|
gptkbp:instanceOf
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gptkb:satellite
|
|
gptkbp:alsoKnownAs
|
gptkb:Boeing_702
gptkb:BSS-702
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:firstRun
|
1999
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
HS-702 satellite bus
|
|
gptkbp:introduced
|
1997
|
|
gptkbp:launchMass
|
3,000 to 6,000 kg
|
|
gptkbp:manufacturer
|
gptkb:Boeing_Satellite_Systems
gptkb:Hughes_Space_and_Communications
|
|
gptkbp:notableFeature
|
gptkb:Xenon_Ion_Propulsion_System_(XIPS)
modular design
high power capability
|
|
gptkbp:notableUser
|
gptkb:Sirius_Satellite_Radio
gptkb:XM_Satellite_Radio
gptkb:DirecTV
gptkb:AsiaSat
gptkb:Intelsat
gptkb:PanAmSat
gptkb:NSS
gptkb:Inmarsat
gptkb:Eutelsat
gptkb:Telesat
Yamal
|
|
gptkbp:numberOfIssues
|
solar array degradation (early models)
|
|
gptkbp:orbitType
|
geostationary
|
|
gptkbp:payload
|
up to 6,000 kg
|
|
gptkbp:power_capability
|
10 to 18 kW
|
|
gptkbp:predecessor
|
gptkb:HS-601_satellite_bus
|
|
gptkbp:propulsion
|
bi-propellant chemical propulsion
ion propulsion (optional)
|
|
gptkbp:solarArrays
|
gallium arsenide solar cells
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
gptkb:BSS-702
|
|
gptkbp:usedFor
|
communications satellites
|
|
gptkbp:variant
|
gptkb:BSS-702HP
gptkb:BSS-702MP
gptkb:BSS-702SP
|
|
gptkbp:bfsParent
|
gptkb:Hughes_Space_and_Communications
|
|
gptkbp:bfsLayer
|
6
|