Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:designedFor |
geostationary satellites
|
| gptkbp:duration |
15 years design life
|
| gptkbp:firstRun |
2001
|
| gptkbp:introduced |
late 1990s
|
| gptkbp:launchMass |
up to 6,000 kg
|
| gptkbp:manufacturer |
gptkb:Boeing
|
| gptkbp:notableFeature |
high power capability
|
| gptkbp:notableUser |
gptkb:DIRECTV
gptkb:Inmarsat gptkb:Eutelsat gptkb:Telesat |
| gptkbp:part_of |
gptkb:Boeing_702_series
|
| gptkbp:power_capability |
up to 18 kW
|
| gptkbp:predecessor |
gptkb:Boeing_601
|
| gptkbp:propulsion |
chemical and electric propulsion
|
| gptkbp:solarArrays |
triple-junction gallium arsenide
|
| gptkbp:successor |
gptkb:Boeing_702MP
|
| gptkbp:usedFor |
communications satellites
|
| gptkbp:bfsParent |
gptkb:Boeing_702X_satellite_platform
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Boeing 702HP satellite bus
|