptkb:Boeing_702_MP
|
|
gptkbp:satellite_bus_type
|
geostationary satellite bus
high-power satellite bus
multi-mission satellite bus
|
|
gptkbp:stabilization_system
|
three-axis stabilization
|
|
gptkbp:successor
|
gptkb:Boeing_702
|
|
gptkbp:transponders
|
multiple transponders
|
|
gptkbp:weight
|
approximately 1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:TDRS-21
gptkb:Boeing_601
gptkb:Boeing_601_satellite_platform
|
|
gptkbp:bfsLayer
|
6
|