|
gptkbp:instance_of
|
gptkb:satellite
|
|
gptkbp:communication_system
|
gptkb:broadcasting
internet access
C-band
Ku-band
telephony
Ka-band
|
|
gptkbp:competitors
|
gptkb:Thales_Alenia_Space
gptkb:Boeing_702_X
gptkb:SSL_(Maxar)
gptkb:SSL_1300
gptkb:Airbus_Eurostar
gptkb:Lockheed_Martin
gptkb:Northrop_Grumman
gptkb:Airbus_Defence_and_Space
gptkb:Lockheed_Martin_A2100
gptkb:Boeing_601
gptkb:Hughes_HS-601
gptkb:Northrop_Grumman_GEOStar
|
|
gptkbp:control_system
|
digital control system
|
|
gptkbp:controls
|
reaction wheels
|
|
gptkbp:cooling_system
|
passive thermal control
|
|
gptkbp:data_usage
|
up to 1 Gbps
|
|
gptkbp:debut
|
gptkb:1997
|
|
gptkbp:design
|
15 years
modular design
|
|
gptkbp:design_features
|
digital signal processing
modular architecture
redundant systems
high data rate transmission
flexible payload options
high efficiency solar arrays
high power capacity
advanced thermal control
onboard propulsion system
|
|
gptkbp:designed_by
|
gptkb:Boeing
|
|
gptkbp:development
|
gptkb:Boeing_601
1990s
|
|
gptkbp:first_flight
|
gptkb:1997
|
|
gptkbp:home_ground
|
Boeing Ground Systems
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Boeing 702
|
|
gptkbp:launch_date
|
gptkb:1997
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
gptkb:Kennedy_Space_Center
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:launch_vehicle
|
gptkb:Space_X_Falcon_9
gptkb:Atlas_V
|
|
gptkbp:launched
|
over 30
|
|
gptkbp:manufacturer
|
gptkb:Boeing_Defense,_Space_&_Security
gptkb:Boeing
|
|
gptkbp:market_segment
|
military satellites
commercial satellites
government satellites
|
|
gptkbp:mass
|
approximately 5,000 kg
|
|
gptkbp:notable_features
|
gptkb:advanced_technology
high reliability
flexible payload configurations
high power capacity
|
|
gptkbp:notable_users
|
gptkb:Telesat
gptkb:Eutelsat
gptkb:Inmarsat
gptkb:Intelsat
gptkb:SES_S._A.
|
|
gptkbp:number_built
|
over 30 satellites
|
|
gptkbp:operational_status
|
operational
|
|
gptkbp:operational_use
|
15 years
|
|
gptkbp:orbit_type
|
gptkb:geostationary_orbit
phased array antenna
|
|
gptkbp:orbital_period
|
approximately 15 years
|
|
gptkbp:payload_capacity
|
up to 20 k W
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:propulsion
|
ion propulsion
|
|
gptkbp:purpose
|
communications
|
|
gptkbp:reliability
|
high
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
gptkb:Boeing_702_X
|
|
gptkbp:used_for
|
communications
|
|
gptkbp:bfsParent
|
gptkb:MEASAT-3b
gptkb:Intelsat_satellites
|
|
gptkbp:bfsLayer
|
5
|